KVD-1

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KVD-1 (12KRB)
Country of origin USSR/Russia
First flight 2001-04-20, GSAT-1 Mission, GSLV debut flight
Last flight 2010-12-25, GSAT-5P launch, GSLV Mk I final flight
Designer KB KhIMMASH
Application Upper stage engine
Associated L/V GSLV Mk 1
Status Retired
Liquid-fuel engine
Propellant Liquid oxygen / Liquid hydrogen
Mixture ratio 6
Cycle Staged combustion
Configuration
Chamber 1 + 2 verniers
Performance
Thrust (vac.) 69.6 kN (15,600 lbf)
Chamber pressure 5.6 MPa (810 psi)
Isp (vac.) 462s
Burn time 800s (600s in a single burn)
Gimbal range None; uses 2 vernier engines for attitude control[1]
Dimensions
Length 2.14 m (7 ft 0 in)
Diameter 1.58 m (5 ft 2 in)
Dry weight 282 kg (622 lb)
References
References [2][3][4]

KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s. It is a modified version of RD-56 which was developed with an intention to manufacture cryogenic engine for upper stage of Lunar N-1 launch vehicle. It was to be used in USSR moon missions.[5][unreliable source?] KVD-1 can produce engine thrust of 7.5 tonnes.

Initial Development

KVD-1 was originated from the RD-56 engine which were intended to be used for USSR moon programmes.[6] RD-56 aka 11D56 engines were developed for N1M rocket programme, the planned derivative of N1, but later they were abandoned due to four successive launch failures of N1.[7] Later the design of the engine was sold to ISRO under the name "KVD-1" under a deal worth $120 million [8] with soviet agency Glavkosmos which enabled ISRO to import 2 KVD-1 engines and an agreement for transfer of technology from Russia.[9]

ISRO Programme

The engines were proved to be inefficient because of low thrust/weight ratio. Later Russian agency optimised the engine to launch a satellite with liftoff mass of 2.5 tonnes. As a result INSAT-4CR satellite with a liftoff mass of 2,140 kg was launched in 2007.[7]

Sanctions imposed by United States

In 1991, An agreement was signed between India and Russia for technology transfer to India so that KVD-1 engines can be built indigenously in India. But later in July 1993, US imposed sanctions on ISRO and Glavkosmos saying it voids the Missile Technology Control Regime. After suffering setback in this case ISRO was forced to develop its own cryogenic programme.[10]

Features

The engine was single chamber fueled rocket which could be used as cryogenic engines for launching of spacecrafts that could be put in elliptical and geostationary orbits.

  • Unfuelled mass  : 282 kg (621 lb).
  • Height  : 2.14 m
  • Diameter  : 1.56 m
  • Specific impulse: 462 seconds
  • Thrust: 69.60 kN (15,647 lbf)
  • Burn time  : 800 seconds[2]

Use

KVD-1 was used in following launch vehicles

  • GSLV Mk I

References

  1. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  2. ↑ 2.0 2.1 Lua error in package.lua at line 80: module 'strict' not found.
  3. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  4. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  5. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  6. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  7. ↑ 7.0 7.1 Lua error in package.lua at line 80: module 'strict' not found.
  8. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  9. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  10. ↑ Lua error in package.lua at line 80: module 'strict' not found.

External links

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