Aerojet solid rocket engine. 11,143 kN. Design concept 1960's. Isp=263s.
Status: Design concept 1960's.
Thrust: 11,143.00 kN (2,505,046 lbf).
Specific impulse: 263 s.
Specific impulse sea level: 238 s.
Burn time: 114 s.
More... - Chronology...
Associated Countries
See also
Associated Manufacturers and Agencies
-
Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
Associated Propellants
-
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
-
Saturn 3S-2 Solid propellant rocket stage. Loaded/empty mass 561,100/57,600 kg. Thrust 11,143.20 kN. Vacuum specific impulse 263 seconds. 260 inch solid booster - full length. More...
Home - Browse - Contact
© / Conditions for Use
