RPI solid rocket engine. 9 kN.
AKA: 9KS2150.
Gross mass: 10 kg (22 lb).
Unfuelled mass: 2.00 kg (4.40 lb).
Height: 1.70 m (5.50 ft).
Diameter: 0.0800 m (0.2620 ft).
Thrust: 9.00 kN (2,023 lbf).
Burn time: 1.90 s.
More... - Chronology...
Associated Countries
See also
Associated Manufacturers and Agencies
-
RPI American manufacturer of rocket engines and rockets. RPI, 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
Home - Browse - Contact
© / Conditions for Use
