RO solid rocket engine. 50.1 kN.
Gross mass: 1,100 kg (2,400 lb).
Unfuelled mass: 230 kg (500 lb).
Height: 5.40 m (17.70 ft).
Diameter: 0.44 m (1.44 ft).
Thrust: 50.10 kN (11,263 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 4-2 Solid rocket stage. 50.10 kN (11,263 lbf) thrust. Mass 1,100 kg (2,425 lb). More...
Home - Browse - Contact
© / Conditions for Use
