Solid propellant rocket stage. Loaded/empty mass 875/150 kg. Thrust 19.60 kN. Vacuum specific impulse 291 seconds.
Status: Out of production.
Gross mass: 875 kg (1,929 lb).
Unfuelled mass: 150 kg (330 lb).
Height: 2.20 m (7.20 ft).
Diameter: 2.05 m (6.72 ft).
Span: 2.05 m (6.72 ft).
Thrust: 19.60 kN (4,406 lbf).
Specific impulse: 291 s.
Specific impulse sea level: 200 s.
Burn time: 100 s.
Number: 2 .
More... - Chronology...
Associated Countries
Associated Engines
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CZ-1D-3 Fourth Academy solid rocket engine. Out of production. Motor for proposed CZ-1D launch vehicle. Isp=291s. First flight 1995. More...
Associated Launch Vehicles
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T-7/GF-01A Chinese sounding rocket. Three stage vehicle consisting of T-7A + GF-01A More...
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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