Solid propellant rocket stage. Loaded/empty mass 1,710/650 kg. Thrust 90.70 kN. Vacuum specific impulse 277 seconds.
Cost $ : 1.000 million.
AKA: Advanced Satellite Launch Vehicle.
Status: Retired 1994.
Gross mass: 1,710 kg (3,760 lb).
Unfuelled mass: 650 kg (1,430 lb).
Height: 2.44 m (8.00 ft).
Diameter: 0.82 m (2.69 ft).
Span: 0.82 m (2.69 ft).
Thrust: 90.70 kN (20,390 lbf).
Specific impulse: 277 s.
Specific impulse sea level: 190 s.
Burn time: 45 s.
Number: 4 .
More... - Chronology...
Associated Countries
Associated Engines
-
SLV-3 ISRO solid rocket engine. 90.7 kN. Isp=277s. Used on ASLV, SLV. First flight 1979. More...
Associated Launch Vehicles
Associated Propellants
-
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...
Home - Browse - Contact
© / Conditions for Use
