Rockets

	A	B	C	D	E	F	G	H	I	J	K	L	M	N	O	P	Q	R	S	T	U	V	W	Y	Z	AB	AD
1	Name	ID	Country	Launch Site	Function of the rocket	Cost Per Launch	Height of the rocket	Diameter	Mass	Stages	Rocket Thrust	Rocket Propellant	Rocket Engine Burn Time	Fairing Diameter	Faring Height	Capacity of the rocket	Staus	First Launch	Last Launch	Total Launches	Sucess	Failures	History of the Rocket	Family Tree of European Rockets		Rocket Variants Order

2
3	Blue Streak	Europe	United Kingdom	Woomera Test Range/Guiana Space Centre	Nuclear strike, satellite vehicle	N/A	24 Meters (80ft)	3 Meters (10ft)	90,000 kg (90 Tonnes)	1 Stage		liquid oxygen/kerosene		N/A	N/A	N/A	Retired	06 June 1964	05 November 1971					Diamant
4
5
6	Black Arrow	Europe	United Kingdom	Woomera Test Range	Carrier rocket	$8 Million	13 metres (43 ft)	2 Metres (6 ft 7 in)	18,130 kilograms (39,970 lb)	3 Stages				N/A	N/A	Payload to Low Earth Orbit (220 km)	Retired	27 June 1969	28 October 1971	4	2	2
7										First Stage: Powered by Gamma 8 Rocket Engine	234.80 kN (52,785 lbf)	RP-1/HTP	131 Seconds			135 kilograms (298 lb)								Europa Rocket
8										Second Stage: Powered by Gamma 2 Rocket Engine	64.60 kN (14,523 lbf)	RP-1/HTP	116 Seconds
9										Third Stage: Powered by Waxwing Solid Rocket Motor	29.400 kN (6,609 lbf)	Solid	55 Seconds			Payload to Low Earth Orbit (500 km)								Ariane 1
10																102 kilograms (225 lb)
11
12
13	Diamant A	Europe	France	Guiana Space Centre/Hammaguir	Small launch vehicle	N/A	18.95 Meters (62.17 ft)	1.34 Meters (4.39 ft)	18,400 kg (40,500 lb)	3 Stages				N/A	N/A	Payload to Low Earth Orbit (200 km)	Retired	26 November 1965	15 February 1967	4	3	1		Ariane 2	Ariane 3
14										First Stage: Emeraude Powered by 1 Vexin B Rocket Engine	269 kN(60,473 Ibf)	N2O4/UDMH	93 Seconds			160 kg (350 lb)
15										Second Stage: Topaze Powered by 1 P2.2 Solid Rocket Motor	120.082 kN (26,996 lbf)	N2O4/UDMH	44 Seconds
16										Third Stage: P-064 Powered by 1 P-064 Solid Rocket Motor	29.400 kN (6,609 lbf)	Solid	45 Seconds
17
18
19	Diamant B	Europe	France	Guiana Space Centre/Hammaguir	Small launch vehicle	N/A	23.50 Meters (77.00 ft)	1.34 Meters (4.39 ft)	26,990 kg (59,500 lb)	3 Stages				N/A	N/A	Payload to Low Earth Orbit (200 km)	Retired	10 March 1970	21 May 1973	5	3	2
20										First Stage: Améthyste Powered by 1 Valois Rocket Engine	316 kN(71,039 Ibf)	N2O4/UDMH	116 Seconds			160 kg (350 lb)
21										Second Stage: Topaze Powered by 1 P2.2 Solid Rocket Motor	120.082 kN (26,996 lbf)	N2O4/UDMH	44 Seconds
22										Third Stage: P-068 Powered by 1 P-068 Solid Rocket Motor	50.000 kN (11,240 lbf)	Solid	46 Seconds
23
24
25	Diamant BP.4	Europe	France	Guiana Space Centre/Hammaguir	Small launch vehicle	N/A	21.6 Meters (70.80 ft)	1.40 m (4.50 ft)	26,300 kg (57,900 lb)	3 Stages				N/A	N/A	Payload to Low Earth Orbit (200 km)	Retired	6 February 1975	27 September 1975	3	3	0
26										First Stage: Améthyste Powered by 1 Valois Rocket Engine	316 kN(71,039 Ibf)	N2O4/UDMH	116 Seconds			160 kg (350 lb)
27										Second Stage: P-4/Rita Powered by 1 P-4 Solid Rocket Motor	180 kN kN (40,465 lbf)	N2O4/UDMH	55 Seconds
28										Third Stage: P-068 Powered by 1 P-068 Solid Rocket Motor	50.000 kN (11,240 lbf)	Solid	46 Seconds
29
30
31
32
33
34	Europa	Europe	ELDO	Woomera Test Range/Guiana Space Centre	Orbital carrier rocket	N/A	33 Meters (108ft)	3 Meters (10ft)	105,000 kg (105 Tonnes)	3 Stages				2 Meters	N/A	Circular Orbit Above Earth 500 km (310 mi)	Retired	Europa I: 29 November 1968	Europa I: 12 November 1970	11	4	7		Aiane 4
35										First Stage: Blue streak	1,673 kN (376,000 lbf)	RP-1/LOX	160 Seconds			1,000 kg (2,200 lb)–1,200 kg (2,600 lb)		Blue Streak: 4 June 1964	Blue Streak: 14 November 1966							Order of the year that each launched
36										Second Stage: Coralie (rocket)	274 KN (61,597 Ibf)	UDMH/N2O4	96 Seconds					Coralie: 4 August 1967	Coralie: 4 December 1967					Ariane 5		Ariane 44LP
37										Third Stage: Astris (rocket stage)	23.3 KN	N2O4/Aerozine 50	330 Seconds													Ariane 44L
38																										Ariane 40	This is the standard variant of the rocket
39																										Ariane 2P
40																										Ariane 44P
41	Ariane 1	Europe	European Space Agency (ESA)	Guiana Space Centre	Medium lift launch vehicle	$32 Million	47.4 Meters	3.8 Meters	207,200 kg (207.2 Tonnes)	3 Stages				3 Meters	N/A	Payload to Low Earth Orbit	Retired	24 December 1979	22 February 1986	11	9	2				Ariane 42L
42										Stage 1: Powered by 4 Viking-2	2,771.940 kN (623,157 lbf)	N2O4 / UDMH	145 Seconds			4,850 kg (10,690 lb)
43										Stage 2: Powered by 1 Viking-4	720.965 kN (162,079 lbf)	N2O4 / UDMH	132 Seconds
44										Stage 3: Powered by 1 HM7-A	61.674 kN (13,865 lbf)	LH2 / LOX	563 Seconds			Payload to Geostationary Transfer Orbit
45																1,850 kg (4,080 lb)
46
47
48
49	Ariane 2	Europe	European Space Agency (ESA)	Guiana Space Centre	Medium lift launch vehicle		49 Meters	3.8 Meters	219,000 kg (219 Tonnes)	3 Stages				3 Meters	N/A	Payload to Geostationary Transfer Orbit	Retired	31 May 1986	2 April 1989	6	5	1
50										Stage 1: Powered by 4 Viking-2B	2,880 kN (647,4498 lbf)	UH 25 / N2O4	140 Seconds			2,175 kg (4,795 lb)
51										Stage 2: Powered by 1 Viking-4B	805.00 kN (180,971 lbf).	UH 25 / N2O4	125 Seconds
52										Stage 3: Powered by 1 HM7-B	64.2 kN (14,400 lbf)	LH2 / LOX	729 Seconds			Payload to Low Earth Orbit
53																2,175 kg (4,795 lb)
54
55
56
57	Ariane 3	Europe	European Space Agency (ESA)	Guiana Space Centre	Medium lift launch vehicle		49 Meters	3.8 Meters	237,000 kg (237 Tonnes)	3 Stages				3 Meters	N/A	Payload to Geostationary Transfer Orbit	Retired	4 August 1984	12 June 1989	11	10	1
58										Boosters: Powered by 2 SPB 7.35 Strap On Rocket Boosters	1,380 kN (310,236 Ibf)	CTPB	26 Seconds			2,700 kg (6,000 lb)
59										Stage 1: Powered by 4 Viking-2	2,880 kN (647,4498 lbf)	UH 25 / N2O4	140 Seconds
60										Stage 2: Powered by 1 Viking-4B	805.00 kN (180,971 lbf).	UH 25 / N2O4	125 Seconds			Payload to Low Earth Orbit
61										Stage 3: Powered by 1 HM7-B	64.2 kN (14,400 lbf)	LH2 / LOX	729 Seconds			2,175 kg (4,795 lb)
62
63
64
65
66	Ariane 40	Europe	European Space Agency (ESA)	Guiana Space Centre	Expendable launch vehicle	$40-50 million for 1,200-1,600 kg	58.72 Meters	3.8 Meters	240,000 kg (240 Tonnes)	3 Stages				N/A	N/A	Payload to Geostationary Transfer Orbit	Retired	22 January 1990	3 December 1999	7	7	0
67										Stage 1: Powered by 4 Viking-5C	2710 kN (609,232 Ibf)	UH 25 / N2O4	209 Seconds			2,000 kg (4,409 lb)
68										Stage 2: Powered by 1 Viking-4B	805.00 kN (180,971 lbf).	UH 25 / N2O4	125 Seconds
69										Stage 3: Powered by 1 HM7-B	64.2 kN (14,400 lbf)	LH2 / LOX	729 Seconds			Payload to Low Earth Orbit
70																4,600 kg (10,141 lb)
71
72																Payload to Sun-Synchronous Orbit
73																2,740 kg (6,040 Ib)
74
75
76
77	Ariane 42P	Europe	European Space Agency (ESA)	Guiana Space Centre	Expendable launch vehicle	$55-65 million for 2,000-2,500 kg	58.72 Meters	3.8 Meters	320,000 kg (320 Tonnes)	3 Stages				N/A	N/A	Payload to Geostationary Transfer Orbit	Retired	20 November 1990	4 May 2002	15	15	1
78										Boosters: Powered by 2 PAP Solid Strap On Rocket Boosters	650 kN (150,000 lbf) Each or 1300 kN (300,000 Ibf) 2 Solid Boosters	CTPB 1613	33 Seconds			2,600 kg (5,732 lb)
79										Stage 1: Powered by 4 Viking-5C	2710 kN (609,232 Ibf)	UH 25 / N2O4	209 Seconds
80										Stage 2: Powered by 1 Viking-4B	805.00 kN (180,971 lbf).	UH 25 / N2O4	125 Seconds			Payload to Low Earth Orbit
81										Stage 3: Powered by 1 HM7-B	64.2 kN (14,400 lbf)	LH2 / LOX	729 Seconds			6,000 kg (13,227 lb)
82
83																Payload to Sun-Synchronous Orbit
84																3,400 kg (7,495 Ib)
85
86
87
88	Ariane 44P	Europe	European Space Agency (ESA)	Guiana Space Centre	Expendable launch vehicle	$65-80 million for 2,500-3,000 kg	58.72 Meters	3.8 Meters	350,000 kg (350 Tonnes)	3 Stages				N/A	N/A	Payload to Geostationary Transfer Orbit	Retired	4 April 1991	25 September 2001	15	15	0
89										Boosters: Powered by 4 PAP Solid Strap On Rocket Boosters	650 kN (150,000 lbf) Each or 2,600 kN (600,000 Ibf) 4 Solid Boosters	CTPB 1613	33 Seconds			3,000 kg (6,613 lb)
90										Stage 1: Powered by 4 Viking-5C	2710 kN (609,232 Ibf)	UH 25 / N2O4	209 Seconds
91										Stage 2: Powered by 1 Viking-4B	805.00 kN (180,971 lbf).	UH 25 / N2O4	125 Seconds			Payload to Low Earth Orbit
92										Stage 3: Powered by 1 HM7-B	64.2 kN (14,400 lbf)	LH2 / LOX	729 Seconds			6,500 kg (14,330 lb)
93
94																Payload to Sun-Synchronous Orbit
95																4,100 kg (9,038 Ib)
96
97
98
99	Ariane 42L	Europe	European Space Agency (ESA)	Guiana Space Centre	Expendable launch vehicle	$90-110 million for >3,000 kg	58.72 Meters	3.8 Meters	360,000 kg (360 Tonnes)	3 Stages				N/A	N/A	Payload to Geostationary Transfer Orbit	Retired	12 May 1993	23 January 2002	13	13	0
100										Boosters: Powered by 2 PAL Liquid Strap On Rocket Boosters with Viking 6 engine	670 kN (150,621 lbf) Each or 1,340 kN (301,242 Ibf) 2 Liquid Boosters	N2O4 / UDMH	142 Seconds			3,200 kg (7,054 lb)