Encyclopedia Astronautica
Raven 1


RO solid rocket engine. 44.5 kN.

Gross mass: 1,000 kg (2,200 lb).
Unfuelled mass: 240 kg (520 lb).
Height: 5.10 m (16.70 ft).
Diameter: 0.44 m (1.44 ft).
Thrust: 44.50 kN (10,004 lbf).
Burn time: 30 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
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
  • Skylark 1-1 Solid rocket stage. 44.50 kN (10,004 lbf) thrust. Mass 1,000 kg (2,205 lb). More...

Home - Browse - Contact
© / Conditions for Use