Solid rocket stage. 53.00 kN (11,915 lbf) thrust. Mass 200 kg (441 lb).
Status: Retired 1995.
Gross mass: 200 kg (440 lb).
Unfuelled mass: 60 kg (132 lb).
Height: 3.50 m (11.40 ft).
Diameter: 0.22 m (0.72 ft).
Thrust: 53.00 kN (11,914 lbf).
Burn time: 9.50 s.
Number: 538 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Tomahawk Sandia American sounding rocket. Test and sounding vehicles developed by Sandia using the TE-416 Tomahawk motor. More...
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Nike Tomahawk American sounding rocket. Two stage vehicle consisting of a Nike booster and Tomahawk upper stage. Payload 45 kg to 370 km or 115 kg to 215 km. More...
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Ute Tomahawk American sounding rocket. The Ute (TU-715) motor was developed from the Genie motor baseline to serve as a first stage booster in the Ute-Tomahawk sounding rocket vehicle. 2 stage vehicle consisting of 1 x Ute + 1 x Tomahawk More...
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Taurus Tomahawk American sounding rocket. NASA two stage sounding rocket. Payload 27 kg to 590 km or 59 kg to 490 km. More...
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Taurus Tomahawk Nike Three stage vehicle consisting of 1 x Taurus (Honest John motor) + 1 x Nike + 1 x Tomahawk. Payload 32 kg to 700 km or 125 kg to 400 km. More...
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Strypi Tomahawk American target missile. Four stage vehicle consisting of 2 x Recruit + 1 x Castor + 1 x ? + 1 x Tomahawk 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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