Solid rocket stage. 25.00 kN (5,620 lbf) thrust. Mass 35 kg (77 lb).
Status: Active.
Gross mass: 35 kg (77 lb).
Unfuelled mass: 9.00 kg (19.80 lb).
Height: 2.40 m (7.80 ft).
Diameter: 0.11 m (0.36 ft).
Thrust: 25.00 kN (5,620 lbf).
Burn time: 2.20 s.
Number: 366 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Viper 3A American sounding rocket. The Viper 3A/10D Dart was a two stage sounding rocket vehicle consisting of a solid propellant Viper 3A rocket motor as the first stage and a non-propulsive Dart containing the payload as the second stage. More...
Associated Manufacturers and Agencies
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Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. 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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