Encyclopedia Astronautica
RTV-100


JPL solid rocket engine. 22 kN.

Gross mass: 100 kg (220 lb).
Unfuelled mass: 63 kg (138 lb).
Height: 1.20 m (3.90 ft).
Diameter: 0.30 m (0.98 ft).
Thrust: 22.00 kN (4,945 lbf).
Burn time: 6.00 s.

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Associated Countries
See also
Associated Manufacturers and Agencies
  • JPL American agency;manufacturer of rockets, spacecraft, and rocket engines. Jet Propulsion Laboratory, Pasadena, 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...

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