Thiokol solid rocket engine. 107.2 kN. Used in Shuttle,Titan 34D. Isp=282s. Used on Delta 7925 launch vehicle. First flight 1990.
Area Ratio: 27.33.
Gross mass: 3,697 kg (8,150 lb).
Unfuelled mass: 431 kg (950 lb).
Height: 1.83 m (6.00 ft).
Diameter: 1.60 m (5.20 ft).
Thrust: 107.20 kN (24,100 lbf).
Specific impulse: 282 s.
Burn time: 120 s.
Number: 104 .
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Associated Countries
See also
Associated Launch Vehicles
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Delta 7925 American orbital launch vehicle. Four stage vehicle consisting of 9 x GEM-40 + 1 x EELT Thor/RS-27A + 1 x Delta K + 1 x Star 48B More...
Associated Manufacturers and Agencies
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Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, 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...
Associated Stages
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PAM-D2 Solid propellant rocket stage. Loaded/empty mass 3,697/431 kg. Thrust 107.20 kN. Vacuum specific impulse 282 seconds. More...
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