Guided weaponry data (in-game values) Honorable mention for Jaek_ for making amazing videos on missile on YouTube If you want to reach enlightment, then you have to spade the Italian heli line, no talisman/ premium/ boosters


1	This sheet contains most of the useful values of guided weapons.

2	Author: Koppany99 aka JohnWick(9)
3	Co-Author:♥ gszabi99 ♥
4	Last change in stats was in 2.37.0.16
5	For the better understanding of the PID terms, read this wiki article: https://en.wikipedia.org/wiki/PID_controller#Controller_theory
6
7	If you found a mistake or have a suggestion fill out this form
8	If you want you can tip me on kofi
9	This page is pink, cuz fu thats why


1	Name:	AIM-9B	AIM-9B FGW. 2	AIM-9D	AIM-9E	AIM-9G	AIM-9H	AIM-9J	AIM-9N	AIM-9P	Flz.Lwf. LL 63/80	R-3S	R-13M	R-13M1	R-60	Firestreak	Red Top	SRAAM	PL-2	PL-5B	PL-7	R530E	R550 Magic 1	Rb 24	Rb 24J	Shafrir	Shafrir 2

2	Physical properties
3	Mass: [kg]	72,57	77,55	88,45	76,43	88,45	88,45	76,93	76,93	76,93	76,93	75,3	87,7	90,6	43,5	136	167,8292	70	75,3	84,5	89	193,5	89	72,57	76,93	65	93
4	Mass at end of booster burn: [kg]	55,8	60,79	55,8	57,5	55,8	55,8	58	58	58	58	54,8	60	60	33,5	96	131,9954	51	54,8	59,7	66	160	66	55,8	58	45	63
5	Mass at end of sustainer burn: [kg]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	148	-	-	-	-	-
6	Calibre: [mm]	127	127	127	127	127	127	127	127	127	127	127	127	127	120	222	230	165	127	127	157	263	157	127	127	140	150
7	Length: [m]	2,83	2,83	3	3	3	3	3,05	3,05	3,05	3,05	2,83	2,83	2,876	2,095	3,18	3,32	2,75	2,83	2,892	2,748	3,28	2,748	2,83	3,05	2,5	2,8
8	Engine properties
9	Force exerted by booster: [N]	17263	17263	11000	18100	11000	11000	18100	18100	18100	18100	17318	26000	26000	9500	38000	30500	15300	17318	27900	27000	34500	27000	17263	18100	17263	11400
10	Burn time of booster: [s]	2,2	2,2	5	2,2	5	5	2,2	2,2	2,2	2,2	2,2	2	2	3	1,9	2,5	3,2	2,2	2	2	2,7	2	2,2	2,2	2,2	5
11	Raw acceleration at ignition: [m/s²]	237,88	222,60	124,36	236,82	124,36	124,36	235,28	235,28	235,28	235,28	229,99	296,47	286,98	218,39	279,41	181,73	218,57	229,99	330,18	303,37	178,29	303,37	237,88	235,28	265,58	122,58
12	Specific impulse of booster: [s]	230,85	230,99	171,72	214,43	171,72	171,72	214,43	214,43	214,43	214,43	189,45	191,36	173,23	290,52	184,00	216,91	262,68	189,45	229,36	239,33	283,45	239,33	230,85	214,43	193,57	193,68
13	ΔV of booster: [m/s]	595,11	551,77	776,00	598,65	776,00	776,00	594,15	594,15	594,15	594,15	590,62	712,56	700,32	744,46	628,69	511,07	816,01	590,62	781,69	701,96	528,60	701,96	595,11	594,15	698,28	739,98
14	Booster start delay: [s]	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0
15	Force exerted by sustainer: [N]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	4000	-	-	-	-	-
16	Burn time of sustainer: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	6,5	-	-	-	-	-
17	Specific impulse of sustainer: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	220,86	-	-	-	-	-
18	ΔV of sustainer: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	168,92	-	-	-	-	-
19	Total ΔV: [m/s]	595,11	551,77	776,00	598,65	776,00	776,00	594,15	594,15	594,15	594,15	590,62	712,56	700,32	744,46	628,69	511,07	816,01	590,62	781,69	701,96	697,52	701,96	595,11	594,15	698,28	739,98
20	Fuse and warhead properties
21	Explosive mass: [kg of TNT equivalent]	7,616	7,616	4,6905	7,616	3,5328	3,5328	7,616	7,616	7,616	7,616	8,8	5,5	5,5	1,15	11,2	23,2239232	4	8,8	7,616	8	10,368	9,6	7,616	7,616	7,616	7,616
22	Proximity fuse:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
23	Proximity fuse range: [m]	9,144	9,144	5	5	5	5	5	5	5	5	9	5	5	3	10	12	5	5	9	9	8	5	9,144	5	5	5
24	Proximity fuse shell detection (80-200 mm):	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
25	Proximity fuse delay: [s]	2,2	2,2	1,8	0,5	1,8	1,8	0,5	0,5	0,5	0,5	0,5	0,5	0,5	0,5	2,49	1,3	0,5	0,5	0,5	0,5	1,5	1,8	2,2	0,5	0,5	0,5
26	Guidance properties
27	Guidance type:	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR
28	Guidance start delay: [s]	0,5	0,5	0,4	0,5	0,4	0,4	0,5	0,5	0,5	0,5	0,5	0,5	0,5	0,35	0,34	0,3	-	0,5	0,5	0,25	0,5	0,25	0,5	0,5	0,5	0,5
29	Guidance duration: [s]	20	20	60	20	60	60	40	40	40	40	21	60	60	25	13	30	3,7	21	23	25	100	25	20	40	20	30
30	Seeker warm up time: [s]	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1
31	Seeker search duration: [s]	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20
32	Field of view: [degrees]	4	4	2,5	2,5	2,5	2,5	2,5	2,5	2,5	2,5	3,5	3	2,5	5	5	2	5	4	2,4	2,5	2,5	2,5	4	2,5	4	4
33	Gimbal limit: [degrees]	25	25	40	40	40	40	40	40	40	40	28	40	40	45	30	60	50	28	40	30	45	30	25	40	25	30
34	Track rate: [degrees/second]	11	11	12	12	12	20	16,5	16,5	16,5	16,5	6	12	16,5	30	12	12	100	11	20	35	10	35	11	16,5	11	18
35	Uncaged seeker before launch:	No	No	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes	No	Yes	Yes	Yes	Yes	Yes	Yes	No	Yes	Yes	Yes	Yes	No	Yes	No	Yes
36	Maximum lock angle before launch: [degrees]	-	-	-	10	40	40	40	40	40	40	-	10	10	12	20	30	40	-	25	30	20	30	-	40	-	30
37	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	20	5	10	10	10	10	10	10	10	10	20	10	10	15	3	5	10	20	17	10	5	10	20	10	20	20
38	Lock-on range from rear-aspect: [km]	4	5,5	5,5	5,5	5,5	5,5	5,5	5,5	5,5	5,5	3,5	5,5	5,5	5	4	6	4	3,5	5,5	5,5	5,5	5,5	4	5,5	4	4
39	Flare and IRCM detection range: [km]	10	8	8	8	8	8	8	8	8	8	8,7	8	8	7,5	8	7	6	8,7	8	8	8	8	10	8	10	10
40	DIRCM detection range: [km]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
41	Head-on lock-on range against afterburning target: [km]	0,5	0,5	1	1	1	1	1	1	1	1	0,5	1	1	0,5	1	2,5	0,5	0,5	1	1	0,5	1	0,5	1	0,5	1
42	Maximum break lock time: [s]	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	1	3	3	3	3	3	3	3	3	3
43	Can be slaved to radar:	No	No	No	No	Yes	Yes	No	No	Yes	No	No	No	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	Yes	No	Yes	No	No
44	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	12	4	4	4	4	4	4	4	4	4
45	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	2600	1800	1800	1800	1800	1800	1800	1800	1800	1800
46	PID proportional term:	0,0005	0,0005	0,0055	0,0035	0,0055	0,0055	0,0025	0,0025	0,0025	0,0025	0,0025	0,01	0,0015	0,0015	0,004	0,0041	0,0004	0,0005	0,0045	0,0016	0,007	0,0016	0,0005	0,0025	0,0015	0,0045
47	PID integral term:	0,0531	0,0531	0,0631	0,0651	0,0631	0,0631	0,0406	0,0406	0,0406	0,0406	0,0491	0,005	0,0316	0,0496	0,0486	0,0386	0,002	0,0531	0,0466	0,0396	0,0451	0,0396	0,0531	0,0406	0,0571	0,0381
48	PID integral term limit:	1	1	1	1	1	1	1	1	1	1	1	0,5	1	1	1	1	0,7	1	1	1	1	1	1	1	1	1
49	PID derivative term:	0,0007	0,0007	0,0012	0,001	0,0012	0,0012	0,0006	0,0006	0,0006	0,0006	0,0006	0,002	0,0005	0,0005	0,0007	0,0007	0,0006	0,0007	0,0009	0,0005	0,011	0,0005	0,0007	0,0006	0,0004	0,0007
50	Flight characteristics
51	Maximum fin angle of attack: [degrees]	9,9	9,9	15,3	9,9	15,3	15,3	16,2	16,2	16,2	16,2	9,9	14,4	19,8	16,2	10,8	12,80088	-	9,9	15,3	32,04	16,2	32,04	9,9	16,2	8,1	16,2
52	Maximum fin lateral acceleration:	10,4	10,4	19,8	10,6	19,8	19,8	17,6	17,6	17,6	17,6	10,7		18,7	21,9	10,9	10,2787		10,4	31	27,3543	15,5	27,3543	10,4	17,6	11	18,5
53	Wing area multiplier:	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,25	1,3	1,3	-	1,4	1,4	1,45	1,4	1,45	1,4	1,4	1,4	1,4
54	Start speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
55	Maximum speed: [m/s]	1000	1000	1000	1000	1000	1000	1000	1000	1000	1000	1000	1000	1000	-	1000	-	1000	800	1000	-	-	-	1000	1000	1000	1000
56	Maximum statcard (useless) speed: [Mach]	1,7	1,7	2,5	2,5	2,5	2,5	2,5	2,5	2,5	2,5	1,7	2,4	2,4	2,5	3,4	3,4	2,4	1,7	2,5	3	2,7	3	1,7	2,5	1,7	2,1
57	Maximum statcard (useless) launch range: [km]	10	10	18	18	18	18	18	18	18	18	9	16	16	10	7	20	2	9	10	16	18	10	10	18	10	20
58	Flight time until guidance starts (delay): [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	0,5	-	-	-	-	-
59	Flight time when pull limit reaches 40%: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
60	Flight time when pull limit reaches 100%: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	2,5	-	-	-	-	-
61	Minimum range: [m]	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30
62	Maximum (flight) range: [km]	12	12	18	18	18	18	18	18	18	18	11	15	15	15	8	20	3	11	18	18	18	18	12	18	12	12
63	Maximum G-load: [G]	11	11	18	11	18	18	20	20	20	20	11	15	20	30	15	12	-	11	30	35	15	35	11	20	11	18
64	Maximum statcard (useless) G-load: [G]	10	10	18	10	18	18	20	20	20	20	10	15	20	30	15	12	20	10	30	35	15	35	10	20	11	18
65	Thrust vectoring:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	Yes	No	No	No	No	No	No	No	No	No
66	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	4,5	-	-	-	-	-	-	-	-	-
67	Additional Notes:								Identical to the AIM-9J currently.	AIM-9J with radar slaving	Swiss copy of AIM-9J										Chinese Magic1			Swedish AIM-9B	Swedish AIM-9P-3
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1	Name:	AIM-9L	AIM-9L/I	AIM-9M	AIM-9P-4	R-23T	R-24T	R-27T	R-27T1	R-27ET	R-27ET1	R-60M	R-60MK	R-73	R-73E	AAM-3	PL-5C	PL-8	PL-9	R550 Magic 2	Rb 74	Rb 74M	Python 3	Python 4	MAA-1 Piranha

2	Physical properties
3	Mass: [kg]	84,46	84,46	84,46	76,93	215	237	245	245	343	343	44	44	105	105	91	84,5	121	115	89	84,46	84,46	121	105	90
4	Mass at end of booster burn: [kg]	57,06	57,06	57,06	58	182	162	178,5	178,5	262,6	262,6	34	34	71	71	63,6	59,7	108	95	66	57,06	57,06	108	81	63
5	Mass at end of sustainer burn: [kg]	-	-	-	-	-	-	-	-	204,5	204,5	-	-	-	-	-	-	82,3	74,8	-	-	-	82,3	63	-
6	Calibre: [mm]	127	127	127	127	200	200	230	230	260	260	120	120	170	170	127	127	160	157	157	127	127	160	160	127
7	Length: [m]	2,85	2,85	2,85	3,05	4,16	4,194	3,7	3,7	4,5	4,5	2,095	2,095	2,9	2,9	3,02	2,892	2,999	2,992	2,748	2,85	2,85	2,999	3	2,85
8	Engine properties
9	Force exerted by booster: [N]	10800	10800	10800	18100	60000	50000	25125	25125	55275	55275	9500	9500	13750	13750	11952,69	27900	37675	35200	25000	10800	10800	37675	17600	27000
10	Burn time of booster: [s]	5,3	5,3	5,3	2,2	1,85	3	6	6	3,2	3,2	3	3	5,5	5,5	5,2	2	0,785	1,25	2,2	5,3	5,3	0,785	3	2,1
11	Raw acceleration at ignition: [m/s²]	127,87	127,87	127,87	235,28	279,07	210,97	102,55	102,55	161,15	161,15	215,91	215,91	130,95	130,95	131,35	330,18	311,36	306,09	280,90	127,87	127,87	311,36	167,62	300,00
12	Specific impulse of booster: [s]	212,95	212,95	212,95	214,43	342,88	203,87	231,08	231,08	224,26	224,26	290,52	290,52	226,73	226,73	231,23	229,36	231,91	224,26	243,76	212,95	212,95	231,91	224,26	214,07
13	ΔV of booster: [m/s]	819,27	819,27	819,27	594,15	560,49	760,93	717,86	717,86	587,62	587,62	734,81	734,81	870,31	870,31	812,64	781,69	258,57	420,32	714,96	819,27	819,27	258,57	570,92	749,02
14	Booster start delay: [s]	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0
15	Force exerted by sustainer: [N]	-	-	-	-	-	-	-	-	26630	26630	-	-	-	-	-	-	20500	16160	-	-	-	20500	7920	-
16	Burn time of sustainer: [s]	-	-	-	-	-	-	-	-	4,8	4,8	-	-	-	-	-	-	2,85	2,75	-	-	-	2,85	5	-
17	Specific impulse of sustainer: [s]	-	-	-	-	-	-	-	-	224,27	224,27	-	-	-	-	-	-	231,74	224,26	-	-	-	231,74	224,26	-
18	ΔV of sustainer: [m/s]	-	-	-	-	-	-	-	-	550,16	550,16	-	-	-	-	-	-	617,80	525,93	-	-	-	617,80	552,89	-
19	Total ΔV: [m/s]	819,27	819,27	819,27	594,15	560,49	760,93	717,86	717,86	1137,77	1137,77	734,81	734,81	870,31	870,31	812,64	781,69	876,38	946,25	714,96	819,27	819,27	876,38	1123,82	749,02
20	Fuse and warhead properties
21	Explosive mass: [kg of TNT equivalent]	4,5824	4,5824	4,5824	7,616	20,8	20,8	24	24	24	24	1,78875	1,78875	5,94	5,94	4,864	7,616	9,6	8,4	9,6	4,5824	4,5824	9,6	9,6	7,2
22	Proximity fuse:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
23	Proximity fuse range: [m]	5	5	5	5	10	10	8	8	8	8	3	3	6	6	6	9	7	7	8	5	5	7	7	5
24	Proximity fuse shell detection (80-200 mm):	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
25	Proximity fuse delay: [s]	1,8	1,8	1,8	0,5	1	1	2	2	2	2	0,5	0,5	0,5	0,5	1,5	0,5	0,5	0,5	1,8	1,8	1,8	0,5	0,5	1,8
26	Guidance properties
27	Guidance type:	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR	IR
28	Guidance start delay: [s]	0,4	0,4	0,4	0,5	0,5	0,5	0,35	0,35	0,35	0,35	0,35	0,35	0,15	0,15	0,4	0,5	0,5	0,5	0,25	0,4	0,4	0,5	0,2	0,5
29	Guidance duration: [s]	60	60	60	60	35	45	60	60	60	60	25	25	20	20	45	23	20	30	25	60	60	20	20	40
30	Seeker warm up time: [s]	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1
31	Seeker search duration: [s]	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20	20
32	Field of view: [degrees]	3,6	3,6	3,6	3,6	2,6	2,6	2	2	2	2	5	5	4,5	4,5	3,6	4	3,6	3	2,4	3,6	3,6	3,6	3,6	3,6
33	Gimbal limit: [degrees]	45	45	45	45	60	55	60	60	60	60	45	45	75	75	60	40	40	40	45	45	45	40	90	40
34	Track rate: [degrees/second]	22	22	22	22	12	20	30	30	30	30	30	30	60	60	30	20	20	20	60	22	22	20	45	50
35	Uncaged seeker before launch:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
36	Maximum lock angle before launch: [degrees]	40	40	40	40	60	55	45	45	45	45	20	20	45	45	40	25	30	30	45	40	40	30	60	30
37	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	10	10	10	10	7	7	5	5	5	5	7	7	15	15	10	17	12	12	10	10	10	12	15	12
38	Lock-on range from rear-aspect: [km]	11	11	11	11	12	16	18	18	18	18	7,4	7,4	11	11	11	11	11	11	11	11	11	11	11	11
39	Lock-on range from all-aspect: [km]	3	3	3	3	2,3	4,3	4,8	4,8	4,8	4,8	2	2	3,4	3,4	3	2,5	3	3	3,4	3	3	3	3,8	3
40	Flare detection range: [km]	11	11	11	11	12	15	15	15	15	15	7,4	7,4	10	10	11	11	11	11	10	11	11	11	11	11
41	IRCM detection range: [km]	11	11	11	11	12	15	15	15	15	15	7,4	7,4	-	-	11	11	11	11	-	11	11	11	-	11
42	DIRCM detection range: [km]	-	-	-	-	-	-	-	-	-	-	-	-	1	1	-	-	-	-	1	-	-	-	1	-
43	Head-on lock-on range against afterburning target: [km]	6	6	6	6	4	8	9	9	9	9	3	3	6	6	6	6	6	6	6	6	6	6	6	6
44	IRCCM:	No	Yes	Yes	No	No	No	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	No	No	No	Yes	No	Yes	No	Yes	No
45	IRCCM type:	-	Seeker shut off	Seeker shut off	-	-	-	FOV	FOV	FOV	FOV	-	-	FOV	FOV	Seeker shut off	-	-	-	FOV	-	Seeker shut off	-	FOV + Seeker shut off	-
46	IRCCM field of view: [degrees]	-	-	-	-	-	-	1,33	1,33	1,33	1,33	-	-	0,75	0,75	-	-	-	-	0,75	-	-	-	1,2	-
47	IRCCM rejection treshold:	-	0,1	0,1	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	0,1	-	-	-
48	IRCCM reaction time: [s]	-	0,02	0,02	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	0,02	-	-	-
49	Maximum break lock time: [s]	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3	3
50	Can be slaved to radar:	Yes	Yes	Yes	Yes	Yes	Yes	-	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
51	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4
52	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800
53	PID proportional term:	0,002	0,002	0,002	0,0025	0,0035	0,0025	0,006	0,006	0,0075	0,0075	0,0015	0,0015	Not	Not	0,0021	0,0045	0,0035	0,0021	0,0016	0,002	0,002	0,0035	0,0036	0,0016
54	PID integral term:	0,0361	0,0361	0,0361	0,0406	0,0346	0,0236	0,0311	0,0311	0,0466	0,0466	0,0496	0,0496	applicable	applicable	0,0401	0,0466	0,0346	0,0376	0,0341	0,0361	0,0361	0,0346	0,0341	0,0301
55	PID integral term limit:	1	1	1	1	1	1	1	1	1	1	1	1	dependent	dependent	1	1	1	1	1	1	1	1	1	1
56	PID derivative term:	0,0006	0,0006	0,0006	0,0006	0,001	0,0006	0,0013	0,0013	0,0009	0,0009	0,0005	0,0005	on flight time	on flight time	0,0008	0,0009	0,0007	0,0006	0,0005	0,0006	0,0006	0,0007	0,0007	0,0005
57	Flight characteristics
58	Maximum fin angle of attack: [degrees]	22,5	22,5	22,5	16,2	18,9	25,2	28,8	28,8	28,8	28,8	16,2	16,2	22,5	22,5	25,08858	15,3	19,8	22,32	32,04	24,3	22,5	19,8	19,8	23,86692
59	Maximum fin lateral acceleration:	37,5	37,5	37,5	17,6	15,9	21,9	36,96	36,96	36,96	36,96	21,9	21,9	45	45	37,1989	31	31,2	37,2052	27,3543	37,5	37,5	31,2	60	43,0575
60	Maximum AOA: [degrees]													40	40
61	Wing area multiplier:	1,4	1,4	1,4	1,4	1,35	1,35	1,4	1,4	1,4	1,4	1,25	1,25	1,4	1,4	1,3	1,4	1,4	1,4	1,45	1,4	1,4	1,4	1,45	1,4
62	Start speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	0	0	-	-	-	-	-	-	-	-	-	-
63	Maximum speed: [m/s]	1000	1000	1000	1000	1000	1500	1500	1500	1750	1750	-	-	-	-	1000	1000	1000	1500	-	1000	1000	1000	1000	1000
64	Maximum statcard (useless) speed: [Mach]	2,5	2,5	2,5	2,5	3	3,5	3,5	3,5	5,75	5,75	2,5	2,5	2,5	2,5	2,5	2,5	3,5	3,5	3	2,5	2,5	3,5	4	3,5
65	Maximum statcard (useless) launch range: [km]	18	18	18	18	27	50	50	50	100	100	10	10	30	30	18	16	18	28	10	18	18	18	30	18
66	Flight time until guidance starts (delay): [s]	-	-	-	-	0,5	0,5	0,35	0,35	0,35	0,35	-	-	-	-	-	-	-	-	-	-	-	-	-	-
67	Flight time when pull limit reaches 40%: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
68	Flight time when pull limit reaches 100%: [s]	-	-	-	-	2,5	1	0,4	0,4	0,4	0,4	-	-	-	-	-	-	-	-	-	-	-	-	-	-
69	Minimum range: [m]	30	30	30	30	30	30	20	20	20	20	30	30	30	30	30	30	30	30	30	30	30	30	30	30
70	Maximum (flight) range: [km]	18	18	18	18	27	45	50	50	67,5	67,5	15	15	25	25	18	18	18	28	18	18	18	18	30	18
71	Maximum G-load: [G]	30	30	30	20	20	24	30	30	35	35	30	30	40	40	40	30	40	35	35	30	30	40	50	45
72	Maximum statcard (useless) G-load: [G]	30	30	30	20	20	24	30	30	35	35	30	30	40	40	40	30	40	35	35	30	30	40	50	45
73	Thrust vectoring:	No	No	No	No	No	No	No	No	No	No	No	No	Yes	Yes	No	No	No	No	No	No	No	No	No	No
74	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	-	-	-	4,0500	4,0500	-	-	-	-	-	-	-	-	-	-
75	Additional Notes:		AIM-9M with smoke	AIM-9L with IRCCM against flares Low visiblity smoke motor Image found under artist Atamonica					Export version of T, no changes		Export version of ET, no changes		Identical to the R-60M currently.		Export version, no changes	Low visiblity smoke motor		Chinese Python 3.				AIM-9M copy
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1	Name:	AIM-92A ATAS	9M39V	9M336	Mistral SATCP	TY-90

2	Physical properties
3	Mass: [kg]	10,1	10,6	10,6	18,7	24
4	Mass at end of booster burn: [kg]	7,445	7,69	7,69	17,1	16,1
5	Mass at end of sustainer burn: [kg]	5,5	5,59	5,59	11,5	13,3
6	Calibre: [mm]	70	72,2	72,2	90	90
7	Length: [m]	1,52	1,68	1,68	1,86	1,862
8	Engine properties
9	Force exerted by booster: [N]	4340	2975	2975	0	4641,25
10	Burn time of booster: [s]	1,4	1,9	1,9	0	4
11	Raw acceleration at ignition: [m/s²]	429,70	280,66	280,66	0,00	193,39
12	Specific impulse of booster: [s]	233,28	198,01	198,01	0,00	239,55
13	ΔV of booster: [m/s]	697,98	623,39	623,39	0,00	938,20
14	Booster start delay: [s]	0	0,4	0,4	0	0
15	Force exerted by sustainer: [N]	675	705	705	5925	980
16	Burn time of sustainer: [s]	5,6	6,6	6,6	2,2	6
17	Specific impulse of sustainer: [s]	198,11	225,86	225,86	237,28	214,07
18	ΔV of sustainer: [m/s]	588,46	706,68	706,68	923,46	401,22
19	Total ΔV: [m/s]	1286,44	1330,08	1330,08	923,46	1339,42
20	Fuse and warhead properties
21	Explosive mass: [kg of TNT equivalent]	0,54	0,53	0,53	1,776	1,5
22	Proximity fuse:	No	Yes	Yes	Yes	Yes
23	Proximity fuse range: [m]	-	0,5	0,5	1,5	4
24	Proximity fuse shell detection (80-200 mm):	-	No	No	No	Yes
25	Proximity fuse delay: [s]	-	0,5	0,5	2	0,5
26	Guidance properties
27	Guidance type:	IR	IR	IR	IR	IR
28	Guidance start delay: [s]	0,3	0,7	0,7	0,1	0,5
29	Guidance duration: [s]	17	14	14	14	12
30	Seeker warm up time: [s]	2	2	2	2	2
31	Seeker search duration: [s]	60	60	60	60	60
32	Field of view: [degrees]	3	2	2	3	3
33	Gimbal limit: [degrees]	40	38	38	38	60
34	Track rate: [degrees/second]	12	12	12	20	40
35	Uncaged seeker before launch:	Yes	No	No	Yes	Yes
36	Maximum lock angle before launch: [degrees]	15	-	-	25	20
37	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	5	5	5	10	5
38	Lock-on range from rear-aspect: [km]	11	11	11	11	11
39	Lock-on range from all-aspect: [km]	6	6	6	6	6
40	Flare detection range: [km]	11	11	11	11	11
41	IRCM detection range: [km]	-	-	-	-	-
42	DIRCM detection range: [km]	1	1	1	1	1
43	IRCCM:	Yes	Yes	Yes	Yes	Yes
44	IRCCM type:	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off
45	IRCCM field of view: [degrees]	1,25	1	1	1,5	1,25
46	Head-on lock-on range against afterburning target: [km]	6	6	6	6	6
47	Maximum break lock time: [s]	3	5	5	5	3
48	Can be slaved to radar:	No	No	No	No	No
49	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4
50	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800
51	PID proportional term:	0,0056	0,0026	0,0026	0,0016	0,0005
52	PID integral term:	0,00841	0,1646	0,1646	0,0926	0,0271
53	PID integral term limit:	1	1	1	1	1
54	PID derivative term:	0,0005	0,0012	0,0012	0,0004	0,0002
55	Flight characteristics
56	Maximum fin angle of attack: [degrees]	4,185	4,185	4,185	3,6	18
57	Fins lateral acceleration:	-	14,16	14,16	-	-
58	Wing area multiplier:	1,05	1,05	1,05	1,05	1,2
59	Start speed: [m/s]	30	30	30	35	-
60	Maximum speed: [m/s]	1000	1000	1000	-	1000
61	Maximum statcard (useless) speed: [Mach]	2	1,7	1,7	2,5	2,2
62	Maximum statcard (useless) launch range: [km]	5	5	5,2	6	6
63	Minimum range: [m]	30	30	30	30	30
64	Maximum (flight) range: [km]	10	8	8	10	6
65	Maximum G-load: [G]	13	10,2	10,2	16	20
66	Maximum statcard (useless) G-load: [G]	13	10,2	10,2	16	20
67	Thrust vectoring:	No	No	No	No	No
68	Thrust vectoring angle: [degrees]	-	-	-	-	-
69	Additional Notes:			Copy-paste 9M39V when it was added.
70	IRCCM field of view is the FoV after lock-on, outside of this FoV other heat sources are ignored. This basically means, that for the seeker to not reject other heat source, like a flare, it must be inside the IRCCM field of view. For a quick comparison (Stinger values) 3° FoV means a 104 m radius circle at 4 km distance, while 1.25° FoV means a 44 m radius circle. At closer than 2 km range, the circle would be as large or smaller than the target, effectively making flaring useless.
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1	Name:	AIM-7C	AIM-7D	AIM-7E	AIM-7E-2 (dogfight)	AIM-7F	AIM-7M	AIM-9C	R-3R	R-23R	R-24R	R-27R	R-27R1	R-27ER	R-27ER1	Skyflash	Skyflash (dogfight)	Skyflash SuperTEMP	Aspide-1A	PL-11	R511	R530	Super 530F	Super 530D	Rb 71

2	Physical properties
3	Mass: [kg]	172	182,34	205	193,7	231,33	231,33	95,2544	75,3	223	244	253	253	350	350	193	193	208,2	230	230	172,5	193,5	245	270	193
4	Mass at end of booster burn: [kg]	144	144	146	146	193,68	193,68	67,85742	54,8	190	169	186	186	286	286	146	146	163	173	173	148,7	160	210,45	234	146
5	Mass at end of sustainer burn: [kg]	-	-	-	-	170,1	170,1	-	-	-	-	-	-	211,5	211,5	-	-	146	-	-	136,8	148	165	171,5	-
6	Calibre: [mm]	200	200	200	200	200	200	127	127	200	200	230	230	260	260	200	200	200	200	200	263	263	263	263	200
7	Length: [m]	3,66	3,66	3,66	3,66	3,662	3,662	3,023	2,83	4,46	4,487	4	4	4,7	4,7	3,66	3,66	3,66	3,7	3,7	3,28	3,28	3,54	3,8	3,66
8	Engine properties
9	Force exerted by booster: [N]	32200	41000	35000	35000	26940	26940	11000	17318	60000	50000	25125	25125	55275	55275	35000	35000	33900	37500	37500	15500	34500	38000	38700	35000
10	Burn time of booster: [s]	2,04	2,1	2,8	2,8	4,5	4,5	5	2,2	1,85	3	6	6	3,2	3,2	2,8	2,8	3	3,5	3,5	3	2,7	2	2	2,8
11	Raw acceleration at ignition: [m/s²]	187,21	224,85	170,73	180,69	116,46	116,46	115,48	229,99	269,06	204,92	99,31	99,31	157,93	157,93	181,35	181,35	162,82	163,04	163,04	89,86	178,29	155,10	143,33	181,35
12	Specific impulse of booster: [s]	239,14	228,92	169,32	209,43	328,23	328,23	204,64	189,45	342,88	203,87	229,36	229,36	281,73	281,73	212,55	212,55	229,36	234,72	234,72	199,16	283,45	224,23	219,16	212,55
13	ΔV of booster: [m/s]	416,84	530,12	563,75	580,82	571,98	571,98	680,84	590,62	538,68	734,54	692,20	692,20	558,12	558,12	581,92	581,92	550,69	655,76	655,76	290,07	528,60	334,38	307,67	581,92
14	Booster start delay: [s]	0,25	0,25	0,25	0,25	0,25	0,25	0	0	0	0	0	0	0	0	0,25	0,25	0,25	0,25	0,25	0	0	0	0	0,25
15	Force exerted by sustainer: [N]	-	-	-	-	6340	6340	-	-	-	-	-	-	26630	26630	-	-	9562	-	-	1765	4000	25000	16800	-
16	Burn time of sustainer: [s]	-	-	-	-	11	11	-	-	-	-	-	-	4,8	4,8	-	-	4	-	-	13,5	6,5	4	8	-
17	Specific impulse of sustainer: [s]	-	-	-	-	301,49	301,49	-	-	-	-	-	-	174,90	174,90	-	-	229,35	-	-	204,11	220,86	224,28	219,20	-
18	ΔV of sustainer: [m/s]	-	-	-	-	383,96	383,96	-	-	-	-	-	-	517,76	517,76	-	-	247,81	-	-	167,01	168,92	535,32	668,21	-
19	Total ΔV: [m/s]	416,84	530,12	563,75	580,82	955,94	955,94	680,84	590,62	538,68	734,54	692,20	692,20	1075,87	1075,87	581,92	581,92	798,50	655,76	655,76	457,09	697,52	869,70	975,88	581,92
20	Fuse and warhead properties
21	Explosive mass: [kg of TNT equivalent]	11,52	11,52	11,52	11,52	15,0912	15,0912	4,6905	8,8	20,8	20,8	24	24	24	24	11,52	11,52	11,52	10,24	10,24	10,24	10,368	10,368	10,368	11,52
22	Proximity fuse:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
23	Proximity fuse range: [m]	3	8	8	8	8	8	5	5	10	10	8	8	8	8	15,25	15,25	15,25	8	8	8	8	8	8	15,25
24	Proximity fuse shell detection (80-200 mm):	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
25	Proximity fuse delay: [s]	2	1,8	1,8	0,8	1,8	1,8	0,5	0,5	1,7	1,7	2	2	2	2	1,8	0,8	0,8	0,8	0,8	4	4	2,2	2,2	0,8
26	Guidance properties
27	Guidance type:	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH + IOG	SARH+IOG+DL	SARH+IOG+DL	SARH+IOG+DL	SARH+IOG+DL	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH	SARH
28	Guidance start delay: [s]	2	1,8	1,8	0,7	-	-	0,5	0,5	1,7	0,5	0,35	0,35	0,35	0,35	1,8	0,7	0,7	0,5	0,5	1,5	0,5	0,5	0,5	0,7
29	Guidance duration: [s]	20	40	40	40	75	75	60	21	35	45	60	60	60	60	40	40	50	45	45	30	25	60	60	40
30	Seeker warm up time: [s]	1	1,4	1,4	1,4	1,4	1,4	2	2	1	1	1	1	1	1	1,4	1,4	1,4	1,4	1,4	2	2	1.4	1.4	1,4
31	Seeker search duration: [s]	60	100	100	100	100	100	15	15	100	100	100	100	100	100	100	100	100	100	100	15	15	100	100	100
32	Gimbal limit: [degrees]	25	45	45	45	55	55	30	30	50	50	55	55	55	55	46	46	46	50	50	10	45	55	55	46
33	Track rate: [degrees/second]	12	12	12	12	20	20	12	12	12	20	20	20	20	20	44	44	44	12	12	12	12	12	12	44
34	Uncaged seeker before launch:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
35	Maximum lock angle before launch: [degrees]	15	15	35	35	35	35	30	30	50	50	55	55	55	55	35	35	35	35	15	10	40	55	55	35
36	Lock-on range from all-aspect: [km]	12	15	25	25	40	40	9	8	20	25	25	25	25	25	37	37	37	30	30	8	12,5	25	30	37
37	Maximum break lock time: [s]	5	5	5	5	20	20	3	3	3	15	60	60	60	60	5	5	20	5	5	3	3	20	20	5
38	Can lock after launch:	Yes	Yes	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	No	No	No	Yes	Yes
39	Band:	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I	I
40	Angular speed rejection threshold: [degrees/second]	-	-	-	-	30	30	-	-	-	30	30	30	30	30	30	30	30	45	45	-	-	30	30	30
41	Acceleration rejection threshold range: [m/s^2]	-	-	-	-	100-250	100-250	-	-	-	100-250	100-250	100-250	100-250	100-250	100-250	100-250	100-250	100-250	100-250	-	-	50-100	100-250	100-250
42	Sidelobe attenuation:	-18	-20	-20	-20	-20	-20	-13	-18	-20	-20	-20	-20	-20	-20	-20	-20	-20	-20	-20	-16	-18	-20	-20	-20
43	Transmitter power:	200	200	200	200	200	200	400	300	270	270	900	900	900	900	200	200	200	200	200	200	200	200	1000	200
44	Transmitter angle of half sensitivity:	10	10	10	10	12	12	5	5	10	10	3,5	3,5	3,5	3,5	10	10	2,6	12	12	5	5	5	3	10
45	Transmitter sidelobe sensitivity:	-26	-30	-30	-30	-30	-30	-25	-20	-30	-30	-30	-30	-30	-30	-30	-30	-30	-27	-27	-27	-27	-27	-30	-30
46	Receiver angle of half sensitivity:	14	13	13	13	13	13	15	16	11	11	13	13	13	13	12	10	10	12	12	10	10	10	10	10
47	Receiver sidelobe sensitivity:	-16	-17	-17	-17	-17	-17	-12	-14	-17	-17	-17	-17	-17	-17	-17	-17	-17	-17	-17	-15	-15	-17	-17	-17
48	Distance minimum value:	-	-	-	-	-	-	300	300	-	-	-	-	-	-	-	-	-	-	-	300	300	150	-	-
49	Distance maximum value:	-	-	-	-	-	-	15000	15000	-	-	-	-	-	-	-	-	-	-	-	38000	38000	75000	-	-
50	Distance width:	-	-	-	-	-	-	300	300	-	-	-	-	-	-	-	-	-	-	-	300	300	150	-	-
51	Distance minimum signal gate:	-	-	-	-	-	-	150	150	-	-	-	-	-	-	-	-	-	-	-	150	150	75	-	-
52	Distance refWidth:	-	-	-	-	-	-	1200	900	-	-	-	-	-	-	-	-	-	-	-	1500	1500	750	-	-
53	Doppler speed minimum value:	-2000	-3000	-3000	-3000	-3000	-3000	-	-	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-	-	-	-3000	-3000
54	Doppler speed maximum value:	2000	3000	3000	3000	3000	3000	-	-	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	-	-	-	3000	3000
55	Doppler speed width:	30	22	22	22	20	20	-	-	24	20	20	20	20	20	20	20	20	20	20	-	-	-	20	20
56	Doppler speed ref width:	150	120	120	120	100	100	-	-	120	100	100	100	100	100	100	100	100	100	100	-	-	-	100	100
57	Doppler speed minimum signal gate:	7	7	5	5	5	5	-	-	5	5	5	5	5	5	4	4	4	5	5	-	-	-	5	4
58	Doppler speed gate search range:	200	150	150	150	150	150	-	-	150	150	100	100	100	100	150	150	150	150	150	-	-	-	150	150
59	Doppler speed gate alpha filter:	0,15	0,2	0,2	0,2	0,25	0,25	0,8	0,8	0,2	0,25	0,25	0,25	0,25	0,25	0,2	0,2	0,2	0,25	0,25	0,8	0,8	0,8	0,2	0,2
60	Doppler speed gate beta filter:	0,02	0,02	0,02	0,02	0,03	0,03	0,05	0,05	0,02	0,03	0,03	0,03	0,03	0,03	0,02	0,02	0,02	0,03	0,03	0,05	0,05	0,05	0,02	0,02
61	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4	4
62	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1620	1800	1800	1800	1800
63	PID proportional term:	0,003	0,004	0,0025	0,0025	0,001	0,001	0,0055	0,0025	0,0035	0,0025	0,0015	0,0015	0,004	0,004	0,0025	0,0025	0,0105	0,0025	0,0025	0,04	0,007	0,0012	0,002	0,0025
64	PID integral term:	0,0436	0,0426	0,029	0,029	0,0226	0,0226	0,0631	0,0491	0,0346	0,0236	0,0216	0,0216	0,0301	0,0301	0,029	0,029	0,029	0,0266	0,0266	0,02	0,0451	0,034	0,0256	0,029
65	PID integral term limit:	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	0,8	1	1	1	1
66	PID derivative term:	0,0011	0,0011	0,0008	0,0008	0,0007	0,0007	0,0012	0,0006	0,001	0,0006	0,00011	0,00011	0,0012	0,0012	0,0008	0,0008	0,0017	0,0011	0,0011	0,002	0,0011	0,0012	0,0012	0,0008
67	Flight characteristics
68	Maximum fin angle of attack: [degrees]	15,3	14,4	20,7	20,7	27	27	15,3	9,9	19,8	25,2	28,8	28,8	28,8	28,8	20,7	20,7	20,7	20,7	20,7	14,4	16,2	15,3	22,5	20,7
69	Maximum fin lateral acceleration:	15	13	23,3	23,3	29	29	10,4	10,7	15,9	21,9	36,96	36,96	36,96	36,96	23,3	23,3	23,3	23,3	23,3	-	15,5	21	36,8	23,3
70	Wing area multiplier:	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,35	1,35	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4
71	Start speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
72	Maximum speed: [m/s]	1500	1500	1500	1500	1500	1500	1000	1000	1000	1500	1500	1500	1750	1750	1500	1500	1500	1500	1500	-	-	-	-	1500
73	Maximum statcard (useless) speed: [Mach]	3	4	4	4	4	4	2,5	1,7	3	3,5	3,5	3,5	5,75	5,75	4	4	4,4	5	5	1,8	2,7	4,5	5	4
74	Maximum statcard (useless) launch range: [km]	25	45	50	50	100	100	18	9	27	50	55	55	100	100	50	50	50	80	80	8	18	40	40	50
75	Minimum range: [m]	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30	30
76	Maximum (flight) range: [km]	26	45	50	50	70	70	18	11	27	45	55	55	67,5	67,5	50	50	50	80	80	18	18	40	40	50
77	Maximum G-load: [G]	15	15	25	25	25	25	18	11	20	24	35	35	35	35	25	25	25	25	25	15	15	20	30	25
78	Maximum statcard (useless) G-load: [G]	15	15	25	25	25	25	18	10	20	24	35	35	35	35	25	25	25	25	25	12	15	20	30	25
79	Flight time until guidance starts (delay): [s]	2	1,8	1,8	0,7	-	-	0,5	0,5	1,7	0,5	0,35	0,35	0,35	0,35	1,8	0,7	0,7	0,5	0,5	1,5	0,5	0,5	0,5	0,7
80	Flight time when pull limit reaches 40%: [s]	2,5	2,5	2,5	-	-	-	-	-	2,5	-	-	-	-	-	2,5	-	-	-	-	-	-	-	-	-
81	Flight time when pull limit reaches 100%: [s]	4,5	4,5	4,5	-	1	1	-	-	5	1	0,4	0,4	0,4	0,4	4,5	-	-	-	-	2	2,5	1,5	0,7	-
82	ETA to impact when prop multiplier reaches 30%: [s]	-	-	-	-	50	50	-	-	-	45	60	60	60	60	-	-	-	-	-	-	-	-	40/0,05	-
83	ETA to impact when prop multiplier reaches 50%: [s]	-	-	-	-	25	25	-	-	-	25	25	25	25	25	-	-	-	-	-	-	-	-	25/0,1	-
84	ETA to impact when prop multiplier reaches 80%: [s]	-	-	-	-	12	12	-	-	-	12	12	12	12	12	-	-	-	-	-	-	-	-	15/0,15	-
85	ETA to impact when prop multiplier reaches 90%: [s]	-	-	-	-	8	8	-	-	-	8	8	8	8	8	-	-	-	-	-	-	-	-	8/0,7	-
86	ETA to impact when prop multiplier reaches 100%: [s]	-	-	-	-	5	5	-	-	-	5	5	5	5	5	-	-	-	-	-	-	-	-	5/1	-
87	Additional Notes:						Identical to the AIM-7F Image found under artist Atamonica				Can use inertial navigation if radar lock is broken, Internal navigation drift speed is 5.	Can use inertial navigation with data link, Internal navigation drift speed is 10. Can reconnect datalink if connection is broken.	Can use inertial navigation with data link, Internal navigation drift speed is 10. Can reconnect datalink if connection is broken.	Can use inertial navigation with data link, Internal navigation drift speed is 10. Can reconnect datalink if connection is broken.	Can use inertial navigation with data link, Internal navigation drift speed is 10. Can reconnect datalink if connection is broken.					Chinese Aspide-1A				Same ETA table just the percantages arent the usual, shows time/prop multiplier multiplier	Swedish Skyflash
88													Export version of R, no changes
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1	Name:	AIM-54A	AIM-54B	AIM-54C	AIM-120A	AIM-120B	AIM-120C-5	R-77	R-77-1	PL-12	MICA-EM	R-DARTER	DERBY	AAM-4	RB99

2	Physical properties
3	Mass: [kg]	443,613	443,613	463	147,87	147,87	157	177	190	198	112	118	118	222	147,87
4	Mass at end of booster burn: [kg]	273,063	273,063	293	131,75	131,75	105,7441	117	160	160	88,3	92,94	92,94	155	131,75
5	Mass at end of sustainer burn: [kg]	-	-	-	101,33	101,33	-	-	120	132	70,1	74,75	74,75	-	101,33
6	Calibre: [mm]	380	380	380	177,8	177,8	177,8	200	200	203	165	160	160	203	177,8
7	Length: [m]	3,96	3,96	3,96	3,66	3,66	3,66	3,6	3,71	3,93	3,1	3,62	3,62	3,667	3,66
8	Engine properties
9	Force exerted by booster: [N]	14350	14350	14350	21800	21800	15542	23000	34500	34960	20250	21500	21500	20100	21800
10	Burn time of booster: [s]	30	30	30	1,7	1,7	7,75	6	2	2,5	2,75	2,74	2,74	7,5	1,7
11	Raw acceleration at ignition: [m/s²]	32,35	32,35	30,99	147,43	147,43	98,99	129,94	181,58	176,57	180,80	182,20	182,20	90,54	147,43
12	Specific impulse of booster: [s]	257,31	257,31	258,14	234,35	234,35	239,55	234,45	234,45	234,45	239,52	239,63	239,63	229,36	234,35
13	ΔV of booster: [m/s]	1224,86	1224,86	1158,69	265,37	265,37	928,77	952,14	395,26	490,11	558,66	561,20	561,20	808,32	265,37
14	Booster start delay: [s]	-	-	-	0	0	0	-	0	0	0	0	0	-	0
15	Force exerted by sustainer: [N]	-	-	-	13200,00	13200	-	-	18400	12880	10720	11280	11280	-	13200,00
16	Burn time of sustainer: [s]	-	-	-	5,30	5,30	-	-	5	5	4	3,79	3,79	-	5,30
17	Specific impulse of sustainer: [s]	-	-	-	234,43	234,43	-	-	234,4546381	234,45	240,17	239,58	239,58	-	234,43
18	ΔV of sustainer: [m/s]	-	-	-	603,75	603,75	-	-	661,6687666	442,46	543,82	511,90	511,90	-	603,75
19	Total ΔV: [m/s]	1224,86	1224,86	1158,69	869,12	869,12	928,77	952,14	1056,92	932,57	1102,47	1073,10	1073,10	808,32	869,12
20	Fuse and warhead properties
21	Explosive mass: [kg of TNT equivalent]	60,544	60,544	54,640128	9,81211008	9,81211008	11,031424	15,56	15,56	11,776	4,736	8	8	16,1792	9,81211008
22	Proximity fuse:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
23	Proximity fuse range: [m]	20	20	20	12	12	12	10	10	10	12	12	12	12	12
24	Proximity fuse shell detection (80-200 mm):	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
25	Proximity fuse delay: [s]	5	5	5	1,8	1,8	1,8	1,7	1,7	1,7	1,8	1,8	1,8	1,8	1,8
26	Guidance properties
27	Guidance type:	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL	ARH + IOG + DL
28	Guidance start delay: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-
29	Guidance duration: [s]	160	160	160	80	80	120	90	120	80	70	90	90	80	80
30	Seeker warm up time: [s]	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4	1,4
31	Seeker search duration: [s]	200	200	200	100	100	100	100	100	100	100	100	100	100	100
32	Gimbal limit: [degrees]	60	60	60	55	55	55	55	55	60	55	55	55	55	55
33	Track rate: [degrees/second]	20	20	20	60	60	60	60	60	60	60	60	60	60	60
34	Uncaged seeker before launch:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
35	Maximum lock angle before launch: [degrees]	60	60	60	55	55	55	55	55	60	55	55	55	55	55
36	Lock-on range from all-aspect: [km]	16	16	16	16	16	16	16	16	16	16	16	16	16	16
37	Maximum break lock time: [s]	160	160	160	160	160	160	160	160	160	160	160	160	160	160
38	Can lock after launch:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
39	Band:	I	I	I	I	I	I	I	I	I	I	I	I	I	I
40	Angular speed rejection threshold: [degrees/second]	30	30	-	-	-	-	-	-	-	-	-	-	-	-
41	Acceleration rejection threshold range: [m/s^2]	100-250	100-250	100-250	-	-	-	-	-	-	-	-	-	-	-
42	Sidelobe attenuation:	-20	-20	-20	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30
43	Transmitter power:	100	100	100	100	100	100	100	100	100	100	100	100	100	100
44	Transmitter angle of half sensitivity:	8	9	9	15	15	7,5	15	15	15	15	15	15	15	15
45	Transmitter sidelobe sensitivity:	-19	-19	-19	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30
46	Receiver angle of half sensitivity:	9	9	8	15	15	7,5	15	15	15	15	15	15	15	15
47	Receiver sidelobe sensitivity:	-19	-19	-19	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30	-30
48	Distance minimum value: [m]	-	-	-	300	300	300	300	300	300	300	300	300	300	300
49	Distance maximum value: [km]	-	-	-	150	150	150	150	150	150	150	150	150	150	150
50	Distance minimum signal gate: [m]	-	-	-	300	300	300	300	300	300	300	300	300	300	300
51	Distance ref width: [m]	-	-	-	300	300	300	300	300	300	300	300	300	300	300
52	Distance gate search range: [m]	-	-	-	5000	5000	5000	5000	5000	5000	5000	5000	5000	5000	5000
53	Distance gate alpha filter:				0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8
54	Distance gate beta filter:				0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05
55	Doppler speed minimum value:	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000	-3000
56	Doppler speed maximum value:	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000	3000
57	Doppler speed width:	20	20	20	20	20	20	20	20	20	20	20	20	20	20
58	Doppler speed ref width:	80	80	80	80	80	60	80	80	80	80	80	80	80	80
59	Doppler speed minimum signal gate:	5	5	5	5	5	5	5	5	5	5	5	5	5	5
60	Doppler speed gate search range:	300	300	300	300	300	300	300	300	300	300	300	300	300	300
61	Doppler speed gate alpha filter:	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8	0,8
62	Doppler speed gate beta filter:	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05	0,05
63	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4	4	4	4	4	4	4	4	4	4
64	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800
65	PID proportional term:	0,0221	0,0221	0,0221	0,0061	0,0061	0,0011	0,0116	0,0021	0,0071	0,0036	0,0035	0,0035	0,0191	0,0061
66	PID integral term:	0,0981	0,0981	0,0981	0,0475	0,0475	0,0291	0,0116	0,0376	0,047	0,032	0,0221	0,0221	0,0075	0,0475
67	PID integral term limit:	1	1	1	1	1	1	1	1	1	1	1	1	1	1
68	PID derivative term:	0,0045	0,0045	0,0045	0,00015	0,00015	0,0006	0,00015	0,00045	0,00015	0,00005	0,0007	0,0007	0,00045	0,00015
69	Inertial guidance drift speed:	10	10	2	2	2	2	2	2	2	2	2	2	2	2
70	Flight characteristics
71	Maximum fin angle of attack: [degrees]	19,58544	19,58544	19,58544	33,24528	33,24528	30,0429	36,19359	36,19359	32,44779	30,11427	40,0149	40,0149	33,94413	33,24528
72	Maximum fin lateral acceleration:	21,14	21,14	21,14	40,1903	40,1903	46,8191	54,7619	54,7619	38,912	55,3663	41,34	41,34	33,9305	40,1903
73	Wing area multiplier:	1,2	1,2	1,2	1,3	1,3	1,275	1,3	1,3	1,4	1,4	1,45	1,45	1,275	1,3
74	Start speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-
75	Maximum speed: [m/s]	1800	1800	1800	1500	1500	1500	1500	1500	1500	1500	1500	1500	1500	1500
76	Maximum statcard (useless) speed: [Mach]	4,3	4,3	4,3	4	4	4	4	4	4	4	4	4	4	4
77	Maximum statcard (useless) launch range: [km]	150	150	150	80	80	80	80	120	80	50	80	80	100	80
78	Minimum range: [m]	30	30	30	30	30	30	30	30	30	30	30	30	30	30
79	Maximum (flight) range: [km]	150	150	150	80	80	80	80	120	80	50	80	80	100	80
80	Maximum G-load: [G]	17	17	17	35	35	35	50	50	40	50	40	40	32	35
81	Maximum statcard (useless) G-load: [G]	17	17	17	35	35	35	50	50	38	50	40	40	32	35
82	Flight time until guidance starts (delay): [s]	2,5	2,5	2,5	0,3	0,3	0,3	0,3	0,3	0,3	0,3	0,3	0,3	0,3	0,3
83	Flight time when pull limit reaches 40%: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-
84	Flight time when pull limit reaches 100%: [s]	3,5	3,5	3,5	0,31	0,31	0,31	0,31	0,31	0,31	0,16	0,31	0,31	0,31	0,31
85	Loft:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
86	Loft angle: [degrees]	17,5	17,5	17,5	7,5	7,5	25	5	5	5	5	30	30	7,5	7,5
87	Target elevation: [degrees]	-7,75	-7,75	-7,75	-5	-5	-15	-5	-5	-5	-5	-20	-20	-5	-5
88	Maximum target angular change: [degrees/s]	0,25	0,25	0,25	0,5	0,5	0,75	0,5	0,5	2,5	2,5	2,5	2,5	0,5	0,5
89	Thrust vectoring:	No	No	No	No	No	No	No	No	No	Yes	No	No	No	No
90	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	0,025	-	-	-	-
91	ETA to impact when prop multiplier reaches x%: [s]	-	-	-	80/10	80/11	80/10	80/10	80/10	80/10	-	80/10	80/10	80/10	80/10
92	ETA to impact when prop multiplier reaches x%: [s]	-	-	-	60/20	60/21	60/20	60/20	60/20	60/20	-	60/20	60/20	60/20	60/20
93	ETA to impact when prop multiplier reaches x%: [s]	-	-	-	50/50	50/51	50/50	50/50	50/50	50/50	-	50/50	50/50	50/50	50/50
94	ETA to impact when prop multiplier reaches x%: [s]	-	-	-	25/80	25/81	25/80	25/80	25/80	25/80	-	25/80	25/80	25/80	25/80
95	ETA to impact when prop multiplier reaches x%: [s]	-	-	-	10/100	10/101	10/100	10/100	10/100	10/100	-	10/100	10/100	10/100	10/100
96	Additional Notes:			Image found under artist Atamonica		Same as A		Image found under artist Atamonica	Image found under artist Atamonica				Same as R-DARTER		Swedish AIM120
97			Copy-paste AIM-54A
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1	Name:	Fireflash	Starstreak	Starstreak (dart)	AA.20

2	Physical properties
3	Mass: [kg]	150	14	0,9	133
4	Mass at end of booster burn: [kg]	120	13	-	108
5	Mass at end of sustainer burn: [kg]	-	7,5	-	97
6	Calibre: [mm]	140	130	20	250
7	Length: [m]	2,286	1,08	0,68	3,12
8	Engine properties
9	Force exerted by booster: [N]	42000	0	-	28000
10	Burn time of booster: [s]	1,5	0	-	1,8
11	Raw acceleration at ignition: [m/s²]	280,00	0,00	-	210,53
12	Specific impulse of booster: [s]	214,07	0,00	-	205,50
13	ΔV of booster: [m/s]	468,60	0,00	-	419,77
14	Force exerted by sustainer: [N]	-	20000	-	1480
15	Burn time of sustainer: [s]	-	0,58	-	14,5
16	Specific impulse of sustainer: [s]	-	214,99	-	198,87
17	ΔV of sustainer: [m/s]	-	1160,10	-	209,57
18	Total ΔV: [m/s]	468,60	1160,10	-	629,33
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	7	1,572	0,524	10,48
21	Proximity fuse:	Yes	No	No	Yes
22	Proximity fuse range: [m]	10	-	-	15
23	Proximity fuse shell detection (80-200 mm):	Yes	-	-	Yes
24	Proximity fuse delay: [s]	0,5	-	-	0,5
25	Guidance properties
26	Guidance type:	LOSBR	LOSBR	LOSBR	MCLOS
27	Guidance duration: [s]	30	12	12	30
28	Maximum angle allowed between the missile and the crosshair: [degrees]	5	-	-	-
29	Flight characteristics
30	Aim sensitivity:	-	-	-	22,1
31	Maximum axis values:	-	0.01	1,075	1
32	Wing area multiplier:	1,25	-	1,25	1,2
33	Start speed: [m/s]	-	10	1125	-
34	Maximum speed: [m/s]	1500	1125	1125	-
35	Maximum statcard (useless) speed: [m/s] or [Mach]	2	-	-	1,7
36	Maximum statcard (useless) launch range: [km]	4	-	-	-
37	Minimum range: [m]	600	30	30	30
38	Maximum (flight) range: [km]	12	7	9,8	10
39	Maximum G-load: [G]	10	-	47	-
40	Maximum statcard (useless) G-load: [G]	10	47	47	12
41	Thrust vectoring:	No	No	No	No
42	Thrust vectoring angle: [degrees]	-	-	-	-
43	Additional Notes:
44
45
46
47
48
49
50
51
52
53


1	Name:	AGM-65A	AGM-65B	AGM-65D	AGM-65G	AGM-65H	PARS 3 LR	Flz.Lwf. LB 82	PGM-500	PGM-2000	AJ-168	Kh-29T	Kh-29TD	Kh-29TE	Kh-38MT	Rb 75	Rb 75T	UMTAS	SPIKE-ER

2	Physical properties
3	Mass: [kg]	210,467	210,467	226,796	303,453	226,796	49	210,467	404	1060	550	670	686	690	520	210,467	226,796	37,5	34
4	Mass at end of booster burn: [kg]	198,182	198,182	214,511	291,168	214,511	43	198,182	384,5	1021	507	559,2	575,2	579,2	470	198,182	214,511	34,5	31,25
5	Mass at end of sustainer burn: [kg]	180,9835	180,9835	197,3125	273,97	197,3125	41,5	180,9835	-	-	397	-	-	-	350	180,9835	197,3125	30,8	28,25
6	Calibre: [mm]	304,8	304,8	304,8	304,8	304,8	159	304,8	360	457	400	380	380	380	310	304,8	304,8	160	170
7	Length: [m]	2,48158	2,48158	2,48158	2,48158	2,48158	1,6	2,48158	3,38	4,623	3,89	3,875	3,875	3,875	4,2	2,48158	2,48158	1,8	1,65
8	Engine properties
9	Force exerted by booster: [N]	44497	44497	44497	44497	44497	4600	44497	1600	3200	17200	50800	50800	50800	57500	44497	44497	2550	3500
10	Burn time of booster: [s]	0,5	0,5	0,5	0,5	0,5	3	0,5	25	25	5	4,5	4,5	4,5	2	0,5	0,5	2,5	3
11	Raw acceleration at ignition: [m/s²]	211,42	211,42	196,20	146,64	196,20	93,88	211,42	3,96	3,02	31,27	75,82	74,05	73,62	110,58	211,42	196,20	68,00	102,94
12	Specific impulse of booster: [s]	184,61	184,61	184,61	184,61	184,61	234,45	184,61	209,10	209,10	203,87	210,31	210,31	210,31	234,45	184,61	184,61	216,62	389,21
13	ΔV of booster: [m/s]	108,92	108,92	100,86	74,84	100,86	300,43	108,92	101,48	76,90	162,81	372,96	363,45	361,15	232,52	108,92	100,86	177,19	322,03
14	Force exerted by sustainer: [N]	8899	8899	8899	8899	8899	560	8899	-	-	2000	-	-	-	25875	8899	8899	200	210
15	Burn time of sustainer: [s]	3,5	3,5	3,5	3,5	3,5	6	3,5	-	-	110	-	-	-	8	3,5	3,5	40	6
16	Specific impulse of sustainer: [s]	184,62	184,62	184,62	184,62	184,62	228,34	184,62	-	-	203,87	-	-	-	175,84	184,62	184,62	220,40	42,81
17	ΔV of sustainer: [m/s]	164,41	164,41	151,36	110,27	151,36	79,53	164,41	-	-	489,15	-	-	-	508,53	164,41	151,36	245,29	42,39
18	Total ΔV: [m/s]	273,33	273,33	252,21	185,11	252,21	379,96	273,33	101,48	76,90	651,96	372,96	363,45	361,15	741,05	273,33	252,21	422,47	364,42
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	51,1948	51,1948	51,1948	46,447872	51,1948	3,696	51,1948	117,585	505,748	88,5	186,24	186,24	186,24	152	51,1948	51,1948	6,8775	3,3135
21	Tandem charge:	No	No	No	No	No	Yes	No	No	No	No	No	No	No	No	No	No	Yes	Yes
22	Penetration: [mm]	830	830	830	122	830	1000	830	82	111	830	103	103	103	84	830	830	1100	1000
23	Proximity fuse:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
24	Proximity fuse range: [m]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
25	Proximity fuse delay: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
26	Guidance properties
27	Zoom:	14.74x	29.46x	2.48x - 4.92x	2.48x - 4.92x	14.74x	-	29.46x	6.5x/14.74x	6.5x/14.74x	29.46x	6.15x - 25.4x	6.15x - 25.4x	6.15x - 25.4x	6.15x - 25.4x	14.74x	2.48x - 4.92x	-	-
28	Guidance type:	Optical/TV	Optical/TV	IR	IR	Optical/TV	IR	Optical/TV	Optical/TV	Optical/TV	Optical/TV	Optical/TV	Optical/TV	Optical/TV	IR+IOG	Optical/TV	IR	IR	IR
29	Guidance start delay: [s]	0,5	0,5	0,5	0,5	0,5	0,5	0,5	0,75	0,75	0,5	0,8	0,8	0,8	0,8	0,5	0,5	-	0,2
30	Guidance duration: [s]	105	105	105	105	105	30	105	200	200	175	40	70	70	70	105	105	50	60
31	Seeker warm up time: [s]	1	1	1	1	1	1	1	1	1	1	0,01	0,01	0,01	0,01	1	1	1	1
32	Seeker search duration: [s]	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600	3600
33	Field of view: [degrees]	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,25	0,1
34	Gimbal limit: [degrees]	50	50	54	54	54	45	50	45	45	60	58	58	58	60	50	54	45	60
35	Track rate: [degrees/second]	5	2,5	2,5	2,5	2,5	6	2,5	10	10	5	7	7	7	7	5	2,5	6	10
36	Uncaged seeker before launch:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
37	Maximum lock angle before launch: [degrees]	30	30	30	30	30	45	30	40	40	30	55	55	55	55	30	30	45	30
38	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	-	-	1	1	1	1	-	-	-	-	-	-	-	-	-	1	-	1
39	Can lock the ground:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
40	Lock-on range (ground): [km]	24	24	24	24	24	10	24	25	25	34	35	35	30	40	24	24	10	10
41	Lock-on range from rear-aspect: [km]	-	-	20	20	-	20	-	-	-	-	-	-	-	20	-	20	20	20
42	Lock-on range from all-aspect: [km]	6	12	20	20	12	20	12	12	12	12	12	12	12	20	6	20	20	20
43	Can lock after launch:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
44	Inertial guidance drift speed:	-	-	-	-	-	-	-	-	-	-	-	-	-	1,25	-	-	-	-
45	Flight characteristics
46	Maximum fin angle of attack: [degrees]	18	18	9	9	9	18	18	9, 13.5 [H, V]	9, 13.5 [H, V]	18	16,2	16,2	16,2	18	18	9	18	18
47	Maximum fin lateral acceleration:	7,5	7,5	-	-	-	-	7,5	-	-	4,5	-	-	-	-	7,5	-	-	-
48	Wing area multiplier:	1,515	1,515	1,3	1,3	1,3	1,5	1,515	1,65	1,65	1,5	1,35	1,35	1,35	1,3	1,515	1,3	1,35	1,95
49	Start speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	0	130
50	Maximum speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	530	-	-	-	-
51	Maximum statcard (useless) speed: [Mach]	0,9	0,9	0,9	0,9	0,9	0,9	0,9	1	1	0,9	1,75	1,75	1,75	2,2	0,9	0,9	180	-
52	Maximum statcard (useless) launch range: [km]	23	23	23	23	23	7	23	50	50	45	13	35	30	40	23	23	-	8
53	Minimum range: [m]	600	600	600	600	600	30	600	2000	2000	3000	3000	3000	3000	3000	600	600	600	30
54	Maximum (flight) range: [km]	26,4	26,4	26,4	26,4	26,4	7	26,4	50	50	60	13	35	30	40	26,4	26,4	8	8
55	Load factor limit at launch: [G]	7	7	-	-	-	-	7	-	-	7	7	7	7	-	7	-	-	-
56	Maximum G-load: [G]	6	6	6	6	6	6	6	2,5	2,5	6	6	6	6	6	6	6	6	4
57	Maximum statcard (useless) G-load: [G]	5	5	5	5	5	6	5	2,5	2,5	5	6	6	6	6	5	5	-	4
58	Thrust vectoring:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
59	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
60	Loft:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
61	Loft angle: [degrees]	16	16	20	20	20	10	16	7	7	2	27	27	27	10	16	20	8	20
62	Target elevation: [degrees]	-6,75	-6,75	-6,75	-6,75	-6,75	-25	-6,75	-20,00	-20,00	-6,75	-35	-35	-35	-35	-6,75	-6,75	-10	-40
63	Maximum target angular change: [degrees/s]	0,425	0,425	0,425	0,425	0,425	0,85	0,425	0,35	0,35	0,425	0,45	0,45	0,45	1,5	0,425	0,425	0,75	1,45
64	Additional Notes:							Swiss copy of the AGM-65B								Swedish copy of the AGM-65A.	Swedish copy of the AGM-65D.
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1	Name:	AGM-114A	AGM-114B	AGM-114C	AGM-114F	AGM-114K	AGM-123	APKWS- M151	APKWS- M281	Kh-25	Kh-25ML	Kh-29L	Kh-38ML	S-25L	S-25LD	ZT-6 Mokopa	AKD9	AKD10	BA-7	BA-9	AS.30L	CIRIT	L-UMTAS	GATR

2	Physical properties
3	Mass: [kg]	45,132	45,132	45,132	45,132	45,132	580	15,8	15,8	318	297	657	520	410	410	49,8	26,5	46	46	26,5	520	15	37,5	16,4
4	Mass at end of booster burn: [kg]	36,861	36,861	36,861	36,861	36,861	560,9	12,62	12,62	255,5	266	546,2	470	320	320	38,3	23,5	43,5	43,5	23,5	463	11,82	34,5	13,22
5	Mass at end of sustainer burn: [kg]	-	-	-	-	-	537,7	-	-	-	214,5	-	350	-	-	-	21	35	35	21	393	-	30,8	-
6	Calibre: [mm]	178	178	178	178	178	355,6	70	70	275	275	380	310	340	340	178	140	170	170	140	342	70	160	70
7	Length: [m]	1,63	1,63	1,63	1,63	1,63	4,27	1,905	1,905	3,83	3,75	3,875	4,2	4,038	4,038	1,995	1,56	1,78	1,78	1,56	3,885	1,9	1,8	1,84
8	Engine properties
9	Force exerted by booster: [N]	6830	6830	6830	6830	6830	32088	6064	6064	24700	32550	50800	57500	83000	83000	10120	6000	5500	5500	6000	58425	6064	2550	6064
10	Burn time of booster: [s]	3	3	3	3	3	1,25	1,1	1,1	4,9	2	4,5	2	2,35	2,35	2,5	1	1	1	1	2	1,1	2,5	1,1
11	Raw acceleration at ignition: [m/s²]	151,33	151,33	151,33	151,33	151,33	55,32	383,80	383,80	77,67	109,60	77,32	110,58	202,44	202,44	203,21	226,42	119,57	119,57	226,42	112,36	404,27	68,00	369,76
12	Specific impulse of booster: [s]	252,53	252,53	252,53	252,53	252,53	214,07	213,82	213,82	197,40	214,07	210,31	234,45	220,92	220,92	224,26	203,87	224,26	224,26	203,87	208,97	213,82	216,62	213,82
13	ΔV of booster: [m/s]	501,50	501,50	501,50	501,50	501,50	70,32	471,39	471,39	423,76	231,50	381,07	232,52	537,12	537,12	577,64	240,29	122,94	122,94	240,29	238,01	499,77	177,19	452,14
14	Force exerted by sustainer: [N]	-	-	-	-	-	2436	-	-	-	17300	-	25875	-	-	-	625	813	813	625	6525	-	200	-
15	Burn time of sustainer: [s]	-	-	-	-	-	20	-	-	-	6,25	-	8	-	-	-	8	23	23	8	22	-	40	-
16	Specific impulse of sustainer: [s]	-	-	-	-	-	214,07	-	-	-	214,02	-	175,84	-	-	-	203,87	224,25	224,25	203,87	209,04	-	220,40	-
17	ΔV of sustainer: [m/s]	-	-	-	-	-	88,71	-	-	-	451,79	-	508,53	-	-	-	224,96	478,28	478,28	224,96	336,15	-	245,29	-
18	Total ΔV: [m/s]	501,50	501,50	501,50	501,50	501,50	159,03	471,39	471,39	423,76	683,28	381,07	741,05	537,12	537,12	577,64	465,24	601,22	601,22	465,24	574,16	499,77	422,47	452,14
19	Warhead explosive mass
20	Explosive mass: [kg of TNT equivalent]	8,02008	8,02008	8,02008	8,02008	8,02008	8,02008	1,36	0,568	119,04	119,04	186,24	152	20	20	6,252	2,46	6,252	6,252	2,46	99,56	1,4014	6,8775	0,568
21	Tandem charge:	No	No	No	Yes	Yes	Yes	No	No	No	No	No	No	No	No	Yes	Yes	Yes	Yes	Yes	No	No	Yes	No
22	Penetration: [mm]	1100	1100	1100	1200	1200	1200	18	41	100	100	103	84	74	74	1350	800	1400	1400	800	99	290	1100	41
23	Proximity fuse:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
24	Proximity fuse range: [m]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
25	Proximity fuse delay: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
26	Guidance properties
27	Guidance type:	Laser + IOG	Laser + IOG	Laser + IOG	Laser + IOG	Laser + IOG	Laser	Laser	Laser	Laser	Laser	Laser	Laser + IOG	Laser	Laser	Laser + IOG	Laser + IOG	Laser + IOG	Laser + IOG	Laser + IOG	Laser+IOG	Laser	Laser + IOG	Laser
28	Guidance start delay: [s]	-	-	-	-	-	1	-	-	0,8	0,5	0,8	0,8	0,8	0,8	-	-	-	-	-	0,8	0,75	-	-
29	Guidance duration: [s]	45	45	45	45	45	70	30	30	25	45	40	90	18	27	50	25	36	36	25	24	45	50	45
30	Guidance range: [km]	12	12	12	12	12	3,657	5	5	-	-	-	-	-	-	10	6	10	10	6	-	10	8	8
31	Seeker warm up time: [s]	-	-	-	-	-	-	-	-	1	1	1	1	1	1	-	-	-	-	-	1	-	-	-
32	Seeker search duration: [s]	-	-	-	-	-	-	-	-	3600	3600	3600	3600	3600	3600	-	-	-	-	-	3600	-	-	-
33	Field of view: [degrees]	30	30	30	30	30	20	40	40	1	30	30	50	30	30	30	30	30	30	30	30	30	30	40
34	Gimbal limit: [degrees]	45	45	45	45	45	0	0	0	30	30	30	50	30	30	45	45	45	45	45	30	0	45	0
35	Track rate: [degrees/second]	8	8	8	8	8	10000	10000	10000	10	8	8	8	8	8	8	8	8	8	8	8	10000	8	10000
36	Uncaged seeker before launch:	No	No	No	No	No	No	No	No	Yes	No	No	No	Yes	Yes	No	No	No	No	No	Yes	No	No	No
37	Maximum lock angle before launch: [degrees]	-	-	-	-	-	-	-	-	30	-	-	-	30	30	-	-	-	-	-	30	-	-	0
38	Maximum break lock time: [s]	30	30	30	30	30	70	30	30	5	2	5	2	5	5	50	30	30	30	30	22	45	50	30
39	Inertial guidance drift speed:	3,5	3,5	3,5	3,5	3,5	-	-	-	-	-	-	1,25	-	-	3,5	3,5	3,5	3,5	3,5	2	-	3,5	-
40	Flight characteristics
41	Maximum launch angle (horizontally / vertically): [degrees]	20 / 40	20 / 40	20 / 40	20 / 40	20 / 40	-	-	-	-	12.5 / 30	12.5 / 30	-	12.5 / 30	12.5 / 30	20 / 40	20 / 40	20 / 40	20 / 40	20 / 40	30 / 30	-	20 / 40	-
42	Maximum fin angle of attack: [degrees]	13,5	13,5	13,5	13,5	13,5	13,5	4,5	4,5	13,5	13,5	16,2	18	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	4,5	18	4,5
43	Wing area multiplier:	1,125	1,125	1,125	1,125	1,125	1,35	1,05	1,05	1,15	1,15	1,35	1,3	1,2	1,2	1,11	1,15	1,1	1,1	1,15	-	1,05	1,5	1,05
44	Start speed: [m/s]	-	-	-	-	-	0	-	-	-	-	-	-	-	-	-	-	-	-	-	-	0	-	-
45	Maximum speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	530	-	-	-	-	-	-	-	-	-	-	-
46	Maximum statcard (useless) speed: [m/s] or [Mach]	475	475	475	475	475	410	455	455	2	2	1,75	2,2	510	510	530	340	345	345	340	370	480	180	455
47	Maximum statcard (useless) launch range: [km]	-	-	-	-	-	20	-	-	7	10	8	40	10	12	-	-	-	-	-	-	-	-	-
48	Minimum range: [m]	30	30	30	30	30	3000	2000	2000	500	500	3000	3000	2000	2000	1000	30	30	30	30	30	1500	600	2000
49	Maximum (flight) range: [km]	8	8	8	8	8	20	11	11	10	10	10	40	10	12	10	6	10	10	6	12	10	8	10
50	Load factor limit at launch: [G]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
51	Maximum G-load: [G]	6	6	6	6	6	4	2	2	8	8	6	15	6	6	6	6	6	6	6	6	2	2,5	4
52	Maximum statcard (useless) G-load: [G]	-	-	-	-	-	4	-	-	8	8	6	6	2	2	-	-	-	-	-	-	-	-	-
53	Thrust vectoring:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
54	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
55	Loft:	Yes	Yes	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	Yes	Yes	Yes	No	Yes	No
56	Loft angle: [degrees]	9,6	9,6	9,6	9,6	9,6	5	-	-	27	27	27	10	-	-	9,6	8	8	8	8	15	-	10	-
57	Target elevation: [degrees]	-15	-15	-15	-15	-15	-3,75	-	-	-35	-35	-35	-35	-	-	-15	-15	-15	-15	-15	-10	-	-15	-
58	Maximum target angular change: [degrees/s]	0,85	0,85	0,85	0,85	0,85	0,725	-	-	0,85	0,85	0,45	1,5	0,75	0,75	0,85	2	2	2	2	1,5	-	0,75	-
59	Additional Notes:								SAP-HE rocket, penetration falls with speed															SAP-HE rocket, penetration falls with speed
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1	Name:	AGM-12B (Heli)	AGM-22	ITOW	TOW-2	9M14-2 Malyutka	9M14M Malyutka	9M17 Fleyta	9M17M Fleyta	9M17P Fleyta	9M114 Kokon	9M120 Ataka	9M120-1 Ataka	Kh-66	HJ-8A	HJ-8C	HJ-8E	HJ-8H	HJ-8L	HJ-9	AS.11	AS.12	HOT-1	HOT-2	HOT-3	Rb 52	Rb 53	Rb 55B	Rb 55C

2	Physical properties
3	Mass: [kg]	259	29,99	19,05	21,45	13,5	13,5	28,5	31,5	31,5	31,4	33,5	33,5	278	11,2	11,4	12	13	13	29	29,99	76	23	23	23,6	29,99	7,6	19,05	21,45
4	Mass at end of booster burn: [kg]	204	28,35	16,55	18,25	11,6	11,6	20	28,09	28,09	25,83	27,93	27,93	214,55	10,05	10,25	10,85	11,85	11,85	25	28,35	68,8	20,04	20,04	20,64	28,35	7,25	16,55	18,25
5	Mass at end of sustainer burn: [kg]	-	24,45	-	-	9,6	9,6	-	27,1	27,1	21,58	23,68	23,68	-	8,75	8,95	9,55	10,55	10,55	23,5	24,45	61,1	17,44	17,44	18,04	24,45	6,74	-	-
6	Calibre: [mm]	298	164	127	152	125	125	135	142	142	130	130	130	275	120	120	120	120	120	152	164	210	136	150	150	164	110	127	152
7	Length: [m]	3,12	1,21	1,534	1,607	1,005	1,005	1,163	1,16	1,16	1,613	1,93	1,93	3,631	0,85	1,05	1,05	1,05	1,05	2,04	1,21	1,87	1,27	1,3	1,3	1,21	0,848	1,534	1,607
8	Engine properties
9	Force exerted by booster: [N]	53400	3280	2800	3590	1600	1600	3500	6933	6933	6480	6480	6480	24700	800	800	800	800	800	6450	3280	8200	4600	4600	4600	3280	1100	2800	3590
10	Burn time of booster: [s]	2,04	1	1,6	1,6	1	1	3	1	1	2	2	2	4,9	2	2	2	2	2	1	1	1,8	1,1	1,1	1	1	0,5	1,6	1,6
11	Raw acceleration at ignition: [m/s²]	206,18	109,37	146,98	167,37	118,52	118,52	122,81	220,10	220,10	206,37	193,43	193,43	88,85	71,43	70,18	66,67	61,54	61,54	222,41	109,37	107,89	200,00	200,00	194,92	109,37	144,74	146,98	167,37
12	Specific impulse of booster: [s]	201,90	203,87	182,67	182,98	85,84	85,84	125,92	207,25	207,25	237,18	237,18	237,18	194,44	141,83	141,83	141,83	141,83	141,83	164,37	203,87	208,97	174,26	174,26	158,42	203,87	160,19	182,67	182,98
13	ΔV of booster: [m/s]	472,80	112,47	252,10	290,00	127,73	127,73	437,51	232,94	232,94	454,35	423,11	423,11	494,19	150,74	147,95	140,16	128,86	128,86	239,33	112,47	204,04	235,50	235,50	208,27	112,47	74,09	252,10	290,00
14	Force exerted by sustainer: [N]	-	390	-	-	50	50	-	335	335	3070	3070	3070	-	205	205	255	255	255	390	390	525	265	265	265	390	42,5	-	-
15	Burn time of sustainer: [s]	-	20	-	-	27	27	-	6	6	3	3	3	-	13	13	17	17	17	11	20	30	17	17	18	20	24	-	-
16	Specific impulse of sustainer: [s]	-	203,87	-	-	68,81	68,81	-	206,96	206,96	220,90	220,90	220,90	-	208,97	208,97	339,92	339,92	339,92	291,54	203,87	208,51	176,63	176,63	187,01	203,87	203,87	-	-
17	ΔV of sustainer: [m/s]	-	295,99	-	-	127,74	127,74	-	72,85	72,85	389,57	357,72	357,72	-	283,96	278,03	425,58	387,49	387,49	176,96	295,99	242,78	240,78	240,78	247,01	295,99	145,88	-	-
18	Total ΔV: [m/s]	472,80	408,47	252,10	290,00	255,47	255,47	437,51	305,79	305,79	843,92	780,82	780,82	494,19	434,70	425,97	565,74	516,35	516,35	416,29	408,47	446,81	476,28	476,28	455,28	408,47	219,97	252,10	290,00
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	58,05	2,0043	2,8764	4,4133	3,25	3,25	7,2	4,32	4,32	3,9273	4,4838	4,4838	65,28	1,9565	2,015	2,015	2,795	2,795	6,16	2,0043	5,24	3,799	6,4554	6,4554	2,0043	1,4934	2,8764	4,4133
21	Tandem charge:	No	No	No	No	No	No	No	No	No	No	Yes	Yes	No	No	Yes	Yes	Yes	Yes	Yes	No	No	No	No	Yes	No	No	No	No
22	Penetration: [mm]	92	600	630	800	800	650	650	650	650	560	800	800	93	480	590	590	750	750	1200	600	1000	700	900	1250	600	500	630	800
23	Proximity fuse:	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No	No
24	Proximity fuse range: [m]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
25	Proximity fuse arming distance: [m]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
26	Proximity fuse shell detection (80-200 mm):	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
27	Proximity fuse minimum altitude: [m]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
28	Proximity fuse delay: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
29	Guidance properties
30	Guidance type:	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS
31	Guidance duration: [s]	30	21	25	25	30	30	-	37	37	20	25	25	25	15	15	19	19	19	24	21	32	20	20	20	21	25	25	25
32	Guidance range: [km]	11	3,5	3,75	3,75	3	3	2,5	4	4	5	6	6	10	3	3	4	4	4	6	3,5	7	4	4	4,3	3,5	2	3,75	3,75
33	Launch sector: [degrees]											9	9		10	10	10	10	10	10		10						10	10
34	Control cone FOV: [degrees]		30			30	30		30	30	25	25	25		25	25	25	25	25	25	30	30	25	25	25	30		25	25
35	Aim tracking sensitivity:	-	0,5	0,4	0,4	0,5	0,5	-	0,5	0,5	-	0,5	0,5	-							0,5	0,1	0,4	0,4	0,4	0,5	0,1	0,4	0,4
36	Flight characteristics
37	Maximum axis values:	1	0,25			0,25	0,25	-	0,5	0,5	0,75	0,75	0,75	1	-	-	-	-	-		0,25	0,5	0,5	0,5	0,5	0,25	0,25
38	Maximum fin AOA: [degrees]			13,5	13,5										-	-	-	-	-	11,25								13,5	13,5
39	Thrust vectoring:														Yes	Yes	Yes	Yes	Yes	No		Yes
40	Thrust vectroing angle: [degrees]														1.17,4.5	1.17,4.5	1.17,4.5	1.17,5.4	1.17,6.3	-		0,005/0,05
41	Wing area multiplier:	1,2	2,8	2,1	2,1	1,5	1,5	-	2,8	2,8	1,05	1,05	1,05	1,2	1,7	1,7	1,7	1,7	1,7	1,95	2,8	2,35	1,7	1,7	1,7	2,8	2,8	2,1	2,1
42	Max lateral acceleration:	6	3			3	3	-	6	6	10	10	10	6							3	6	6	6	6	3	3	6	6
43	Start speed: [m/s]	-	0	55	55	10	10	55	-	-	55	55	55	-	70	70	70	70	70	75	0	-	20	20	20	0	15	55	55
44	Maximum speed: [m/s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
45	Maximum statcard (useless) speed: [m/s] or [Mach]	455	190	296	329	140	140	400	230	230	550	550	550	2	220	220	240	240	240	500	190	210	250	250	250	190	85	296	329
46	Statcard (useless) guaranteed range: [km]	8	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
47	Minimum range: [m]			65	65			30	30	30	30	30	30	600	30	30	30	30	30	30	30	30	30	30	30	30	230	65	65
48	Maximum (flight) range: [km]	12	3,5	3,75	3,75	3	3	2,5	4	4	5	6	6	10	3	3	4	4	4	5,5	3,5	7	4	4	4,3	3,5	2	3,75	3,75
49	Load factor limit at launch: [G]	-	-	-	-	20	20	-	20	20	-	-	-	7	20	20	20	20	20	20	-	-	20	20	20	-	-	-	-
50	Maximum G-load: [G]	-	-	5	5	-	-	-	-	-	-	-	-	-	7	7	7	7	7	10	-	-	-	-	-	-	-	5	5
51	Statcard (useless) max G-load: [G]	-	-	-	-	-	-	-	-	-	-	-	-	2	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
52	Flight time until guidance starts (delay): [s]														0	0	0	0	0	-
53	Starting G-limit: [G]														0,5	0,5	0,5	0,5	0,5	-
54	Flight time when pull limit reaches 30%: [s]														1,25	1,25	1,25	1,25	1,25	-
55	Flight time when pull limit reaches 100%: [s]														1,5	1,5	1,5	1,5	1,5	-
56	Additional Notes:																		Identical to the HJ8H							Swedish SS.11		Swedish TOW	Swedish TOW-2
57
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67


1	Name:	AGM-12B	AGM-12C	Kh-23M	Kh-25MR	Ki-148	AS.20	AS.30	Rb 05A

2	Physical properties
3	Mass: [kg]	259	810	289	297	680	143,8	520	305
4	Mass at end of booster burn: [kg]	204	647	225,5	277	585	118,8	463	267,25
5	Mass at end of sustainer burn: [kg]	-	-	-	214,5	-	107,8	393	240,5
6	Calibre: [mm]	298	460	275	275	570	250	342	300
7	Length: [m]	3,12	4,14	3,49	3,75	4,09	3,12	3,885	3,636
8	Engine properties
9	Force exerted by booster: [N]	53400	147000	24700	20000	2510	28000	58425	17350
10	Burn time of booster: [s]	2,04	2,25	4,9	2	75	1,8	2	4,9
11	Raw acceleration at ignition: [m/s²]	206,18	181,48	85,47	67,34	3,69	194,71	112,36	56,89
12	Specific impulse of booster: [s]	201,90	206,84	194,29	203,87	202,00	205,50	208,97	229,57
13	ΔV of booster: [m/s]	472,80	455,92	472,89	139,43	298,19	385,02	238,01	297,56
14	Force exerted by sustainer: [N]	-	-	-	16500	-	1480	6525	7535
15	Burn time of sustainer: [s]	-	-	-	8	-	14,5	22	8
16	Specific impulse of sustainer: [s]	-	-	-	215,29	-	198,87	209,04	229,71
17	ΔV of sustainer: [m/s]	-	-	-	540,05	-	189,56	336,15	237,66
18	Total ΔV: [m/s]	472,80	455,92	472,89	679,48	298,19	574,58	574,16	535,22
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	58,05	136,5	96	119,04	143	15,851	99,56	76,8
21	Tandem charge:	No	No	No	No	No	No	No	No
22	Penetration: [mm]	92	102	97	97	400	69	99	95
23	Proximity fuse:	No	No	No	No	No	No	No	Yes
24	Proximity fuse range: [m]	-	-	-	-	-	-	-	6
25	Proximity fuse arming distance: [m]	-	-	-	-	-	-	-	-
26	Proximity fuse shell detection (80-200 mm):	-	-	-	-	-	-	-	Yes
27	Proximity fuse minimum altitude: [m]	-	-	-	-	-	-	-	-
28	Proximity fuse delay: [s]	-	-	-	-	-	-	-	3
29	Guidance properties
30	Guidance type:	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS
31	Guidance duration: [s]	30	30	30	45	90	30	24	24
32	Guidance range: [km]	8	16	10	10	12	8	10	8
33	Flight characteristics
34	Maximum fin angle of attack: [degrees]	13,5	13,5	-	-	11,25	13,5	13,5	13,5
35	Wing area multiplier:	1,2	1,2	1,2	1,2	7,75	1,2	1,2	1,2
36	Max lateral acceleration: [G]	6	6	6	6	6	12	6	-
37	Start speed: [m/s]	-	-	-	-	-	-	-	-
38	Maximum speed: [m/s]	-	-	-	-	-	-	-	-
39	Maximum statcard (useless) speed: [m/s] or [Mach]	455	445	2	2	150	1,7	370	415
40	Minimum range: [m]	30	30	600	600	30	30	30	30
41	Maximum (flight) range: [km]	12	16	10	10	12	10	12	11
42	Additional Notes:
43
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46
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48
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51
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53


1	Name:	9M120-1 Ataka	9M123 Khrizantema	9M133M-2 Kornet	9M133FM-3 Kornet	9M127 Vikhr'

2	Physical properties
3	Mass: [kg]	33,5	46	26	28	47
4	Mass at end of booster burn: [kg]	27,93	36,6	23,38	24,68	42,5
5	Mass at end of sustainer burn: [kg]	23,68	31,3	19,7	18,9	30,75
6	Calibre: [mm]	130	155	152	152	130
7	Length: [m]	1,93	2,04	1,21	1,15	2,75
8	Engine properties
9	Force exerted by booster: [N]	6480	19130	5760	6750	27000
10	Burn time of booster: [s]	2	1	1	1	0,28
11	Raw acceleration at ignition: [m/s²]	193,43	415,87	221,54	241,07	574,47
12	Specific impulse of booster: [s]	237,18	207,45	224,11	207,25	171,25
13	ΔV of booster: [m/s]	423,11	465,21	233,51	256,60	169,08
14	Force exerted by sustainer: [N]	3070	2270	290	407	3500
15	Burn time of sustainer: [s]	3	3	29	29	7,56
16	Specific impulse of sustainer: [s]	220,90	130,98	232,96	208,16	229,55
17	ΔV of sustainer: [m/s]	357,72	201,00	391,39	544,88	728,75
18	Total ΔV: [m/s]	780,82	666,21	624,90	801,48	897,83
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	4,4838	6,16	6,16	9,24	5,16
21	Tandem charge:	No	Yes	Yes	Yes	Yes
22	Penetration: [mm]	800	1200	1200	61	800
23	Proximity fuse:	No	No	No	Yes	Yes
24	Proximity fuse range: [m]	-	-	-	4	2,5
25	Proximity fuse arming distance: [m]	-	-	-	300	300
26	Proximity fuse shell detection (80-200 mm):	-	-	-	Yes	No
27	Proximity fuse minimum altitude: [m]	-	-	-	25	25
28	Proximity fuse delay: [s]	-	-	-	-	-
29	Guidance properties
30	Guidance type:	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR
31	Guidance duration: [s]	25	25	50	60	28
32	Guidance range: [km]	6	6	8	10	10
33	Aim tracking sensitivity:	0,5	0,5	0,5	0,5	0,5
34	Flight characteristics
35	Maximum axis values:	0,75	0,75	0,75	0,75
36	Wing area multiplier:	1,05	1,05	2,1	2,1	1,05
37	Maximum fin AOA: [degrees]					13,5
38	Maximum fin lateral acceleration:					17,5
39	Max lateral acceleration:	10	10	6	6	10
40	Start speed: [m/s]	55	100	76	70	55
41	Maximum speed: [m/s]	-	-	-	-	-
42	Maximum statcard (useless) speed: [m/s]	550	550	300	320	600
43	Statcard (useless) guaranteed range: [km]	-	-	-	-	8
44	Minimum range: [m]	30	30	30	30	1500
45	Maximum (flight) range: [km]	6	6	8	10	10
46	Load factor limit at launch: [G]	-	-	-	-	-
47	Maximum G-load: [G]	-	-	-	-	15
48	Additional Notes:	LOSBR version of the 9M120-1
49	LOSBR missiles trigger LWS, except for the 9M123 in radar guided mode.
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59


1	Name:	AGM-62A	AGM-62A ER	GBU-8/B	GBU-10/B	GBU-12/B	GBU-15(V)1/B	GBU-15(V)2/B	GBU-16	GBU-24/B	GBU-38 AIR-FORCE	GBU-38 NAVY	KAB-50L	KAB-50TV	KAB-500Kr	KAB-500Kr-E	KAB-500L-F-E	Mk. 82 GCS-1	M117 GCS-1	BGL-400	BGL-1000	Mk. 13 (Paveway)	Mk. 18 (Paveway)	GB-500	GB-1000	GB-250

2	Physical properties
3	Mass: [kg]	505,3	510,3	1027	957	277,14	1140,8	1140,8	495,3	1050	240,9	240,9	50	50	520	520	560	283	410	400	970	546,5	546,5	570	1090	260
4	Calibre: [mm]	381	381	457	457,2	279,4	457	457	355,6	368	273	273	120	120	350	350	400	273	410	403	457,2	420	420	377	377	299
5	Length: [m]	3,4544	3,4544	3,63	4,318	3,3274	3,962	3,962	3,683	4,31	2,207	2,207	1,85	1,95	3,05	3,05	3,05	2,873	2,56	3,4	4,37	3,488	3,488	3,34	3,34	2,735
6	Warhead explosive mass
7	Explosive mass: [kg of TNT equivalent]	264,358	264,358	505,748	578,745	117,585	505,748	505,748	238,124	505,748	117,585	117,585	24	24	160	160	312	117,585	206,618	167	500	288	294,4	220	537,6	91
8	Guidance properties
9	Zoom:	14.74x	14.74x	14.74x	-	-	14.74x	2.48x - 4.92x	-	-	-	-	-	14.74x	6.15x - 25.4x	6.15x - 25.4x	-	-	-	-	-	-	-	-	-	-
10	Guidance type:	Optic/TV	Optic/TV	Optic/TV	Laser	Laser	Optic/TV	IR	Laser	Laser+IOG	GNSS	GNSS	Laser	Optic/TV	Optic/TV	Optic/TV	Laser	IR	IR	Laser	Laser	Laser	Laser	Laser	Laser+IOG	Laser+IOG
11	Guidance duration: [s]	-	-	90	60	60	90	90	60	90	-	-	-	-	40	60	60	-	-	60	60	60	60	60	105	80
12	Seeker warm up time: [s]	1	1	1	-	-	1	1	-	-	1	1	-	1	1	1	-	0,1	0,1	-	-	-	-	-	-	-
13	Seeker search duration: [s]	3600	3600	3600	-	-	3600	3600	-	-	3600	3600	-	3600	3600	3600	-	3600	3600	-	-	-	-	-	-	-
14	Field of view: [degrees]	0,1	0,1	0,1	20	20	0,1	0,1	20	30	-	-	30	0,25	0,1	0,1	20	5	5	20	20	20	20	25	30	30
15	Optic sight field of view: [degrees]	5 / 5	5 / 5	5 / 5	5 / 5	5 / 5	5 / 5	30/ 15	5/5	5 / 5	-	-	5 / 5	5 / 5	12 / 2.9	12 / 2.9	5 / 5	-	-	5 / 5	5 / 5	5 / 5	5 / 5	5 / 5	-	5 / 5
16	Gimbal limit: [degrees]	60	60	60	0	0	60	54	0	45	-	-	45	65	58	58	0	30	30	0	0	0	0	0	45	34
17	Track rate: [degrees/second]	5	5	5	10000	10000	5	2,5	10000	8	-	-	8	5	7	7	10000	10	10	10000	10000	10000	10000	10000	8	8
18	Uncaged seeker before launch:	Yes	Yes	Yes	No	No	Yes	Yes	No	-	No	No	Yes	Yes	Yes	Yes	No	Yes	Yes	No	No	No	No	No	No	Yes
19	Maximum lock angle before launch: [degrees]	30	30	30	-	-	30	30	-	45	-	-	35	80	55	55	-	30	30	-	-	-	-	-	45	35
20	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	-	-	-	-	-	-	1	-	-	-	-	-	-	-	-	-	10	10	-	-	-	-	-	-	-
21	Lock-on range (ground): [km]	40	40	40	-	-	40	20	-	40	-	-	-	6	15	15	-	-	-	-	-	-	-	-	-	-
22	Lock-on range (vehicle): [km]	6	6	6	3,657	3,657	6	20	3,657	3,657	-	-	7	18	6	6	4	0,8	0,8	3,657	3,657	3,657	3,657	4	6	6
23	Can lock after launch:	No	No	No	Yes	Yes	No	No	Yes	No	-	-	Yes	No	No	No	Yes	No	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes
24	PID proportional term:	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,0656	0,09	0,0451	0,0451	0,0626	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,0456	0,1
25	PID integral term:	0,05	0,05	0,05	0,1	0,1	0,05	0,05	0,1	0,1	0,05	0,05	0	0,07	0,1276	0,1276	0,1181	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1846	0,1
26	PID integral term limit:	0,85	0,85	1	0,75	0,75	1	1	0,75	0,5	0,85	0,85	0	0,5	1	1	1	0,75	0,75	0,75	0,75	0,75	0,75	0,75	1	0,75
27	PID derivative term:	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,0013	0,0008	0,0003	0,0003	0,0001	0,1	0,1	0,1	0,1	0,1	0,1	0,1	0,0003	0,1
28	Inertial navigation:									Yes			Yes	Yes											Yes	Yes
29	Inertial navigation drift speed:									5			5	5											5	5
30	Flight characteristics
31	Maximum fin angle of attack: [degrees]	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	13,5	22,5	13,5	13,5	18	13,5	13,5	13,5	13,5	13,5	13,5	18	18	13,5
32	Wing area multiplier:	2,175	2	1,8	1,8	1,8	1,8	1,8	1,8	1,8	1,3	1,3	2,25	2,25	1,8	1,8	1,6	1,5	1,5	1,8	1,8	1,8	1,8	1,6	1,65	1,5
33	Maximum G-load: [G]	4	4	4	4	4	4	4	4	4	5	5	5	4,5	3,5	3,5	4	3	3	3	4	4	4	4	3	4
34	Loft:									Yes			Yes	Yes	Yes	Yes
35	Loft angle:									5			7,5	7,5	5	5
36	Target elevation:									-40			-40	-40	-40	-40
37	Maximum target angular change: [degrees/s]									0,75			1,75	1,75	0,75	0,75
38	Additional Notes:	Image found under artist Atamonica	Image found under artist Atamonica		Image found under artist Atamonica	Image found under artist Atamonica			Image found under artist Atamonica
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1	Name:	FIM-92E	FIM-92K	MIM-72A	MIM-72C	MIM-72E	MIM-72G	9M37M	9M39	Type 91 (SAM-3)	Type 81C (SAM-1C)	HN6	Mistral SATCP

2	Physical properties
3	Mass: [kg]	10,1	10,1	86,3	86,3	86,3	86,3	39,2	10,6	11,5	105	10,77	18,7
4	Mass at end of booster burn: [kg]	7,445	7,445	53,65	53,65	53,65	53,65	28,12	7,69	7,8	61	7,685	17,1
5	Mass at end of sustainer burn: [kg]	5,5	5,5	-	-	-	-	23,55	5,59	6,5	-	5,7	11,5
6	Calibre: [mm]	70	70	127	127	127	127	120	72,2	80	160	71	90
7	Length: [m]	1,52	1,52	2,9	2,9	2,9	2,9	2,19	1,68	1,43	2,71	1,495	1,86
8	Engine properties
9	Force exerted by booster: [N]	4340	4340	12460	12460	12460	12460	12400	2975	3410	17700	2910	0
10	Burn time of booster: [s]	1,4	1,4	5	5	5	5	2,1	1,9	2	5,5	2	0
11	Raw acceleration at ignition: [m/s²]	429,70	429,70	144,38	144,38	144,38	144,38	316,33	280,66	296,52	168,57	270,19	0,00
12	Specific impulse of booster: [s]	233,28	233,28	194,51	194,51	194,51	194,51	239,57	198,01	187,89	225,54	192,31	0,00
13	ΔV of booster: [m/s]	697,98	697,98	907,02	907,02	907,02	907,02	780,72	623,39	715,59	1201,58	636,70	0,00
14	Force exerted by sustainer: [N]	675	675	-	-	-	-	2755	705	770	-	723	5925
15	Burn time of sustainer: [s]	5,6	5,6	-	-	-	-	3,9	6,6	6	-	6	2,2
16	Specific impulse of sustainer: [s]	198,11	198,11	-	-	-	-	239,66	225,86	362,27	-	222,77	237,28
17	ΔV of sustainer: [m/s]	588,46	588,46	-	-	-	-	416,98	706,68	647,94	-	653,00	923,46
18	Total ΔV: [m/s]	1286,44	1286,44	907,02	907,02	907,02	907,02	1197,70	1330,08	1363,53	1201,58	1289,70	923,46
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	0,54	0,54	3,541632	4,3056	4,3056	4,3056	1,694	0,77	0,648	5,4	0,77	1,776
21	Proximity fuse:	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
22	Proximity fuse range: [m]	-	0,5	5	5	5	5	4	0,5	0,5	7	0,5	1,5
23	Proximity fuse arming distance: [m]	-	-	-	-	-	-	-	-	-	-	-	-
24	Proximity fuse shell detection (80-200 mm):	-	-	Yes	Yes	Yes	Yes	-	-	-	Yes	-	-
25	Proximity fuse minimum altitude: [m]	-	-	-	-	-	-	-	-	-	25	-	-
26	Proximity fuse delay: [s]	-	0,7	1,8	1,8	1,8	1,8	1,3	0,5	0,7	1,5	0,5	2
27	Guidance properties
28	Guidance type:	IR	IR	IR	IR	IR	IR	IR/Optic	IR	IR/Optic	IR/Optic	IR	IR
29	Guidance start delay: [s]	0,3	0,3	0,4	0,4	0,4	0,4	0,35	0,7	0,5	0,3	0,25	0,1
30	Guidance duration: [s]	15	15	60	60	60	60	16	14	10,5	22,5	16	14
31	Seeker warm up time: [s]	2	2	1,2	1,2	1,2	1,2	1,2	2	2	1,2	2	2
32	Seeker search duration: [s]	60	60	20	20	20	20	20	60	60	20	60	60
33	Field of view: [degrees]	3	3	2,5	3	3	3	1	2	3	3	3	3
34	Gimbal limit: [degrees]	40	40	40	40	40	40	40	38	40	30	40	38
35	Track rate: [degrees/second]	12	12	12	22	22	12	20,4	12	12	15	12	20
36	Uncaged seeker before launch:	Yes	Yes	No	No	No	No	Yes	No	Yes	Yes	Yes	Yes
37	Maximum lock angle before launch: [degrees]	8	8	-	-	-	-	40	-	15	15	15	25
38	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	5	5	10	10	10	5	10	5	5 / 10	5 / 10	5	10
39	Lock-on range from rear-aspect: [km]	11	11	5,5	12	12	11	11 / NA	11	11 / NA	11 / NA	11	11
40	Lock-on range from all-aspect: [km]	6	6	-	3,6	3,6	6	3,2 / 5,950	6	6 / 7	6 / 7	6	6
41	Countermeasure detection range: [km]	11	11	8	12	12	11	11 / 11	11	11 / 11	11 / 11	11	11
42	IRCM detection range: [km]	-	-	8	12	12	-	11 / NA	-	-	-	-	-
43	DIRCM detection range: [km]	1	1	-	-	-	1	-	1	1	1	1	1
44	IRCCM:	Yes	Yes	No	No	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes
45	IRCCM type:	FOV + Seeker shut off	FOV + Seeker shut off	-	-	-	FOV + Seeker shut off	FOV	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off	FOV + Seeker shut off
46	IRCCM field of view: [degrees]	1,25	1,25	-	-	-	1,25	0,5	1	0,5	0,5	1,25	1,5
47	Head-on lock-on range against afterburning target: [km]	6	6	1	6	6	6	6	6	6	6	6	6
48	Maximum break lock time: [s]	3	3	3	3	3	3	3	5	3	3	3	5
49	Can be slaved to radar:	No	No	No	No	No	No	No	No	No	No	No	No
50	Can lock after launch:	No	No	No	No	No	No	No	No	No	No	No	No
51	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	4	4	4	4	4	4	4	4	4	4	4	4
52	Base indicated air speed: [m/s]	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800	1800
53	PID proportional term:	0,0056	0,0056	0,0055	0,0055	0,0055	0,0055	0,0021	0,0026	0,0065	0,0021	0,0036	0,0016
54	PID integral term:	0,00841	0,00841	0,0631	0,0631	0,0631	0,0631	0,0586	0,1646	0,0956001	0,0526	0,1121	0,0926
55	PID integral term limit:	1	1	1	1	1	1	1	1	1	1	1	1
56	PID derivative term:	0,0005	0,0005	0,018	0,012	0,012	0,012	0,0005	0,0012	0,0004	0,0007	0,0008	0,0004
57	Flight characteristics
58	Maximum fin angle of attack: [degrees]	4,185	4,185	9,9	9,9	9,9	9,9	11,25	4,185	4,5	12,15	4,5	3,6
59	Fins laterall acceleration:	-	-	-	-	-	-	-	14,16	-	43,4683	-	-
60	Wing area multiplier:	1,05	1,05	1,4	1,4	1,4	1,4	1,125	1,05	1,05	1,2	1,05	1,05
61	Start speed: [m/s]	30	30	0	0	0	0	-	30	25	5	30	35
62	Maximum speed: [m/s]	680	680	720	720	720	720	700	590	648	955	600	850
63	Maximum statcard (useless) speed: [Mach]	2	2	2	2	2	2	-	1,7	1,9	2,8	1,76	2,5
64	Maximum statcard (useless) launch range: [km]	5	5	10	10	10	10	5	5,2	5	10	5	6
65	Maximum (flight) range: [km]	10	10	10	10	10	10	10	8	10	10	10	10
66	Maximum G-load: [G]	13	13	16,5	16,5	16,5	16,5	20	10,2	10	35	12	16
67	Maximum statcard (useless) G-load: [G]	13	13	16,5	16,5	16,5	16,5	20	10,2	10	35	12	16
68	Thrust vectoring:	No	No	No	No	No	No	No	No	No	No	No	No
69	Thrust vectoring angle: [degrees]	-	-	-	-	-	-	-	-	-	-	-	-
70	Additional Notes:					MIM-72C with smokeless motor							The air and ground based Mistrals are the same.
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1	Name:	MIM-146	RIM-24A	9M133FM3 Kornet-EM	9M220O	9M311	9M311-1M	95Ya6	9M331	V-601	Starstreak	Starstreak (dart)	Roland 1	Roland 2	Roland 3	VT1	Rb 70	Rb 70 Mk. 2	BOLIDE

2	Physical properties
3	Mass: [kg]	51	580	28	33,5	41,6	41,6	72,5	167	912	14	0,9	65	65	77	73	16,5	16,5	17
4	Mass at end of booster burn: [kg]	32	510	24,68	27,93	18,5	18,5	28	108,1	602	13	-	50,3	50,3	57,5	39,75	13,05	12,85	12,5
5	Mass at end of sustainer burn: [kg]	27,5	350	18,9	23,68	-	-	-	82,3	477	7,5	-	38,1	38,1	45,3	-	11,5	11,3	11
6	Calibre: [mm]	152	343	152	130	152	152	90	239	379	130	20	163	163	163	165	105	105	105
7	Length: [m]	2,05	4,57	1,15	1,83	1,5	1,5	1,85	2,898	3,9	1,08	0,68	2,44	2,44	-	2,35	2,05	2,05	2,05
8	Engine properties
9	Force exerted by booster: [N]	43700	55200	6750	6480	10380	10380	25932,95	32370	135625	0	-	16500	16500	19200	22325	7350	8200	10100
10	Burn time of booster: [s]	1	3	1	2	2,6	2,6	2,4	4	4	0	-	1,7	1,7	2	3,5	1	1	1
11	Raw acceleration at ignition: [m/s²]	856,86	95,17	241,07	193,43	249,52	249,52	357,70	193,83	148,71	0,00	-	253,85	253,85	249,35	305,82	445,45	496,97	594,12
12	Specific impulse of booster: [s]	234,45	241,15	207,25	237,18	119,09	119,09	142,57	224,09	178,39	0,00	-	194,51	194,51	200,74	239,55	217,17	229,01	228,79
13	ΔV of booster: [m/s]	1072,01	304,27	256,60	423,11	946,72	946,72	1330,63	956,12	726,92	0,00	-	489,22	489,22	575,06	1428,45	499,74	561,68	690,13
14	Force exerted by sustainer: [N]	5300	30000	407	3070	-	-	-	7100	13125	20000	-	2130	2130	2130	-	660	660	750
15	Burn time of sustainer: [s]	2	12	29	3	-	-	-	8	20	0,58	-	11,7	11,7	11,5	-	5	5	5
16	Specific impulse of sustainer: [s]	240,12	229,36	208,16	220,90	-	-	-	224,42	214,07	214,99	-	208,23	208,23	204,67	-	217,03	217,03	254,84
17	ΔV of sustainer: [m/s]	356,98	847,07	544,88	357,72	-	-	-	600,33	488,76	1160,10	-	567,44	567,44	478,81	-	269,20	273,67	319,58
18	Total ΔV: [m/s]	1428,99	1151,35	801,48	780,82	946,72	946,72	1330,63	1556,45	1215,68	1160,10	-	1056,66	1056,66	1053,87	1428,45	768,94	835,35	1009,72
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	7,86	49,28	9,54	6,16	4,62	4,62	8,47	8,162	40,92	1,572	0,524	4,585	4,585	6,812	7,86	1,441	1,441	1,441
21	Proximity fuse:	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	No	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes
22	Proximity fuse range: [m]	6	25	4	4	5	5	9	8	40	-	-	6	6	6	8	3	3	3
23	Proximity fuse arming distance: [m]	300	300	300	300	300	300	300	300	300	-	-	300	300	300	300	300	300	300
24	Proximity fuse minimum altitude: [m]	25	25	25	-	25	25	25	25	50	-	-	25	25	25	25	-	-	-
25	Proximity fuse shell detection (80-200 mm):	Yes	No	No	No	Yes	Yes	Yes	Yes	No	No	No	Yes	Yes	Yes	Yes	No	No	No
26	Proximity fuse delay: [s]	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
27	Penetration: [mm]	900	71	61	51	39	39	60	60	70	30	50	39	39	54	59	19	200	200
28	Guidance properties
29	Guidance type:	LOSBR	SACLOS	LOSBR	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	LOSBR	LOSBR	SACLOS	SACLOS	SACLOS	SACLOS	LOSBR	LOSBR	LOSBR
30	Guidance duration: [s]	22	30	60	30	13,5	18,5	30	21	26	12	12	14	14	17	20	15	24	32
31	Guidance range: [km]	10	14	10	7	8	10	20	12	16	7	9,8	6,3	6,3	8	12	5	7	9
32	Flight characteristics
33	Maximum axis values:	1,5	0,23	0,75	0,75	-	-	-	-	-	0.01	1,5	1,5	1,5	1,5	-	1,5	1,5	1,5
34	Maximum fin angle of attack: [degrees]					11,09817	11,09817	12,61944	13,05	18		6,84				11,7
35	Maximum fin lateral acceleration:					32	32	32	62	-						65,853
36	Wing area multiplier:	1,2	0,5	2,1	1,05	1,25	1,25	1,25	1,3	1,5	1,25	1,075	1,3	1,3	1,3	1,3	1,3	1,3	1,3
37	Max lateral acceleration: [G]	35	5	6	10	32	32	32	42	10	-	47	15	15	20	50	15	15	15
38	Start speed: [m/s]	-	0	70	55	10	10	10	21	10	10	1125	30	30	30	10	50	50	50
39	Maximum speed: [m/s]	1027	620	320	550	910	910	1300	850	-	1125	1125	500	500	575	1250	525	580	700
40	Maximum (flight) range: [km]	10,5	14,5	11	7	8	10	20	12	16	8,5	9,8	6,3	6,3	8	12	5,5	7,5	10
41	Has a tracer in its tail:	Yes	No	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes
42	Additional Notes:		Naval SAM of the Douglas (PGM-100)	Anti-air variant of 9M133	Anti-air variant of 9M120			Has slight lofting when shooting at low alt targets	Vertical launch, engine fires 0.75 second after launch, has 12000 Nm torque for orientation, minimum range of 1.2 km				Also used by the airfield SAMs	Identical to the Roland 1
43	Because all of these SAMs are LOS guided, the missiles cannot be guided through clouds.
44	LOSBR missiles trigger LWS, except for the 9M123 in radar guided mode.
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1	Name:	9M14 Malyutka	Type 64	HJ-73	SS.11	LFK SS.11	LFK SS.11 (Tager)	Rb 52

2	Physical properties
3	Mass: [kg]	10,9	15,7	10,9	29,99	29,99	29,99	29,99
4	Mass at end of booster burn: [kg]	10	14,98	10	28,35	28,35	28,35	28,35
5	Mass at end of sustainer burn: [kg]	8	14,45	8	24,2	24,2	24,45	24,45
6	Calibre: [mm]	125	120	125	164	164	164	164
7	Length: [m]	0,86	1,02	0,86	1,21	1,21	1,21	1,21
8	Engine properties
9	Force exerted by booster: [N]	1500	1606	1500	3200	3200	3280	3280
10	Burn time of booster: [s]	0,9	0,8	0,9	1	1	1	1
11	Raw acceleration at ignition: [m/s²]	137,61	102,29	137,61	106,70	106,70	109,37	109,37
12	Specific impulse of booster: [s]	152,91	181,90	152,91	198,90	198,90	203,87	203,87
13	ΔV of booster: [m/s]	129,27	83,77	129,27	109,73	109,73	112,47	112,47
14	Force exerted by sustainer: [N]	40	37,98	40	470	470	390	390
15	Burn time of sustainer: [s]	27	25	27	17,5	17,5	19	19
16	Specific impulse of sustainer: [s]	55,05	182,62	55,05	202,03	202,03	193,68	193,68
17	ΔV of sustainer: [m/s]	120,50	64,53	120,50	313,69	313,69	281,19	281,19
18	Total ΔV: [m/s]	249,76	148,30	249,76	423,42	423,42	393,67	393,67
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	3,12	4,5457	3,12	2,0043	2,0043	2,0043	2,0043
21	Tandem charge:	No	No	No	No	No	No	No
22	Penetration: [mm]	400	500	400	600	600	600	600
23	Guidance properties
24	Guidance type:	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS	MCLOS
25	Guidance duration: [s]	35	25	30	18,5	18,5	20	21
26	Guidance range: [km]	3	1,8	3	3,5	3,5	3,75	3,5
27	Flight characteristics
28	Maximum axis values:	0,25	0,25	0,25	0,25	0,25	0,25	0,5
29	Wing area multiplier:	1,5	3,5	1,5	2,8	2,8	2,8	2,8
30	Max lateral acceleration:	3	3	3	3	3	3	10
31	Start speed: [m/s]	10	-	10	0	0	5	0
32	Maximum speed: [m/s]	140	85	140	190	190	190	190
33	Statcard (useless) guaranteed range: [km]	-	-	-	-	-	-	-
34	Maximum (flight) range: [km]	4	2	3,5	3,5	3,5	3,5	3,5
35	Additional Notes:			Chinese 9M14		Identical to the SS.11	For some reason the SS.11 of the Zachlam (Tager) defers from other SS.11s.	Identical to the SS.11
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1	Name:	MGM-51B	MGM-51C	TOW	ITOW	TOW-2	TOW-2A	TOW-2B	3M7 Drakon	Rubin	9M112 Kobra	9M113 Konkurs	9M114 Shturm	9M120 Ataka	9M120F-1 Ataka	Swingfire	Swingfire Mk. 2	Type 79	Type 79 ASM	302	HJ-9	HJ-73E	QN201	HOT	HOT-2	MILAN	MILAN 2	LFK SS.11B	Rb 55	Rb 55B	Rb 55C	Rb 56 BILL II

2	Physical properties
3	Mass: [kg]	27,8	27,8	18,82	19,05	21,45	22,63	22,59	54	28,5	27,5	14,5	31,4	33,5	33,5	27	27	19,9	19,9	11,2	29	12,5	7	23	23	6,7	7	29,99	18,82	19,05	21,45	10,9
4	Mass at end of booster burn: [kg]	23,12	23,12	16,32	16,55	18,25	19,43	19,39	48,5	20,5	24,2	12,8	25,83	27,93	27,93	24,65	24,65	18,34	18,34	9,05	21	11,6	5,65	20,04	20,04	6,53	6,83	28,35	16,32	16,55	18,25	9,8
5	Mass at end of sustainer burn: [kg]	-	-	-	-	-	-	-	47	-	-	11,7	21,58	23,68	23,68	22,3	22,3	16	16	-	-	9,6	-	17,44	17,44	5,8	6,1	24,2	-	-	-	-
6	Calibre: [mm]	152	152	127	127	127	152	152	180	125	125	135	130	130	130	170	170	152	152	120	152	125	70	136	150	103	115	164	127	127	127	150
7	Length: [m]	1,15	1,15	1,16	1,534	1,607	1,607	1,168	1,25	1,505	1,15	1,165	1,83	1,15	1,15	1,07	1,07	1,15	1,15	0,68	1,5	0,68	1,12	1,27	1,3	0,68	0,68	1,21	1,16	1,534	1,607	1,15
8	Engine properties
9	Force exerted by booster: [N]	4200	4200	2800	2800	3590	3590	3590	27300	2900	735	1395	6480	6480	6480	2370	2370	2080	2080	268,75	3780	1600	2970	4600	4600	230	230	3200	2800	2800	3590	945
10	Burn time of booster: [s]	1,3	1,3	1,6	1,6	1,6	1,6	1,6	0,4	5,5	9	2	2	2	2	2	2	1,5	1,5	16	5	0,9	1	1,1	1,1	1,3	1,3	1	1,6	1,6	1,6	2,2
11	Raw acceleration at ignition: [m/s²]	151,08	151,08	148,78	146,98	167,37	158,64	158,92	505,56	101,75	26,73	96,21	206,37	193,43	193,43	87,78	87,78	104,52	104,52	24,00	130,34	128,00	424,29	200,00	200,00	34,33	32,86	106,70	148,78	146,98	167,37	86,70
12	Specific impulse of booster: [s]	118,93	118,93	182,67	182,67	182,98	182,98	182,98	202,39	203,24	204,34	167,30	237,18	237,18	237,18	205,61	205,61	203,87	203,87	203,87	240,83	163,10	224,26	174,26	174,26	179,29	179,29	198,90	182,67	182,67	182,98	192,66
13	ΔV of booster: [m/s]	215,06	215,06	255,41	252,10	290,00	273,66	274,19	213,28	656,90	256,25	204,66	454,35	423,11	423,11	183,67	183,67	163,27	163,27	426,30	762,55	119,56	471,36	235,50	235,50	45,20	43,24	109,73	255,41	252,10	290,00	201,06
14	Force exerted by sustainer: [N]	-	-	-	-	-	-	-	150	-	-	223	3070	3070	3070	230	230	260	260	-	-	50	-	265	265	135	135	470	-	-	-	-
15	Burn time of sustainer: [s]	-	-	-	-	-	-	-	13	-	-	13	3	3	3	24	24	18	18	-	-	27	-	17	17	10,7	10,7	17,5	-	-	-	-
16	Specific impulse of sustainer: [s]	-	-	-	-	-	-	-	132,52	-	-	268,65	220,90	220,90	220,90	239,44	239,44	203,87	203,87	-	-	68,81	-	176,63	176,63	201,71	201,71	202,03	-	-	-	-
17	ΔV of sustainer: [m/s]	-	-	-	-	-	-	-	40,84	-	-	236,81	389,57	357,72	357,72	235,34	235,34	272,99	272,99	-	-	127,74	-	240,78	240,78	234,58	223,67	313,69	-	-	-	-
18	Total ΔV: [m/s]	215,06	215,06	255,41	252,10	290,00	273,66	274,19	254,12	656,90	256,25	441,47	843,92	780,82	780,82	419,01	419,01	436,26	436,26	426,30	762,55	247,30	471,36	476,28	476,28	279,78	266,91	423,42	255,41	252,10	290,00	201,06
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	3,6	3,6	3,7524	2,8764	4,4133	4,512	3,384	3,15	3,5775	5,544	4,3725	3,9273	4,4838	6,93	4,5457	4,5457	5,502	3,013	1,9565	4,03	1,834	0,75	3,799	6,4554	1,834	2,358	2,0043	3,7524	2,8764	4,4133	2,7248
21	Tandem charge:	No	No	No	No	No	Yes	No	No	No	No	No	No	Yes	No	No	No	No	No	No	Yes	Yes	No	No	No	No	No	No	No	No	No	No
22	Penetration: [mm]	431	431	430	630	800	800	100	500	500	650	500	560	800	55	535	700	700	700	480	1200	800	200	700	900	530	730	600	430	630	800	510
23	Guidance properties																						No
24	Guidance type:	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS	SACLOS
25	Guidance duration: [s]	16	16	17	25	25	25	25	18	10	17	16	20	25	25	26	26	25	25	16	24	28	15	20	20	15	15	18,5	17	25	25	15
26	Guidance range: [km]	3,2	3,2	3	3,75	3,75	3,75	3,75	3	4	5	3	5	6	6	4	4	4	4	3	5,5	3,2	4	4	4	2	2	3,5	3	3,75	3,75	2,2
27	Flight characteristics																						-
28	Maximum axis values:	0,5	0,5						0,5	-	0,5	0,5	0,75	0,75	0,75	1	1	0,5	0,5	0,5	0,75	0,25	0,5	0,5	0,5			0,25				0,5
29	Maximum fin AOA: [degrees]			13,5	13,5	13,5	13,5	13,5		9																			13,5	13,5	13,5
30	Wing area multiplier:	1,1	1,1	2,1	2,1	2,1	2,1	2,1	2,8	1,1	1,1	1,7	1,05	1,05	1,05	1,7	1,7	1,7	1,7	2,25	1,05	1,5	1,7	1,7	1,7	1,7	1,7	2,8	2,1	2,1	2,1	1,7
31	Start speed: [m/s]	81,4	81,4	55	55	55	55	52	10	350	400	64	55	55	55	10	10	30	21	70	70	10	10	20	20	75	75	-	55	55	55	72
32	Maximum speed: [m/s]	286	286	299	296	329	329	309	224	550	400	248	550	550	550	185	185	200	200	250	500	130	450	250	250	200	185	190	299	296	329	250
33	Statcard (useless) guaranteed range: [km]	3	3	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-	500	-	-	-	-	-	-	-	-	-	-	-
34	Maximum (flight) range: [km]	3,5	3,5	3,5	3,75	3,75	3,75	3,75	3,2	5	5	4	6,5	6	6,5	4,2	4,2	4	4,2	3	5,5	3,5	4	4,6	4,6	2	6,5	3,5	3,5	3,75	3,75	2,2
35	Maximum G-overload:			5	5	5	5	5		10																7		3	5	5	5
36	Thrust vectoring:									-																Yes	Yes
37	Thrust vectoring angle: [degrees]									-																2.7/4.5	2.7/4.5
38	Additional Notes:	The two Shillelagh missiles are identical.	The two Shillelagh missiles are identical.					Uses Top-down attack. Has a proximity fuse with a range of 3 m that arms after 30 m.											Has a proximity fuse with a range of 2.5m that arms after 30m and only works against ground targets.										Swedish TOW	Swedish ITOW	Swedish TOW-2	Uses Top-down attack. Has a proximity fuse with a range of 2.5m that arms after 10m.
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1	Name:	MGM-166A LOSAT	9M117 Bastion	9M117M-1 Arkan	9M119 Refleks	9M119M-1 Invar-M	9M123 Khrizantema	9M123F Khrizantema	9M133 Kornet-EM	ZT3A1 Swift	ZT3A2 Ingwe	APS03	APS04	APS	Falaric

2	Physical properties
3	Mass: [kg]	78,92	18,8	18,8	16,5	17,2	46	46	26	26	28,5	18,8	19,8	19	24
4	Mass at end of booster burn: [kg]	37,92	17,3	17,3	12,3	13,7	36,6	36,6	23,2	25,7	27,2	17,3	18,3	17,4	22
5	Mass at end of sustainer burn: [kg]	-	-	-	-	-	31,3	31,3	19,2	24,4	25,9	-	-	-	-
6	Calibre: [mm]	162,56	100/115	100	125	125	155	155	152	127	127	100	105	125	105
7	Length: [m]	2,85	1,15	1,15	0,695	0,695	2,04	2,04	1,21	1,15	1,15	1,15	1,15	0,695	1,015
8	Engine properties
9	Force exerted by booster: [N]	61500	674	500	1210	1210	19130	19130	5760	2950	2950	674	500	540	815
10	Burn time of booster: [s]	1,5	6	6	7	5,8	1	1	1	1	1	6	6	6	5
11	Raw acceleration at ignition: [m/s²]	779,27	35,85	26,60	73,33	70,35	415,87	415,87	221,54	113,46	103,51	35,85	25,25	28,42	33,96
12	Specific impulse of booster: [s]	229,36	274,82	203,87	205,57	204,40	207,45	207,45	209,70	1002,38	231,32	274,82	203,87	206,42	207,70
13	ΔV of booster: [m/s]	1649,15	224,17	166,30	592,42	456,20	465,21	465,21	234,40	114,12	105,94	224,17	157,56	178,14	177,29
14	Force exerted by sustainer: [N]	-	-	-	-	-	2270	2270	445	360	360	-	-	-	-
15	Burn time of sustainer: [s]	-	-	-	-	-	3	3	19	8	8	-	-	-	-
16	Specific impulse of sustainer: [s]	-	-	-	-	-	130,98	130,98	215,47	225,83	225,83	-	-	-	-
17	ΔV of sustainer: [m/s]	-	-	-	-	-	201,00	201,00	400,01	115,00	108,50	-	-	-	-
18	Total ΔV: [m/s]	1649,15	224,17	166,30	592,42	456,20	666,21	666,21	634,41	229,12	214,44	224,17	157,56	178,14	177,29
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	-	4,77	4,77	5,724	5,724	6,16	9,24	6,36	3,584	3,584	4,77	4,77	5,724	5,088
21	Tandem charge:	No	No	Yes	No	Yes	Yes	Yes	Yes	No	Yes	Yes	No	Yes	Yes
22	Penetration: [mm]	775	600	750	700	850	1200	61	1200	650	1000	600	750	850	550
23	Guidance properties
24	Guidance type:	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR	LOSBR
25	Guidance duration: [s]	5	17	26	26	26	25	25	35	25	35	17,6	26	26	17
26	Guidance range: [km]	5	4	5,5	5	5	6	6	5,5	4	5	5,5	5	5	5
27	Flight characteristics
28	Maximum fin AOA: [degrees]	18	10,35	10,35								10,35		13,5	15,75
29	Maximum lateral acceleration: [G]	20
30	Wing area multiplier:	1,15	1,05	1,05	1,25	1,25	1,05	1,05	2,1	1,7	1,7	1,05	1,05	1,5	1,55
31	Start speed: [m/s]	0	370	370	350	340	100	100	76	50	50	370	370	405	370
32	Maximum speed: [m/s]	1520	370	370	400	400	550	550	300	240	220	370	370	405	370
33	Statcard (useless) guaranteed range: [km]	-	-	-	-	-	-	-	-	-	-	-	-	-	-
34	Maximum (flight) range: [km]	5	5	5	5	6	6	6	6	5	5,5	5	5	6	5
35	Additional Notes:	11.83 kg, 30 mm wide, Long core APFSDS penetrator					Can be used in either laser or in radar beam riding mode. Dual guidance is possible, where one missile is guided by laser, while the other is guided by radar	Can be used in either laser or in radar beam riding mode. Dual guidance is possible, where one missile is guided by laser, while the other is guided by radar
36	LOSBR missiles trigger LWS, except for the 9M123 in radar guided mode.
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1	Name:	QN502C	SPIKE-MR	SPIKE-LR2

2	Physical properties
3	Mass: [kg]	16,2	13	13
4	Mass at end of booster burn: [kg]	14,7	12	12
5	Mass at end of sustainer burn: [kg]	11,7	-	-
6	Calibre: [mm]	151	110	110
7	Length: [m]	1,25	1,22	1,22
8	Engine properties
9	Force exerted by booster: [N]	5400	550	550
10	Burn time of booster: [s]	0,5	2	2
11	Raw acceleration at ignition: [m/s²]	333,33	42,31	42,31
12	Specific impulse of booster: [s]	183,49	112,13	112,13
13	ΔV of booster: [m/s]	174,89	88,05	88,05
14	Force exerted by sustainer: [N]	80,00	-	-
15	Burn time of sustainer: [s]	55,00	-	-
16	Specific impulse of sustainer: [s]	149,51	-	-
17	ΔV of sustainer: [m/s]	334,78	-	-
18	Total ΔV: [m/s]	509,67	88,05	88,05
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	1,386	1,269	1,269
21	Tandem charge:	Yes	Yes	Yes
22	Penetration: [mm]	1000	700	700
23	Proximity fuse:	No	No	No
24	Proximity fuse range: [m]	-	-	-
25	Proximity fuse delay: [s]	-	-	-
26	Guidance properties
27	Zoom:	-	-	-
28	Guidance type:	IR	IR	IR
29	Guidance start delay: [s]	-	-	-
30	Guidance duration: [s]	65	35	35
31	Seeker warm up time: [s]	0,2	0,2	0,2
32	Seeker search duration: [s]	3600	3600	3600
33	Field of view: [degrees]	0,1	0,1	0,1
34	IRCCM field of view: [degrees]	0,05	0,05	0,05
35	Gimbal limit: [degrees]	45	45	45
36	Track rate: [degrees/second]	15	15	15
37	Uncaged seeker before launch:	Yes	Yes	Yes
38	Maximum lock angle before launch: [degrees]	45	45	45
39	Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]	1	1	1
40	Can lock the ground:	Yes	Yes	Yes
41	Lock-on range (ground): [km]	10	10	10
42	Lock-on range from rear-aspect: [km]	20	20	20
43	Lock-on range from all-aspect: [km]	20	20	20
44	Can lock after launch:	No	No	No
45	Flight characteristics
46	Maximum fin angle of attack: [degrees]	18	18	18
47	Wing area multiplier:	1,75	1,5	1,5
48	Start speed: [m/s]	25	100	100
49	Maximum speed: [m/s]	205	180	180
50	Maximum statcard (useless) speed: [Mach]	-	-	-
51	Maximum statcard (useless) launch range: [km]	-	-	-
52	Minimum range: [m]	300	200	200
53	Maximum (flight) range: [km]	8	4	4
54	Load factor limit at launch: [G]	-	-	-
55	Maximum G-load: [G]	8	4	4
56	Maximum statcard (useless) G-load: [G]	-	-	-
57	Thrust vectoring:	No	No	No
58	Thrust vectoring angle: [degrees]	-	-	-
59	Loft:	Yes	Yes	Yes
60	Loft angle: [degrees]	7,5	20	20
61	Target elevation: [degrees]	-7,5	-15	-15
62	Maximum target angular change: [degrees/s]	2,5	0,95	0,95
63	Additional Notes:		Two spikes are identical
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1	Name:	Nettuno	AS.34 Kormoran	AM-38 / AM-39 Exocet

2	Physical properties
3	Mass: [kg]	168	600	735
4	Mass at end of booster burn: [kg]	110	587,75	625
5	Mass at end of sustainer burn: [kg]	-	460	475
6	Calibre: [mm]	201	345	350
7	Length: [m]	3,73	4,4	4,7
8	Engine properties
9	Force exerted by booster: [N]	30000	26950	120000
10	Burn time of booster: [s]	5	1	2
11	Raw acceleration at ignition: [m/s²]	178,57	44,92	163,27
12	Specific impulse of booster: [s]	263,63	224,26	222,41
13	ΔV of booster: [m/s]	1095,22	45,38	353,71
14	Force exerted by sustainer: [N]	-	2810	2900
15	Burn time of sustainer: [s]	-	100	120
16	Specific impulse of sustainer: [s]	-	224,22	236,49
17	ΔV of sustainer: [m/s]	-	539,07	636,69
18	Total ΔV: [m/s]	1095,22	584,45	990,41
19	Fuse and warhead properties
20	Explosive mass: [kg of TNT equivalent]	25,28	73,36	104,8
21	Tandem charge:	No	No	No
22	Penetration: [mm]	24	75	75
23	Guidance properties
24	Guidance type:	SACLOS	ARH+IOG	ARH+IOG
25	Guidance duration: [s]	-	101	180
26	Guidance range: [km]	10	-	-
27	Guidance start delay: [s]	-	-	-
28	Seeker warm up time: [s]	-	1,4	1
29	Seeker search duration: [s]	-	100	180
30	Gimbal limit: [degrees]	-	45	45
31	Track rate: [degrees/second]	-	20	20
32	Uncaged seeker before launch:	-	Yes	Yes
33	Maximum lock angle before launch: [degrees]	-	15	15
34	Lock-on range from all-aspect: [km]	-	15	15
35	Maximum break lock time: [s]	-	101	120
36	Can lock after launch:	-	Yes	Yes
37	Band:	-	I	J
38	Sidelobe attenuation:	-	-80	-80
39	Transmitter power:	-	2000	2000
40	Transmitter angle of half sensitivity:	-	5	5
41	Transmitter sidelobe sensitivity:	-	-30	-60
42	Receiver angle of half sensitivity:	-	5	5
43	Receiver sidelobe sensitivity:	-	-60	-60
44	Distance minimum value: [m]	-	150	100
45	Distance maximum value: [m]	-	15000	15000
46	Distance gate: [m]	-	150	150
47	Distance minimum signal gate: [m]	-	75	75
48	Distance refWidth: [m]	-	750	750
49	Proportional navigation multiplier: (affects how far ahead it attempts to lead)	-	6	6
50	Base indicated air speed: [m/s]	-	1800	1800
51	PID proportional term:	-	0,012	0,0295
52	PID integral term:	-	0,0001	0,0225
53	PID integral term limit:	-	1	1
54	PID derivative term:	-	0,0005	0,0058
55	Inertial guidance drift speed:	-	0	0
56	Flight characteristics
57	Maximum axis values:	0,5	-	-
58	Maximum fin angle of attack: [degrees]	-	13,5	13,5
59	Wing area multiplier:	-	2,75	2,75
60	Start speed: [m/s]	100	-	-
61	Maximum speed: [m/s]	280	1000	1000
62	Statcard (useless) guaranteed range: [km]	10	-	-
63	Maximum (flight) range: [km]	10	34	70
64	Start speed: [m/s]	-	-	-
65	Maximum statcard (useless) speed: [Mach]	-	0,95	0,95
66	Maximum statcard (useless) launch range: [km]	-	32	70
67	Minimum range: [m]	-	2000	2000
68	Maximum G-load: [G]	-	5	5
69	Maximum statcard (useless) G-load: [G]	-	2,5	2,5
70	Sea skimming:	No	No	Yes
71	Loft:	No	Yes	No
72	Loft angle: [degrees]	-	7	-
73	Target elevation: [degrees]	-	-10	-
74			2
75	Additional Notes:		Minimum target size is 30 m.	Minimum target size is 30 m. 30 second before impact travels at 15 m above sea level, 20 second before impact lowers to 2.5 m above sea level
76	New page, all future AShMs will be here
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