Encyclopedia Astronautica
Loki


GCR solid rocket engine. 15 kN.

Unfuelled mass: 3.00 kg (6.60 lb).
Height: 1.70 m (5.50 ft).
Diameter: 0.0800 m (0.2620 ft).
Thrust: 15.00 kN (3,372 lbf).
Burn time: 0.80 s.

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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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