Solid propellant rocket stage. Loaded mass 600 kg. Thrust 13.00 kN.
Status: Retired 1975.
Gross mass: 600 kg (1,320 lb).
Height: 5.00 m (16.40 ft).
Diameter: 0.35 m (1.14 ft).
Thrust: 13.00 kN (2,922 lbf).
Burn time: 32 s.
Number: 1 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Nike Hawk American sounding rocket. Two stage vehicle consisting of 1 x Nike + 1 x Hawk More...
Associated Manufacturers and Agencies
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Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
Associated Propellants
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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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