Encyclopedia Astronautica
RM-1400


Cooper solid rocket engine. 12.7 kN.

Gross mass: 94 kg (207 lb).
Unfuelled mass: 27 kg (59 lb).
Height: 2.80 m (9.10 ft).
Diameter: 0.17 m (0.54 ft).
Thrust: 12.70 kN (2,855 lbf).
Burn time: 12 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Cooper American manufacturer of rocket engines and rockets. Cooper Development Company, 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
  • Asp IV Solid rocket stage. 12.70 kN (2,855 lbf) thrust. Mass 94 kg (207 lb). More...

Home - Browse - Contact
© / Conditions for Use