Solid rocket stage. 152.00 kN (34,171 lbf) thrust. Mass 3,600 kg (7,937 lb).
Status: Active.
Gross mass: 3,600 kg (7,900 lb).
Unfuelled mass: 400 kg (880 lb).
Height: 2.30 m (7.50 ft).
Diameter: 1.32 m (4.33 ft).
Thrust: 152.00 kN (34,170 lbf).
Burn time: 61 s.
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Associated Countries
Associated Engines
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SR73 Aerojet solid rocket engine. Minuteman 1 LGM-30 3rd stage. More...
Associated Launch Vehicles
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Minuteman 3 American four-stage solid-propellant intercontinental ballistic missile. In the 21st Century, the sole remaining US ICBM. More...
Associated Manufacturers and Agencies
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Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, 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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