Encyclopedia Astronautica
Meteor-2


Polish solid rocket engine. 24 kN.

Gross mass: 400 kg (880 lb).
Unfuelled mass: 126 kg (277 lb).
Height: 4.20 m (13.70 ft).
Diameter: 0.35 m (1.14 ft).
Thrust: 24.00 kN (5,395 lbf).
Burn time: 18 s.

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Associated Countries
See also
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
  • Meteor-2H-1 Solid rocket stage. 24.00 kN (5,395 lbf) thrust. Mass 400 kg (882 lb). More...

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