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Star 37E


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Star 37E Part of Star 37 Thiokol solid rocket engine. Out of Production. Total impulse 296,635 kgf-sec. Motor propellant mass fraction 0.926.

AKA: TE-M-364-4. Status: Out of Production. Number: 91 . Thrust: 68.00 kN (15,287 lbf). Gross mass: 1,123 kg (2,475 lb). Unfuelled mass: 83 kg (182 lb). Specific impulse: 284 s. Burn time: 42 s. Diameter: 0.93 m (3.07 ft).

Country: USA. Launch Vehicles: Atlas F/PTS, Atlas F/SVS, N-2, Atlas E/SVS, Delta 3924. Propellants: Solid. Stages: Star 37E. Agency: Thiokol. Bibliography: 410. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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