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) of payload into low Earth orbit (LEO). The next larger category consists of medium-lift launch vehicles.[1]
The first small-lift launch vehicle was the Sputnik rocket, which was derived from the R-7 Semyorka ICBM of the Soviet Union. On 4 October 1957, the rocket was used to perform the world's first satellite launch, placing Sputnik 1 satellite into a low Earth orbit.[2][3][4] The USA responded by attempting to launch the Vanguard rocket.[5][6] However, the Vanguard TV3 launch failed, with the 3 January 1958 launch of the Explorer 1 satellite using a Juno I rocket the first successful US orbital launch. Vanguard I was the second successful U.S. orbital launch. This was the start of the space race.[7][8]
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launch vehicles, and super heavy-lift launch vehicles have also been extensively developed but have not completely superseded the small vehicles. Small vehicles can meet the requirements of some spacecraft, and can be less expensive than larger vehicles.[citation needed]
Rated launch vehicles
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
References
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Notes
Further reading
- Isakowitz, Hopkins, and Hopkins International Guide to Space Launch Systems, AIAA. ISBN 1-56347591-X.