Small-lift launch vehicle
| Class overview | |
|---|---|
| Name | Small-lift launch vehicle |
| Preceded by | Sounding rocket |
| Succeeded by | Medium-lift launch vehicle |
| Built | Since 1957 |
| General characteristics | |
| Capacity |
|
A small-lift launch vehicle is a rocket orbital launch vehicle that is capable of lifting 2,000 kilograms (4,400 lb) or less (by NASA classification) or under 5,000 kilograms (11,000 lb) (by Roscosmos classification)[1] of payload into low Earth orbit (LEO). Small launch vehicles can meet the requirements of some spacecraft and can be less expensive than a larger launch vehicle would be.[2] The next larger category is medium-lift launch vehicles.[3]
History
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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.[4][5][6] The US responded by attempting to launch the Vanguard rocket.[7][8] However, the Vanguard TV3 launch attempt failed, with the 31 January 1958 launch of the Explorer 1 satellite using the Juno I rocket being the first successful US orbital launch. The Vanguard I mission was the second successful US orbital launch. This was the start of the space race.[9][10]
Since the late 1950s, small-lift launch vehicles have continued launching payloads into orbits including LEO, Sun-synchronous orbit (SSO), and geostationary transfer orbit (GTO). Medium-lift launch vehicles, heavy-lift launch vehicles, and super heavy-lift launch vehicles have also been extensively developed but have not completely superseded small launch vehicles.
Rated launch vehicles
Operational
| Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Launches | First flight |
|---|---|---|---|---|---|---|
| Qased | IRGCASF | 10−50 | 3 | 2020 | ||
| Qaem 100 | IRGC | 80[11] | 3(+1) | 2023 | ||
| HANBIT-NANO | Innospace | 90[12] | 1 | 2025 | ||
| SK solid fueled TV2 | MND | >100 | 1 | 2023 | ||
| Shavit 2 | IAE | 160[13] | 12 | 1988 | ||
| Unha | KCST | 200[14] | 4 | 2009 | ||
| OS-M[a] | OneSpace | 205[15] | 73 to SSO | 1 | 2019 | |
| KAIROS | Space One | 250 | 150 to SSO | 1 | 2024 | |
| Electron | Rocket Lab | 300[16] | 200 to SSO[16] | 62 | 2017 | |
| Jielong 1 | CALT | 200 to SSO | 1[17] | 2019 | ||
| Hyperbola-1 | i-Space | 300[18] | 6 | 2020 | ||
| Chollima-1 | NADA | ≥300[19] | 3 | 2023 | ||
| Simorgh | Iranian Space Agency | 350[20] | 6(+1) | 2016 | ||
| Ceres-1 | Galactic Energy | 350[21] | 11 | 2020 | ||
| Kuaizhou-1 | CASC | 400[22] | 250 to SSO | 28[b] | 2013[22] | |
| SSLV | ISRO / NSIL | 500 | 300 to SSO | 2 | 2022 | |
| Start-1 | MITT | 532[23] | 350 to SSO[24] | 5[25] | 1993 | |
| Minotaur I | Northrop Grumman | 580[26] | 12[27] | 2000 | ||
| Long March 6 | CALT | 500 to SSO | 11 | 2015 | ||
| Long March 11 | CALT | 700[28] | 17 | 2015[29] | ||
| Alpha | Firefly | 1,000[30] | 600 to SSO | 5 | 2021 | |
| Spectrum | Isar Aerospace | 1,000 | 700 to SSO | 1 | 2025 | |
| Epsilon | IHI[31] | 1,200[32] | 5 | 2013 | ||
| RS1 | ABL | 1,350[33] | 400 to GTO | 1 | 2023 | |
| Strela | Khrunichev | 1,400[34] | 3[35] | 2003 | ||
| Minotaur-C | Northrop Grumman | 1,450[36] | 1,050[36] to SSO | 10[37] | 1994 | |
| Kuaizhou-11 | CASC | 1,500 | 1,000 to SSO | 2 | ||
| SK solid fueled LV | MND | 1,500 | 1(+2) | 2023[38] | ||
| Minotaur IV | Northrop Grumman | 1,735[39] | 7[40] | 2010[41] | ||
| Kinetica 1 | CAS Space | 2,000 | 1,500 to SSO | 3 | 2022 | |
| Tianlong-2 | Space Pioneer | 2,000[42] | 1,500 to SSO | 1 | 2023 | |
| Jielong 3 | CALT | 1,500 to SSO | 3[43] | 2022 | ||
| Tundra | NordSpace | 500 | 250 to SSO | 1 | 2025 |
Under development
| Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
First flight
(expected) |
|---|---|---|---|---|---|
| Blue Whale 1 | Perigee Aerospace | 63[44] | 50 to SSO | TBD | |
| Agnibaan | Agnikul Cosmos | 100 | TBD | ||
| ZERO | Interstellar Technologies | 100 to SSO[45] | 2027[46] | ||
| VLM[47] | Brazilian General Command for Aerospace Technology | 150 | 2028 | ||
| DNLV | Independence-X Aerospace[48] | 200 | 2029 | ||
| Volans | Equatorial Space Systems[49] | 220 | 150 to SSO | TBD | |
| Zuljanah | Iranian Space Agency | 220 | TBD | ||
| Vikram 1 | Skyroot Aerospace | 315 | 255 to SSO[50] | TBD | |
| Skyrora XL | Skyrora | 315[51] | 2027[52] | ||
| Hapith V | TiSPACE | 390[53] | 350 to SSO | ||
| Ravn X SL3 | Aevum Space & Defense | 500[54] | 470 to SSO | 2026 | |
| Vikram II | Skyroot Aerospace | 520 | 410 to SSO[50] | TBD | |
| Rocket 4 | Astra Space, Inc. | 600[55] | 2026 | ||
| Vikram III | Skyroot Aerospace | 720 | 580 to SSO[50] | TBD | |
| Tronador II | VENG | 750[56] | 2029 | ||
| Miura 5 | PLD Space | 900 | 2026 | ||
| RFA One | Rocket Factory Augsburg | 1,600 | 1,300 | 2026 |
Retired
Notes
- ^ OS-M1 Variant of OS-M was launched
- ^ Includes 2 Kuaizhou-1 launches and 26 Kuaizhou-1A launches.
- ^ The lead manufacturer is from Italy, but the rocket has significant contributions from companies based in Belgium, France, Netherlands, Spain, Switzerland and Ukraine.
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) to low Earth orbit
- 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.


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