Encyclopedia Astronautica
LAPSTAR-300


WRE solid rocket engine. 80 kN.

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
See also
Associated Manufacturers and Agencies
  • WRE Australian manufacturer of rockets, spacecraft, and rocket engines. Australian Weapons Research Establishment, Australia. More...

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
  • Aeolus-1 Solid propellant rocket stage. Loaded mass 300 kg. Thrust 80.00 kN. More...

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