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Engine Model: TU-904. Designer: Thiokol. Gross Mass: 53,400 kg (117,700 lb). Empty Mass: 4,400 kg (9,700 lb). Propellants: Solid. Thrust(vac): 1,711.000 kN (384,648 lbf). Burn time: 79 sec. Diameter: 2.35 m (7.70 ft). Length: 9.10 m (29.80 ft). Country: USA.
TU-904 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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