Solid rocket stage. 45.00 kN (10,116 lbf) thrust. Mass 718 kg (1,583 lb).
Status: Retired 1977.
Gross mass: 718 kg (1,582 lb).
Unfuelled mass: 64 kg (141 lb).
Height: 1.50 m (4.90 ft).
Diameter: 0.94 m (3.08 ft).
Thrust: 45.00 kN (10,116 lbf).
Number: 6 .
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Associated Countries
Associated Engines
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Star 37D Thiokol solid rocket engine. 45 kN. Out of Production. Total impulse 189,489 kgf-sec. Motor propellant mass fraction 0.91. Isp=266s. More...
Associated Launch Vehicles
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Delta M American orbital launch vehicle. Long Tank Thor augmented with 3 Castor 2 boosters and Delta E / Burner 2 (Star 37D) upper stages. More...
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Delta 1913 American orbital launch vehicle. Four stage vehicle consisting of 9 x Castor 2 + 1 x ELT Thor/MB-3 + 1 x Delta P /TR-201 + 1 x Star 37D More...
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Delta 2313 American orbital launch vehicle. Three stage vehicle consisting of 3 x Castor 2 + 1 x ELT Thor/RS-27 + 1 x Delta P /TR-201 + 1 x Star 37D More...
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Delta 2913 American orbital launch vehicle. Three stage vehicle consisting of 9 x Castor 2 + 1 x ELT Thor/RS-27 + 1 x Delta P /TR-201 + 1 x Star 37D 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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