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Augmented Satellite Launch Vehicle

 
Wikipedia: Augmented Satellite Launch Vehicle
Augmented Satellite Launch Vehicle
Augmented Satellite Launch Vehicle
Augmented Satellite Launch Vehicle
Function Small carrier rocket
Manufacturer ISRO
Country of origin  India
Size
Height 24 metres (79 ft)
Diameter 1 metre (3.3 ft)
Mass 41,000 kilograms (90,000 lb)
Capacity
Payload to
400km LEO
150 kilograms (330 lb)
Associated rockets
Family SLV, PSLV, GSLV
Launch history
Status Retired
Launch sites Sriharikota
Total launches 4
Successes 1
Failures 2
Partial failures 1
Maiden flight 24 March 1987
Last flight 4 May 1994
Notable payloads SROSS
First Stage
Engines 2 solid
Thrust 502.6 kilonewtons (113,000 lbf) each
Specific impulse 253 sec
Burn time 49 seconds
Fuel Solid
Second Stage
Engines 1 solid
Thrust 702.6 kilonewtons (158,000 lbf)
Specific impulse 259 sec
Burn time 45 seconds
Fuel Solid
Third Stage
Engines 1 solid
Thrust 304 kilonewtons (68,000 lbf)
Specific impulse 276 sec
Burn time 36 seconds
Fuel Solid
Fourth Stage
Engines 1 solid
Thrust 90.7 kilonewtons (20,400 lbf)
Specific impulse 277 sec
Burn time 45 seconds
Fuel Solid
Fifth Stage
Engines 1 solid
Thrust 35 kilonewtons (7,900 lbf)
Specific impulse 281 sec
Burn time 33 seconds
Fuel Solid

Augmented Satellite Launch Vehicle (ASLV) (संवर्धित उपग्रह प्रक्षेपण यान), was a 5-stage solid propellant rocket developed by the Indian Space Research Organisation (ISRO) to place 150 kg satellites into LEO.[1] This project was started by India during the early 1980s to develop technologies needed for a payload to be placed into a geostationary orbit.[2] Its design was based on Satellite Launch Vehicle.[3] ISRO did not have sufficient funds for both the PSLV programme and the ASLV programme at the same time and the ASLV programme was terminated after the initial developmental flights.[2] The payloads of ASLV were Stretched Rohini Satellites.[3]

Launch log

Version Date of Launch Launch Location Launch Pad Payload Mission Status
3 D1 24 March 1987 SDHC, Sriharikota 1 SROSS A, 150 kg Failure; First stage did not ignite after strap-on burnout.[3]
3 D2 12 July 1988 SDHC, Sriharikota 1 SROSS-B, 150 kg Failure Insufficient control gain[3]
3 D3 20 May 1992 SDHC, Sriharikota 1 SROSS-C, 106 kg Partial Success.[4]
3 D4 4 May 1994 SDHC, Sriharikota 1 SROSS-C2, 113 kg Success.[4]

References

  1. ^ http://www.isro.org/aslv.htm
  2. ^ a b http://www.bharat-rakshak.com/SPACE/space-launchers-aslv.html
  3. ^ a b c d http://www.astronautix.com/lvs/aslv.htm
  4. ^ a b http://heasarc.gsfc.nasa.gov/docs/heasarc/missions/sross3.html



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