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Star 37X


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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 37X Part of Star 37 Thiokol solid rocket engine. Out of Production. Total impulse 310,668 kgf-sec. Motor propellant mass fraction 0.928.

AKA: Burner 3;TE-M-714-1. Status: Out of Production. Thrust: 51.10 kN (11,488 lbf). Gross mass: 1,150 kg (2,530 lb). Unfuelled mass: 83 kg (182 lb). Specific impulse: 296 s. Specific impulse sea level: 230 s. Burn time: 60 s. Height: 1.86 m (6.10 ft). Diameter: 0.94 m (3.08 ft).

Thrust (sl): 39.600 kN (8,902 lbf). Thrust (sl): 4,039 kgf.

Country: USA. Propellants: Solid. Stages: Star 37X. Agency: Thiokol. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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