Encyclopedia Astronautica
M112


Aerojet solid rocket engine. 13 kN.

Gross mass: 600 kg (1,320 lb).
Height: 5.00 m (16.40 ft).
Diameter: 0.35 m (1.14 ft).
Thrust: 13.00 kN (2,922 lbf).
Burn time: 32 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
  • Aerobee 75-1 Nitric acid/Aniline propellant rocket stage. Loaded/empty mass 500/142 kg. Thrust 13.00 kN. More...

Home - Browse - Contact
© / Conditions for Use