SpaceX Roadmap Speculation

	A	B	C	D	E	F	G	H	I	J	K	L	M	N	O	P	Q
1		Calculations;	http://www.braeunig.us/space/propuls.htm
2		Methane;	http://www.braeunig.us/space/comb-OM.htm				http://www.braeunig.us/space/comb-OK.htm						Std Grav.	9.80665
3			http://en.wikipedia.org/wiki/Rocket_engine_nozzle											http://www.kbkha.ru/?p=8&cat=11&prod=59
4			Raptor 10	Raptor 15	Raptor 25	Raptor 30	Merlin 1D ref.	Merlin 1D+ (1E?)	Raptor - Merlin slayer	Raptor - MS+	Mini Raptor 25	Micro Raptor 25	Quantum Raptor 25	RD0162	Note; RD0162 is reusable up to 25 times
5		Pa, bar	1	1	1	1	1	1	1	1	1	1	1	1
6		Pa, pa	100000	100000	100000	100000	100000	100000	100000	100000	100000	100000	100000	100000
7	Optimize for:	Pe, bar	0.7	0.7	0.7	0.45	0.43	0.475	0.55	0.9	1.1	1.1	1.1	1.1
8		Pe, pa	70000	70000	70000	45000	43000	47500	55000	90000	110000	110000	110000	110000
9		Pc, bar	100	150	250	300	97	107.65	116.72	190.56	250	250	250	160
10		Pc, pa	10000000	15000000	25000000	30000000	9700000	10765000	11672000	19056000	25000000	25000000	25000000	16000000
11		Pt, pa	5,631,162	8,452,551	14,102,132	16,928,386	5,441,670	6,039,131	6,586,271	10,752,911
12		Tt, K	3,104	3,175	3,270	3,317	3,233	3,269	3,317	3,317
13		At, m^2	0.17701	0.11477	0.06668	0.05567	0.04232	0.04232	0.04232	0.04232	0.01943	0.00972	0.00486
14		Nm / Mach number	3.60	3.82	4.09	4.43	3.88	3.88	3.80	3.80
15		Ae, m^2	2.71	2.42	2.11	2.88	0.90	0.90	0.89	0.89	1.1083212	0.5541606	0.5541606	2.1382465
16		Diameter, m	1.86	1.75	1.64	1.92	1.07	1.07	1.07	1.07
17		Mixture	2.81	2.86	2.93	2.97	2.34	2.36	2.97	2.97	2.93	2.93	2.93	2.86
18		Tc, K	3425	3500	3600	3650	3585	3625	3650	3650	3600	3600	3600	3450
19		M, g/mol	19.75	20	20.4	20.6	21.82	21.95	20.6	20.6	20.4	20.4	20.4	19.9
20		k, Specific heat ratio	1.207	1.205	1.202	1.201	1.218	1.218	1.201	1.201	1.202	1.202	1.202	1.205
21		R', Gas constant	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51
22		q, kg / s	958	927	893	892.7	229	253.5	264	431	440	220	110	639
23		q incl gas gen. kg/s	100%	100%	100%	100%	103.25%	103.25%	100%	100%
24		Ve	3,104.01	3,200.24	3,310.51	3,416.94	3,078.52	3,087.25	3,228.53	3,228.11	3,232.07	3,232.07	3,232.07	3,111.70	Ve = SQRT[(2k/(k-1))(R'Tc/M)(1-(Pe/Pc)^(k-1)/k)]
25		F, sl, N	2,892,202.83	2,894,142.75	2,893,116.73	2,891,862.03	653,910.86	735,409.50	812,125.86	1,382,395.31	1,433,195.20	716,597.60	361,069.60	2,009,757.45	F = qVe+(Pe-Pa)Ae
26		F, sl, lbf	650,193.06	650,629.17	650,398.51	650,116.45	147,005.01	165,326.63	182,573.16	310,774.83	322,195.10	161,097.55	81,171.68	451,811.45
27		Isp, sl, s	307.85	318.36	330.36	330.33	282.02	286.51	313.69	327.07	332.34	332.34	334.91	320.90	Isp = F/(g*q)
28		F vac, N	3,163,665.24	3,135,752.46	3,103,666.46	3,179,937.91	743,508.59	825,330.83	901,474.26	1,471,582.78
29		F vac, lbf	711,220.24	704,945.20	697,731.98	714,878.48	167,147.38	185,541.75	202,659.48	330,824.97
30		Isp vac, s	336.75	344.94	354.41	363.24	320.66	321.54	348.20	348.17
31		q, kg / s	958.00	927.00	893.00	892.70	236.44	261.74	264.00	431.00	439.75	219.87	109.94	638.63
32		Expansion Nozzle Fact.									3	3	3
33			Raptor 10 Vac	Raptor 15 Vac	Raptor 25 Vac	Raptor 30 Vac	Raptor 1D Vac	Raptor 1D+ Vac	Merlin Slayer Vac	Merlin Slayer+ Vac	Mini Raptor 25 Vac	Micro Raptor 25 Vac	Quantum Raptor 25 Vac
34		Pa, bar	0	0	0	0	0	0	0	0	0	0	0
35		Pa, pa	0	0	0	0	0	0	0	0	0	0	0
36	Optimize for:	Pe, bar	0.02	0.02	0.02	0.02	0.03	0.0336	0.0392	0.064	0.12	0.12	0.12
37		Pe, pa	2000	2000	2000	2000	3000	3360	3920	6400	12,222.22	12,222.22	12,222.22
38		Pc, bar	100	150	250	300	97	107.65	116.72	190.56	250	250	250
39		Pc, pa	10000000	15000000	25000000	30000000	9700000	10765000	11672000	19056000	25000000	25000000	25000000
40		Pt, pa	5,631,161.89	8,452,550.85	14,102,131.95	16,928,385.94	5,441,669.71	6,039,131.39	6,586,270.69	10,752,910.75	4.30039935	1.13094	0.282735
41		Tt, K	3,103.76	3,174.60	3,269.75	3,316.67	3,232.64	3,268.71	3,316.67	3,316.67	2.96	2.96	2.96
42		At, m^2	0.18	0.11	0.07	0.06	0.04	0.04	0.04	0.04	3615	3615	3615
43		Nm / Mach number	5.65	5.90	6.20	6.31	5.45	5.43	5.29	5.29	20.5	20.5	20.5
44		Ae, m^2	44.61	40.44	36.02	35.05	7.22	7.22	7.22	7.22	1.2015	1.2015	1.2015
45		Diameter, m	7.54	7.18	6.77	6.68	3.03	3.03	3.03	3.03	8314.51	8314.51	8314.51
46		Mixture	2.81	2.86	2.93	2.97	2.36	2.375	2.97	2.97	440	220	110			440	880
47		Tc, K	3425	3500	3600	3650	3600	3625	3650	3650	3,551.94	3,551.94	3,551.94
48		M, g/mol	19.75	20	20.4	20.6	21.9	22.1	20.6	20.6	1,615,416.08	795,250.42	394,169.56
49		k, Specific heat ratio	1.207	1.205	1.202	1.201	1.217	1.215	1.201	1.201	363,159.98	178,779.41	88,612.84			357558.8136	715117.6272
50		R', Gas constant	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	8314.51	374.59	368.82	365.61
51		q, kg / s	958	927	893	892.7	229	253.5	264	431
52		q incl gas gen. kg/s	100%	100%	100%	100%	103.25%	103.25%	100%	100%
53		Ve	3,593.42	3,654.69	3,726.17	3,752.82	3,420.78	3,423.38	3,604.06	3,604.06
54		F vac, N	3,531,706.66	3,468,781.34	3,399,510.48	3,420,237.10	805,003.49	892,093.67	979,766.28	1,599,542.04
55		F vac, lbf	793,959.24	779,813.07	764,240.36	768,899.89	180,971.98	200,550.63	220,260.22	359,591.36
56		Isp vac, s	375.92	381.57	388.19	390.69	347.18	347.55	378.44	378.44
57		q, kg / s	958	927.00	893.00	892.70	236.44	261.74	264.00	431.00
58			1.221113067	1.198552262	1.175033986	1.182711024			1.206421717	1.157080051
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