User:MNW-NYC-2021/test
Orbital Launches by Launcher Family
Family | Country | Launches | Successes | Failures | Partial failures |
Retired | Active |
---|---|---|---|---|---|---|---|
Ariane | Europe | 202 | 191 | 9 | 2 | Ariane 1,2,3,4 | Ariane 5 |
Atlas | United States | 3 | 3 | 0 | 0 | Atlas 1,2,3 | Atlas 5 |
Thor/Delta | United States | 4 | 4 | 0 | 0 | Delta 1,3 | Delta 2, 4 |
Energia | Ukraine/ Russia | 2 | 2 | 0 | 0 | ||
Falcon | United States | 7 | 4 | 3 | 0 | Falcon 1 | Falcon 9 |
H-II | Japan | 27 | 21 | 6 | 0 | H-II | H-IIA, H-IIB |
Long March | People's Republic of China | 6 | 6 | 0 | 0 | ||
Minotaur | United States | 2 | 2 | 0 | 0 | Minotaur | |
Pegasus | United States | 40 | 35 | 3 | 2 | Pegasus | |
R-7 | Russia | 1748 | 0 | 0 | Soyuz | ||
Redstone/Saturn | United States | ALL | |||||
Safir | Iran | 1 | 1 | 0 | 0 | ||
SLV | India | 2 | 2 | 0 | 0 | PSLV | |
Space Shuttle | United States | 135 | 134 | 1 | 0 | ALL | |
Titan | United States | ALL | |||||
Universal Rocket | Russia | 3 | 2 | 1 | 0 | Proton | |
Vega | Europe | 0 | 0 | 0 | 0 | Vega |
Active Launch Vehicles
Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Cost (Mil US$) |
Cost/kg (LEO) (US$) |
Launches | Status | First flight | Last flight |
---|---|---|---|---|---|---|---|---|---|---|
Ariane 5ECA | Europe | EADS Astrium | 21,000[1] | 10,050 to GTO[2] | 20,000[3] | 31 [note 1] |
Operational | 2002 | ||
Ariane 5ES | Europe | EADS Astrium | 21,000[1] | 8,000 to GTO[4] | 20,000[5] | 2 | Operational | 2008 | ||
Atlas V 401 | United States | United Launch Alliance | 9,050[6] | 6,670 to SSO 4,950 to GTO[6] |
11[6] | Operational | 2002 | |||
Atlas V 411 | United States | United Launch Alliance | 9,050[6] | 8,495 to SSO 6,075 to GTO[6] |
3[6] | Operational | 2006 | |||
Atlas V 421 | United States | United Launch Alliance | 9,050[6] | 9,050 to SSO 7,000 to GTO[6] |
3[6] | Operational | 2007 | |||
Atlas V 431 | United States | United Launch Alliance | 9,050[6] | 9,050 to SSO 7,800 to GTO[6] |
2[6] | Operational | 2005 | |||
Atlas V 501 | United States | United Launch Alliance | 8,250[6] | 5,945 to SSO 3,970 to GTO 1,500 to GEO[6] |
3[6] | Operational | 2010 | |||
Atlas V 511 | United States | United Launch Alliance | 10,950[6] | 7,820 to SSO 5,370 to GTO 1,750 to GEO[6] |
0[6] | Operational | ||||
Atlas V 521 | United States | United Launch Alliance | 13,300[6] | 9,585 to SSO 6,485 to GTO 2,760 to GEO[6] |
2[6] | Operational | 2003 | |||
Atlas V 531 | United States | United Launch Alliance | 15,300[6] | 11,160 to SSO 7,425 to GTO 3,250 to GEO[6] |
1[6] | Operational | 2010 | |||
Atlas V 541 | United States | United Launch Alliance | 17,100[6] | 12,435 to SSO 8,240 to GTO 3,730 to GEO[6] |
0[6] | Operational | ||||
Atlas V 551 | United States | United Launch Alliance | 18,500[6] | 12,435 to SSO 8,700 to GTO 3,960 to GEO[6] |
1[6] | Operational | 2006 | |||
Delta II 7920 | United States | United Launch Alliance | 5,030[note 2][7] | 3,123 to SSO[note 2][7] | 27[7] | Operational | 1998 | |||
Delta II-H 7920H | United States | United Launch Alliance | 6,097[note 2][7] | 2[7] | Operational | 2003 | ||||
Delta II-H 7925H | United States | United Launch Alliance | 2,171 to GTO 1,508 to HCO[note 2][7] |
3[7] | Operational [citation needed][note 3] |
2003 | ||||
Delta IV-H | United States | United Launch Alliance | 22,950[8] | 12,980 to GTO [8] | 5 | Operational | 2004 | |||
Delta IV-M+(4,2) | United States | United Launch Alliance | 11,750[9] | 5,740 to GTO[9] | 8[10] | Operational | 2002 | |||
Delta IV-M+(5,2) | United States | United Launch Alliance | 10,250[9] | 4,590 to GTO[9] | 0[10] | Operational |
| |||
Delta IV-M+(5,4) | United States | United Launch Alliance | 13,500[9] | 16,470 to GTO[9] | 1[10] | Operational | 2009[11] | |||
Dnepr-1 | Ukraine | Yuzhmash | 3,700[12] | €10 million.[13] | 16 | Operational | 1999 | |||
Falcon 9 | United States | SpaceX | 10,450[14][15] | 4,680 to GTO[14] | 56[14] | 5,359 | 2 | Operational | 2010 | |
H-IIA 202 | Japan | Mitsubishi Heavy Industries | 10,000[16] | 3,800 to GTO[16] | 7[16] | Operational | 2001 | |||
H-IIA 204 | Japan | Mitsubishi Heavy Industries | 5,800 to GTO[16] | 1[16] | Operational | 2006 | ||||
H-IIB 304 | Japan | Mitsubishi Heavy Industries | 19,000[17] | 8,000[18] | 2[19] | Operational | 2009 | |||
Long March 3B | China | CALT | 5,100[citation needed] | 10 | Operational | 1996 | ||||
Long March 3B/E | China | CALT | 11,500[citation needed] | 5,500[citation needed] | 4 | Operational | 2007 | |||
Proton | Soviet Union Russia |
Khrunichev | 21,600[20] | 6,360 to GTO[20] | 85 [21] | 4,302[21] | 335 [22] | Operational | 1965 | |
PSLV | India | ISRO | 3,200[23] | 1,600 to SSO 1,050 to GTO[24] |
11 | Operational | 1993 | |||
PSLV-CA | India | ISRO | 2,800[23] | 1,100 to SSO[24] | 6 | Operational | 2007 | |||
PSLV-XL | India | ISRO | 3,800[24] | 1,750 to SSO 1300 to GTO[24] |
2 | Operational | 2008 | |||
Zenit-2M (2SLB) | Ukraine | Yuzhnoye | 13,920[25] | 1 | Operational | 2007 |
Orbital Launch Vehicles In Development
Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Cost (Mil US$) |
Cost/kg (LEO) (US$) |
Launches | Status | First flight | Last flight |
---|---|---|---|---|---|---|---|---|---|---|
Angara 1.2 | Russia | Khrunichev | 3,800[26] | 0 | Development | |||||
Angara A3 | Russia | Khrunichev | 14,600[26] | 2,400-3,600 to GTO[26] | €50 million[13] | 0 | Development | |||
Angara A5 | Russia | Khrunichev | 24,500 (63°) [27][28] | 0 | Development | |||||
Angara A7 | Russia | Khrunichev | 41,000[27][28] | 0 | Development | |||||
Falcon Heavy | United States | SpaceX | 53,000[29] | 19,000 to GTO[29] 16,000 to TLI[29] |
80-125 | 2,204 | 0 | Development | ||
GSLV Mk.III | India | ISRO[30] | 10,000 | 4,500 - 5,000[31] | 0 | Development | ||||
Long March 2F/G | China | CALT | 0 | Development | ||||||
Rus-M | Russia | TsSKB-Progress | 35,500-54,000 [32][33] | 7,500-11,500 to GTO[32][34] | 0 | Development [note 4] |
||||
Space Launch System | United States | Alliant Techsystems (SRBs) Lockheed Martin Stage I |
70,000 — 130000[35] | 0 | Development |
Retired Launch Vehicles
Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Cost (Mil US$) |
Cost/kg (LEO) (US$) |
Launches | Status | First flight | Last flight |
---|---|---|---|---|---|---|---|---|---|---|
Ariane 1 | Europe | Aérospatiale | 1,400 | 1,830 to GTO[36] | 11[36] | Retired | 1979 | 1986 | ||
Ariane 2 | Europe | Aérospatiale | 2,270 to GTO[36] | 6[36] | Retired | 1986 | 1989 | |||
Ariane 3 | Europe | Aérospatiale | 2,650 to GTO[36] | 11[36] | Retired | 1984 | 1989 | |||
Ariane 4 40 | Europe | Aérospatiale | 4,600[36] | 2,740 to SSO 1,900 to GTO[36] |
3[36] | Retired | 1990 | 1993 | ||
Ariane 4 40 H10+ | Europe | Aérospatiale | 2,020 to GTO[36] | 1[36] | Retired | 1995 | 1995 | |||
Ariane 4 40 H10-3 | Europe | Aérospatiale | 2,105 to GTO[36] | 3[36] | Retired | 1995 | 2009 | |||
Ariane 4 42L | Europe | Aérospatiale | 7,000[36] | 4,500 to SSO 3,200 to GTO[36] |
1[36] | Retired | 1993 | 1993 | ||
Ariane 4 42L H10+ | Europe | Aérospatiale | 7,000[36] | 3,350 to GTO[36] | 1[36] | Retired | 1994 | 1994 | ||
Ariane 4 42L H10-3 | Europe | Aérospatiale | 7,000[36] | 3,480 to GTO[36] | 11[36] | Retired | 1995 | 2002 | ||
Ariane 4 42P | Europe | Aérospatiale | 6,000[36] | 3,400 to SSO 2,600 to GTO[36] |
2[36] | Retired | 1990 | 1992 | ||
Ariane 4 42P H10+ | Europe | Aérospatiale | 2,740 to GTO[36] | 4[36] | Retired | 1992 | 1994 | |||
Ariane 4 42P H10-3 | Europe | Aérospatiale | 2,930 to GTO[36] | 9[36] | Retired | 1994 | 2002 | |||
Ariane 4 44L | Europe | Aérospatiale | 7,000[36] | 6,000 to SSO 4,200 to GTO[36] |
11[36] | Retired | 1989 | 1992 | ||
Ariane 4 44L H10+ | Europe | Aérospatiale | 7,000[36] | 4,460 to GTO[36] | 5[36] | Retired | 1992 | 1994 | ||
Ariane 4 44L H10-3 | Europe | Aérospatiale | 7,000[36] | 4,720 to GTO[36] | 24[36] | Retired | 1995 | 2003 | ||
Ariane 4 44LP | Europe | Aérospatiale | 7,000[36] | 5,000 to SSO 3,700 to GTO[36] |
7[36] | Retired | 1988 | 1993 | ||
Ariane 4 44LP H10+ | Europe | Aérospatiale | 7,000[36] | 4,030 to GTO[36] | 6[36] | Retired | 1992 | 1995 | ||
Ariane 4 44LP H10-3 | Europe | Aérospatiale | 7,000[36] | 4,220 to GTO[36] | 13[36] | Retired | 1995 | 2001 | ||
Ariane 4 44P | Europe | Aérospatiale | 6,500[36] | 4,100 to SSO 3,000 to GTO[36] |
2[36] | Retired | 1991 | 1991 | ||
Ariane 4 44P H10-3 | Europe | Aérospatiale | 3,465 to GTO[36] | 9[36] | Retired | 1995 | 2001 | |||
Ariane 5G | Europe | EADS Astrium | 18,000[4] | 6,900[4] | 16[4] | Retired[37] | 1996 | 2003 | ||
Ariane 5G+ | Europe | EADS Astrium | 18,000 | 7,100 to GTO [4] | 3[4] | Retired[37] | 2004 | 2004 | ||
Ariane 5GS | Europe | EADS Astrium | 18,000 | 6,600 to GTO [4] | 6[4] | Retired[37] | 2005 | 2009 | ||
Atlas G | United States | Lockheed | 5,900[38] | 2,222 to GTO 1,179 to HCO[38] |
7[38] | Retired | 1984 | 1989 | ||
Atlas H/MSD | United States | Lockheed | 5 | Retired | 1983 | 1987 | ||||
Atlas I | United States | Lockheed Martin | 5,900[38] | 2,340[38] | 11[38] | Retired | 1990 | 1997 | ||
Atlas II | United States | Lockheed Martin | 6,780[38] | 2,810 to GTO 2,000 to HCO[38] |
10[38] | Retired | 1991 | 1998 | ||
Atlas IIA | United States | Lockheed Martin | 7,316[38] | 3,180 to GTO 2,160 to HCO[38] |
23[38] | Retired | 1992 | 2002 | ||
Atlas IIAS | United States | Lockheed Martin | 8,618[38] | 3,833 to GTO 2,680 to HCO[38] |
30[38] | Retired | 1993 | 2004 | ||
Atlas IIIA | United States | Lockheed Martin | 8,686[38] | 4,060 to GTO 2,970 to HCO[38] |
2[38] | Retired | 2000 | 2004 | ||
Atlas IIIB/DEC | United States | Lockheed Martin | 10,759[38] | 4,609 to GTO[38] | 1[38] | Retired | 2002 | 2002 | ||
Atlas IIIB/SEC | United States | Lockheed Martin | 4,193 to GTO [38] | 3[38] | Retired | 2003 | 2005 | |||
Delta 0900 | United States | McDonnell Douglas | 1,300[39] | 818 to SSO[7] | 2[7] | Retired | 1972 | 1972 | ||
Delta 1410 | United States | McDonnell Douglas | 1[7] | Retired | 1975 | 1975 | ||||
Delta 1604 | United States | McDonnell Douglas | 2[7] | Retired | 1972 | 1973 | ||||
Delta 1900 | United States | McDonnell Douglas | 1,800[7] | 1[7] | Retired | 1973 | 1973 | |||
Delta 1910 | United States | McDonnell Douglas | 1[7] | Retired | 1975 | 1975 | ||||
Delta 1913 | United States | McDonnell Douglas | 1[7] | Retired | 1973 | 1973 | ||||
Delta 1914 | United States | McDonnell Douglas | 2[7] | Retired | 1972 | 1973 | ||||
Delta 2310 | United States | McDonnell Douglas | 3[7] | Retired | 1974 | 1981 | ||||
Delta 2313 | United States | McDonnell Douglas | 3[7] | Retired | 1974 | 1977 | ||||
Delta 2910 | United States | McDonnell Douglas | 1,887[7] | 6[7] | Retired | 1975 | 1978 | |||
Delta 2913 | United States | McDonnell Douglas | 2,000[40] | 700 to GTO[40] | 6[7] | Retired | 1975 | 1976 | ||
Delta 2914 | United States | McDonnell Douglas | 724 to GTO[7] | 30[7] | Retired | 1974 | 1979 | |||
Delta 3910 | United States | McDonnell Douglas | 2,494[7] | 1,154 to GTO with PAM-D[7] | 10[7] | Retired | 1980 | 1988 | ||
Delta 3913 | United States | McDonnell Douglas | 1[7] | Retired | 1981 | 1981 | ||||
Delta 3914 | United States | McDonnell Douglas | 954 to GTO[7] | 13[7] | Retired | 1975 | 1987 | |||
Delta 3920 | United States | McDonnell Douglas | 3,452[7] | 1,284 to GTO with PAM-D[7] | 10[7] | Retired | 1982 | 1989 | ||
Delta 3924 | United States | McDonnell Douglas | 1,104 to GTO[7] | 4[7] | Retired | 1982 | 1984 | |||
Delta 4925 | United States | McDonnell Douglas | 3,400[41] | 1,312 to GTO[7] | 2[7] | Retired | 1989 | 1990 | ||
Delta 5920 | United States | McDonnell Douglas | 3,848[42] | 1[7] | Retired | 1989 | 1989 | |||
Delta II 6920 | United States | McDonnell Douglas | 3,983[7] | 3[7] | Retired | 1990 | 1992 | |||
Delta II 6925 | United States | McDonnell Douglas | 1,447 to GTO[7] | 14[7] | Retired | 1989 | 1992 | |||
Delta II 7320 | United States | United Launch Alliance | 2,865[note 2][7] | 1,651 to SSO[note 2][7] | 10[7] | Retired | 1999 | 2011 | ||
Delta II 7326 | United States | Boeing IDS | 934 to GTO 636 to TLI 629 to HCO[note 2][7] |
3[7] | Retired | 1998 | 2011 | |||
Delta II 7420 | United States | United Launch Alliance | 3,185[note 2][7] | 1,966 to SSO[note 2][7] | 13[7] | Retired | 1998 | 2010 | ||
Delta II 7425 | United States | Boeing IDS | 1,100 to GTO 804 to HCO[note 2][7] |
4[7] | Retired | 1998 | 2002 | |||
Delta II 7426 | United States | Boeing IDS | 1,058 to GTO 734 to TLI 711 to HCO[note 2][7] |
1[7] | Retired | 1999 | 1999 | |||
Delta II 7925 | United States | Boeing IDS | 1,819 to GTO 1,177 to TLI 1,265 to HCO[note 2][7] |
69[7] | Retired | 1990 | 2009 | |||
Delta III 8930 | United States | Boeing IDS | 8,292[7] | 3,810 to GTO[7] | 3[7] | Retired | 1998 | 2000 | ||
Delta IV-M | United States | Boeing IDS | 8,120[10] | 4,210 to GTO 2,722 to escape[10] |
3[10] | Retired | 2003 | 2006 | ||
Energia[note 5] | Soviet Union | NPO Energia | 100,000[43] | 20000 to GTO[43] 32,000 to TLI[43] |
240[note 6] | 1[44] | Retired | 1987 | 1987 | |
Energia-Buran | Soviet Union | NPO Energia (Launcher) NPO Molniya (Orbiter) |
30,000[43] [note 7] |
1 | Retired | 1988 | 1988 | |||
H-II | Japan | Mitsubishi Heavy Industries | 5[45][note 8] | Retired | 1994 | 1998 | ||||
H-IIA 2022 | Japan | Mitsubishi Heavy Industries | 4,200[16] | 3[16] | Retired | 2005 | 2007 | |||
H-IIA 2024 | Japan | Mitsubishi Heavy Industries | [16] | 7[16] | Retired | 2002 | 2008 | |||
H-II/SSB | Japan | Mitsubishi Heavy Industries | 1[45] | Retired | 1995 | 1995 | ||||
H-IIS | Japan | Mitsubishi Heavy Industries | 1[note 9][45] | Retired | 1999 | 1999 | ||||
N1 | Soviet Union | NPO Energia | 95,000 [46][47][48][note 10] | 4 [49] | Retired | 1969 | 1972 | |||
Saturn IB | United States | Chrysler (S-IB) Douglas (S-IVB) |
20,412[citation needed] | 9[50] | Retired | 1966 | 1975 | |||
Saturn V | United States | Boeing (S-IC) North American (S-II) Douglas (S-IVB) |
118,000[51] | 47,000 to TLI[51] | 185 (1.54 billion in 2024)[52] | 13[53][54][note 11] | Retired | 1967 | 1973 | |
Space Shuttle | United States | Alliant Techsystems (SRBs) Martin Marietta (ET) Rockwell International (Orbiter) |
24,400[note 7] | 300 [21] | 10,416 [21] | 135[55] | Retired | 1981 | 2011 | |
Titan IIIC | United States | Martin Marietta | 36 | Retired | 1965 | 1982 | ||||
Titan IIID | United States | Martin Marietta | 22 | Retired | 1971 | 1982 | ||||
Titan IIIE | United States | Martin Marietta | 7 | Retired | 1974 | 1977 | ||||
Titan 34D | United States | Martin Marietta | 15 | Retired | 1982 | 1989 | ||||
Titan IVA | United States | Martin Marietta | Retired | 1989 | 1998 | |||||
Titan IVB | United States | Lockheed Martin | 21,682[56] | 5,761} to GTO [56] (9,000 with upper stage) |
432 | 39 | Retired | 1997 | 2005 | |
Zenit-2 | Soviet Union Ukraine |
Yuzhnoye | 13,740[25] | 37[19] | Retired | 1985 | 2004[57] |
References
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- ^ a b c d e f g h http://space.skyrocket.de/doc_lau/ariane5.htm
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- ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai aj ak al am an ao ap aq ar as at au av aw ax ay az ba bb bc bd be bf Cite error: The named reference
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- ^ a b c d e f Space launch report -Delta4
- ^ a b c d e f Gunter, Krebs. "Delta-4". Gunter's Space Page. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ New communications craft launched for U.S. military, Spaceflight Now, 5 Dec 2009
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was invoked but never defined (see the help page). - ^ a b "Proton Launch System Mission Planner's Guide, LKEB-9812-1990" (PDF). International Launch Services. pp. 2–2. Archived from the original on 2007-10-27. Retrieved 2007-11-12.
LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
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- ^ a b Семейство ракет-носителей «Ангара», date unknown, Retrieved 2010-08-09.
- ^ a b http://www.russianspaceweb.com/angara7.html
- ^ a b c "SpaceX Brochure" (PDF). Retrieved 14 June 2011.
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naa
was invoked but never defined (see the help page). - ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai aj ak al am an ao ap aq ar as at au av aw ax ay az Gunter, Krebs. "Ariane-1, -2, -3, -4". Gunter's Space Page. Retrieved 2 August 2011.
- ^ a b c Flight V193 was the seventh Ariane 5 launch of 2009 and used the last of the GS version of the launcher.
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- ^ Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ a b c d "S.P.Korolev RSC Energia - LAUNCHERS". Energia.
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- ^ Cite error: The named reference
refN1-1
was invoked but never defined (see the help page). - ^ Cite error: The named reference
refN1-2
was invoked but never defined (see the help page). - ^ Cite error: The named reference
refN1-3
was invoked but never defined (see the help page). - ^ Cite error: The named reference
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was invoked but never defined (see the help page). - ^ Bilstein, Roger E. "Appendix C: Saturn Family/Mission Data". Stages to Saturn A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Office. Retrieved 7 April 2011.
- ^ a b Cite error: The named reference
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was invoked but never defined (see the help page). - ^ "SP-4221 The Space Shuttle Decision- Chapter 6: ECONOMICS AND THE SHUTTLE". NASA. Retrieved 2011-01-15.
- ^ Cite error: The named reference
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was invoked but never defined (see the help page). - ^ Cite error: The named reference
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was invoked but never defined (see the help page). - ^ [http://www.nasa.gov/mission_pages/shuttle/main/index.html
- ^ a b "Fact Sheet - TITAN IVB". United States Air Force. Retrieved 2007-11-12.
- ^ Zenit launch log
Cite error: There are <ref group=note>
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