Solid propellant rocket stage. Loaded mass 2,000 kg. Thrust 85.00 kN.
Status: Retired 1983.
Gross mass: 2,000 kg (4,400 lb).
Height: 2.70 m (8.80 ft).
Diameter: 1.02 m (3.34 ft).
Thrust: 85.00 kN (19,108 lbf).
Burn time: 39 s.
Number: 423 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
Associated Manufacturers and Agencies
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Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. More...
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Martin American manufacturer of rockets, spacecraft, and rocket engines. Martin Marietta Astronautics Group (1956), Denver, CO, USA. 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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