Solid rocket stage. 1365.00 kN (306,864 lbf) thrust. Mass 27,800 kg (61,289 lb).
AKA: SR119.
Status: Retired 2005.
Gross mass: 27,800 kg (61,200 lb).
Unfuelled mass: 2,900 kg (6,300 lb).
Height: 5.40 m (17.70 ft).
Diameter: 2.35 m (7.70 ft).
Thrust: 1,365.00 kN (306,864 lbf).
Burn time: 54 s.
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
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Peacekeeper American intercontinental ballistic missile. 10 nuclear MIRV warheads. In service 1986-2004. 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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