Encyclopedia Astronautica
Icarus St2


ERAU solid rocket engine. 4.1 kN.

Gross mass: 10 kg (22 lb).
Unfuelled mass: 4.00 kg (8.80 lb).
Height: 1.40 m (4.50 ft).
Diameter: 0.11 m (0.36 ft).
Thrust: 4.10 kN (922 lbf).

More... - Chronology...


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
  • Icarus-2 Solid rocket stage. 4.10 kN (922 lbf) thrust. Mass 10 kg (22 lb). More...

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