Solid propellant rocket stage. Loaded/empty mass 6,400/3,300 kg. Thrust 784.00 kN. Zero-length launch stage for Tu-121. Thrust varied from 75 to 80 tonnes and duration from 3.75 to 5.0 seconds.
Propellant Formulation: NMF-2. No Engines: 2.
Status: Out of Production.
Gross mass: 6,400 kg (14,100 lb).
Unfuelled mass: 3,300 kg (7,200 lb).
Thrust: 784.00 kN (176,250 lbf).
Burn time: 4.00 s.
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Associated Countries
Associated Engines
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PRD-52 Kartukov solid rocket engine. 784 kN. DBR-1 Yastreb. Out of Production. Thrust 80 tf at ignition, 75 tf at cutout. More...
Associated Propellants
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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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