Encyclopedia Astronautica
Aerobee 150 MII 20-1


Solid rocket stage. 80.00 kN (17,985 lbf) thrust. Mass 300 kg (661 lb).

Status: Retired 1970.
Gross mass: 300 kg (660 lb).
Unfuelled mass: 140 kg (300 lb).
Height: 1.80 m (5.90 ft).
Diameter: 0.33 m (1.08 ft).
Thrust: 80.00 kN (17,984 lbf).
Burn time: 2.50 s.
Number: 1 .

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Associated Countries
Associated Engines
  • 2.5KS18000 Multiple-source solid rocket engine. 80 kN. Typical ideal dV=259 m/s; gravity and drag losses = 25 m/s. More...

Associated Launch Vehicles
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...

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