Solid propellant rocket stage. Loaded mass 300 kg. Thrust 80.00 kN.
No Engines: 7.
Status: Retired 1961.
Gross mass: 300 kg (660 lb).
Height: 1.80 m (5.90 ft).
Diameter: 0.41 m (1.34 ft).
Thrust: 80.00 kN (17,984 lbf).
Burn time: 2.70 s.
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Aeolus Australian test vehicle. Two stage vehicle consisting of 1 x Aeolus Booster + 1 x Mayfly More...
Associated Manufacturers and Agencies
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WRE Australian manufacturer of rockets, spacecraft, and rocket engines. Australian Weapons Research Establishment, Australia. 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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