Solid propellant rocket stage. Loaded/empty mass 512/195 kg. Thrust 35.00 kN. Vacuum specific impulse 281 seconds.
Cost $ : 0.500 million.
AKA: Advanced Satellite Launch Vehicle.
Status: Retired 1994.
Gross mass: 512 kg (1,128 lb).
Unfuelled mass: 195 kg (429 lb).
Height: 1.40 m (4.50 ft).
Diameter: 0.66 m (2.16 ft).
Span: 0.66 m (2.16 ft).
Thrust: 35.00 kN (7,868 lbf).
Specific impulse: 281 s.
Specific impulse sea level: 110 s.
Burn time: 33 s.
Number: 4 .
More... - Chronology...
Associated Countries
Associated Engines
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SLV-4 ISRO solid rocket engine. 26.8 kN. Isp=283s. Used on ASLV, SLV. First flight 1979. More...
Associated Launch Vehicles
Associated Propellants
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Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
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