Encyclopedia Astronautica
Gosling


RO solid rocket engine. 152 kN.

Gross mass: 200 kg (440 lb).
Height: 3.30 m (10.80 ft).
Diameter: 0.26 m (0.85 ft).
Thrust: 152.00 kN (34,170 lbf).
Burn time: 2.50 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
  • Cockatoo-1 Solid propellant rocket stage. Loaded mass 200 kg. Thrust 152.00 kN. More...
  • Jabiru-3 Solid propellant rocket stage. Loaded mass 300 kg. Thrust 140.00 kN. More...
  • Jaguar 1-2 Solid propellant rocket stage. Loaded mass 200 kg. Thrust 140.00 kN. More...

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