Small-lift launch vehicle
A small-lift launch vehicle is a rocket orbital launch vehicle that is capable of lifting up to 2,000 kg (4,400 lb) (by NASA classification) or up to 5,000 kilograms (11,000 lb) (by ROSCOSMOS classification)[1] of payload into low Earth orbit (LEO). The next larger category consists of medium-lift launch vehicles.[2]
The first small-lift launch vehicle was the Sputnik rocket, launched by the Soviet Union, which was derived from the R-7 Semyorka ICBM. On 4 October 1957, the Sputnik rocket was used to perform the world's first satellite launch, placing the Sputnik 1 satellite into a low Earth orbit.[3][4][5] NASA responded by attempting to launch the Vanguard rocket.[6][7] However, the Vanguard TV3 launch attempt failed, with the 31 January 1958 launch of the Explorer 1 satellite using the Juno I rocket being first successful NASA orbital launch. The Vanguard I mission was the second successful NASA orbital launch. This was the start of the space race.[8][9]
Since the late 1950s, small-lift launch vehicles have continued launching payloads to space. Medium-lift launch vehicles, heavy-lift launch vehicles, and super heavy-lift launch vehicles have also been extensively developed but have not completely been able to supersede the small launch vehicles. Small launch vehicles can meet the requirements of some spacecraft, and can also be less expensive than a larger launch vehicle would be.[citation needed]
Rated launch vehicles[]
Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Launches | Status | First flight | Last flight | Mission cost |
---|---|---|---|---|---|---|---|---|---|
SS-520 | Japan | IHI | 4 | 2 | Retired | 2017 | 2018 | $4.5M[10] | |
Vanguard | United States | Martin | 9[11] | 11(+1) | Retired | 1957 | 1959 | ||
Juno I[12] | United States | Chrysler | 11 | 6 | Retired | 1958 | 1959 | ||
Juno II[13] | United States | Chrysler | 41 | 10 | Retired | 1958 | 1961 | ||
Atlas LV-3B[14] | United States | Convair | 1,360 | 9 | Retired | 1960 | 1963 | ||
Conestoga | United States | Space Services Inc. | 500[15] | 3 | Retired | 1982 | 1995 | ||
Qased | Iran | IRGCASF | 10∼50 | 1 | Operational | 2020 | |||
United States | [16] | 12 | 0 | Development | |||||
Lambda 4S | Japan | Nissan Motors[17] | 26[18] | 5 | Retired | 1966 | 1977[19] | ||
SLV | India | ISRO | 40[20] | 4 | Retired | 1979 | 1983 | ||
Safir | Iran | Iranian Space Agency | 50[21] | 8 | Retired | 2008 | 2019 | ||
Vector-R | United States | Vector Space Systems | 60[22] | 0(+2) | Defunct | (2019) | |||
Blue Whale 1 | South Korea | Perigee Aerospace | 63[23] | 50 to SSO | 0 | Development | (2020) | ||
Black Arrow | United Kingdom | RAE | 73[24] | 4 | Retired | 1969[note 1] | 1971 | ||
Miura 1 | Spain | PLD Space | 100[25] | 0 | Development | 2020-2021 | |||
United States | ABL Space | 1,350 | 0 | Development | 2020-2021 | $12M(2020) | |||
Simorgh | Iran | Iranian Space Agency | 350[26] | 4 | Operational | 2016 | |||
Naro-1 | South Korea Russia |
KARI/Khrunichev | 100[27] | 3 | Retired | 2009 | 2013 | ||
Volna | Russia | Makeyev | 100[28] | 1(+5)[29] | Retired | 1995[note 2] | 2005[29] | ||
Kaituozhe-1 | China | CALT | 100[30] | 2 | Retired | 2002 | 2003[31] | ||
Diamant | France | SEREB | 107[32][33] | 12 | Retired | 1965 | 1975 | ||
Vector-H | United States | Vector Space Systems | 110[34] | 0 | Defunct | ||||
ASLV | India | ISRO | 150 | 4 | Retired | 1987 | 1994 | ||
Shavit 2 | Israel | IAE | 160[35] | 10 | Operational | 1988 | |||
Scout | United States | US Air Force/NASA | 174[36] | 125 | Retired | 1961 | 1994 | ||
Mu-4S | Japan | Nissan Motors[17] | 180[18] | 4 | Retired | 1971 | 1972 | ||
Mu-3C | Japan | Nissan Motors[17] | 195[18] | 4 | Retired | 1974 | 1979 | ||
Unha | North Korea | KCST | 200[37] | 3 | Operational | 2009 | |||
Zuljanah | Iran | Iranian Space Agency | 220 | 1 | Development | 2021 | |||
ZERO | Japan | Interstellar Technologies | 100 to SSO[38] | 0 | Development | (2022) | |||
Skyrora XL | United Kingdom | Skyrora | 315[39] | 0 | Development | (2023)[40] | |||
Vikram I | India | Skyroot Aerospace | 315 | 255 to SSO[41] | 0 | Development | (2021) | ||
Vikram II | India | Skyroot Aerospace | 520 | 410 to SSO[41] | 0 | Development | TBD | ||
Vikram III | India | Skyroot Aerospace | 720 | 580 to SSO[41] | 0 | Development | TBD | ||
Tronador II | Argentina | CONAE | 250[42] | 0 | Development | 2020 | |||
Shtil' | Russia | Makeyev | 280 – 420[43] | 2[29] | Retired | 1998 | 2006 | ||
Mu-3H | Japan | Nissan Motors[17] | 300[18] | 3 | Retired | 1977 | 1978 | ||
Mu-3S | Japan | Nissan Motors[17] | 300[18] | 4 | Retired | 1980 | 1984 | ||
Long March 1 (CZ-1) | China | CALT | 300[44] | 2[45] | Retired[46] | 1970[45] | 1971[45] | ||
Miura 5 | Spain | PLD Space | 300[47] | 0 | Development | 2022 | |||
Capricornio[48] | Spain | Instituto Nacional de Técnica Aeroespacial | 140 | 0 | Canceled | ||||
Electron | New Zealand United States |
Rocket Lab | 300[49] | 200 to SSO[49] | 17 | Operational | 2017 | $7.5M (2019)[50] | |
Delta 1913 | United States | McDonnell Douglas | 328[51] | 1[52] | Retired | 1973 | 1973 | ||
Delta 2310 | United States | McDonnell Douglas | 336[53] | 3[52] | Retired | 1974 | 1981 | ||
Delta 1410 | United States | McDonnell Douglas | 340[54] | 1[52] | Retired | 1975 | 1975 | ||
VLS-1 | Brazil | AEB, INPE | 380[55] | 2[note 3] | Retired | 1997 | 2003 | ||
VLM (rocket)[56] | Brazil | Brazilian General Command for Aerospace Technology | 150 | 0 | Development | 2022 | |||
Delta 1604 | United States | McDonnell Douglas | 390[57] | 2[52] | Retired | 1972 | 1973 | ||
Taiwan | TiSPACE | 390[58] | 350 to SSO | 0 | Development | (2020) | |||
Kuaizhou-1 | China | CASC | 400[59] | 3[59] | Operational | 2013[59] | |||
Falcon 1 | United States | SpaceX | 420[60] | 5 | Retired[61] | 2006 | 2009 | ||
Pegasus | United States | Orbital | 443[62] | 43[63] | Operational | 1990 | $56M (2014) [64] | ||
Sputnik 8K71PS | Soviet Union | RSC Energia | 500[65] | 2 | Retired | 1957 | 1957 | ||
Launcher One | United States | Virgin Orbit | 500[66] | 300 to SSO | 2 | Operational | 2020 | $12M (2020)[67] | |
Boeing Small Launch Vehicle[68] | United States | Boeing | 45[69] | 0 | Development | ||||
SSLV | India | ISRO / | 500 | 300 to SSO | 0 | Development | |||
Start-1 | Russia | MITT | 532[70] | 350 to SSO[71] | 5[72] | Operational | 1993 | ||
Minotaur I | United States | Orbital | 580[73] | 11[74] | Operational | 2000 | $28.8M (2013) [75] | ||
Long March 6 | China | CALT | 500 to SSO | 2 | Operational | 2015 | |||
Long March 11 | China | CALT | 700[76] | 3 | Operational | 2015[77] | |||
Paektusan | North Korea | KCST | 700[78] | 1 | Retired | 1998 | |||
Long March 1D(CZ-1D) | China | CALT | 740[79] | 0(+3) | Retired | 1995[note 4] | 2002 | ||
Mu-3SII | Japan | Nissan Motors[17] | 770[18] | 8 | Retired | 1985 | 1995 | ||
Athena I | United States | Lockheed Martin | 795[80] | 515 to GTO | 4[81] | Retired | 1995 | 2001 | $17M (2000)[82] |
Delta 3913 | United States | McDonnell Douglas | 816[83] | 1[52] | Retired | 1981 | 1981 | ||
Alpha | United States | Firefly Aerospace | 1,000[84] | 600 to SSO | 0 | Development | $15M(2020) [85] | ||
J-I | Japan | IHI Corporation Nissan Motors[17] |
1,000[86] | 0(+1) | Retired | 1996 | 1996 | ||
Delta 1910 | United States | McDonnell Douglas | 1,066[87] | 1[52] | Retired | 1975 | 1975 | ||
Terran 1 | United States | Relativity Space | 1,250[88] | 1[52] | Development | $10M(2019)[89] | |||
N-I | Japan United States |
Mitsubishi Heavy Industries | 1,200[90] | 7 | Retired | 1975 | 1982[citation needed] | ||
Epsilon | Japan | IHI Aerospace[91] | 1,200[18] | 4 | Operational[18] | 2013 | $38M[92] | ||
Delta 0900 | United States | McDonnell Douglas | 1,300[93] | 818 to SSO[52] | 2[52] | Retired | 1972 | 1972 | |
Sputnik 8A91 | Soviet Union | RSC Energia | 1,327 | 2 | Retired | 1958 | 1958 | ||
Strela | Russia | Khrunichev | 1,400[94] | 3[95] | Operational[95] | 2003 | |||
H-I | Japan United States |
Mitsubishi Heavy Industries | 1,400[96] | 9 | Retired | 1986 | 1992 | ||
Minotaur-C | United States | Orbital | 1,450[97] | 1,050[97] to SSO | 10[98] | Operational[99] | 1994 | $45M[100] | |
Kosmos-3M | Soviet Union Russia |
NPO Polyot | 1,500[101] | 442[102] | Retired | 1967 | 2010 | ||
Kuaizhou-11 | China | CASC | 1,500 | 0 | Development | ||||
Minotaur IV | United States | Orbital | 1,735[103] | 4(+2)[104] | Operational | 2010[104] | $50M[105] | ||
M-V | Japan | Nissan Motors[17] (−2000) IHI AEROSPACE[91] (−2006) |
1,800 – 1,850[18] | 7 | Retired | 1997 | 2006 | ||
Athena II | United States | Lockheed Martin | 1,800[106] | 3[107] | Retired[108] | 1998 | 1999 | $46M (2014)[109] | |
Delta 1900 | United States | McDonnell Douglas | 1,800[52] | 1[52] | Retired | 1973 | 1973 | ||
Delta 2910 | United States | McDonnell Douglas | 1,887[52] | 6[52] | Retired | 1975 | 1978 | ||
Rokot | Russia | Khrunichev | 1,950[110] | 1,200 to SSO | 34 | Retired | 1990 | 2019 | $41M |
Vega | Italy | Avio | 1,450 to SSO | 15 | Operational | 2012 | $37M[100] | ||
Haribon SLS-1 | Philippines | OrbitX | 200[111] | 0 | Development | (2023–2024) | |||
Singapore | Equatorial Space Systems[112] | 220 | 150 to SSO | 0 | Development | (2023) |
See also[]
- Sounding rocket, suborbital launch vehicle
- Medium-lift launch vehicle, capable of lifting between 2,000 and 20,000 kg to low Earth orbit
- Heavy lift launch vehicle, capable of lifting between 20,000 and 50,000 kg to low Earth orbit
- Super heavy-lift launch vehicles, capable of lifting more than 50,000 kg (110,000 lb) of payload into LEO
- Comparison of orbital launch systems
- List of orbital launch systems
- Comparison of orbital rocket engines
- Comparison of space station cargo vehicles
- Rocket
- Spacecraft propulsion
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Notes[]
Further reading[]
- Isakowitz, Hopkins, and Hopkins International Guide to Space Launch Systems, AIAA. ISBN 1-56347591-X.
External links[]
- Space launch vehicles
- Microsatellite launch vehicles