Encyclopedia Astronautica
MARC 14B1


ARC solid rocket engine. 84 kN.

Gross mass: 100 kg (220 lb).
Unfuelled mass: 59 kg (130 lb).
Height: 0.80 m (2.62 ft).
Diameter: 0.30 m (0.98 ft).
Thrust: 84.00 kN (18,883 lbf).
Burn time: 0.80 s.

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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
  • Iris-0 Solid rocket stage. 84.00 kN (18,884 lbf) thrust. Mass 100 kg (220 lb). More...

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