Encyclopedia Astronautica
PRD-33


SKB-30 solid rocket engine. 1962 kN.

Gross mass: 3,000 kg (6,600 lb).
Height: 3.10 m (10.10 ft).
Diameter: 1.00 m (3.20 ft).
Thrust: 1,962.00 kN (441,075 lbf).
Burn time: 4.50 s.

More... - Chronology...


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
  • V-1000-0 Solid propellant rocket stage. Loaded mass 3,000 kg. Thrust 1,962.00 kN. More...

Home - Browse - Contact
© / Conditions for Use