Solid propellant rocket stage. Loaded/empty mass 369/34 kg. Thrust 19.40 kN. Vacuum specific impulse 295 seconds.
Status: Out of production.
Gross mass: 369 kg (813 lb).
Unfuelled mass: 34 kg (74 lb).
Height: 1.13 m (3.70 ft).
Diameter: 0.77 m (2.52 ft).
Span: 0.77 m (2.52 ft).
Thrust: 19.40 kN (4,361 lbf).
Specific impulse: 295 s.
Specific impulse sea level: 220 s.
Burn time: 50 s.
Number: 25 .
More... - Chronology...
Associated Countries
Associated Engines
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Mage 1 SEP solid rocket engine. 19.4 kN. Out of production. Orbital circularization motor. Isp=295s. First flight 1979. More...
Associated Launch Vehicles
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Ariane 1 French orbital launch vehicle. First version of the Ariane launch vehicle. 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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