Solid propellant rocket stage. Loaded mass 3,500 kg. Thrust 213.00 kN.
Status: Retired 1959.
Gross mass: 3,500 kg (7,700 lb).
Height: 4.50 m (14.70 ft).
Diameter: 0.79 m (2.59 ft).
Thrust: 213.00 kN (47,884 lbf).
Burn time: 24 s.
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Associated Countries
Associated Engines
Associated Launch Vehicles
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High Virgo American air-launched test vehicle. Two stage vehicle consisting of 1 x B-58 Hustler + 1 x TX-20 Sergeant More...
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Draco American test vehicle. Two stage vehicle consisting of 1 x TX-20 Sergeant + 1 x TX-30 More...
Associated Manufacturers and Agencies
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Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, 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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