Encyclopedia Astronautica
XM-45


Rocket solid engine. 200 kN.

Gross mass: 900 kg (1,980 lb).
Unfuelled mass: 377 kg (831 lb).
Height: 4.50 m (14.70 ft).
Diameter: 0.38 m (1.24 ft).
Thrust: 200.00 kN (44,960 lbf).
Burn time: 6.00 s.

More... - Chronology...


Associated Countries
See also
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
Home - Browse - Contact
© / Conditions for Use