TE-388

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Engine Model: TE-388. Designer: Thiokol. Gross Mass: 100 kg (220 lb). Empty Mass: 43 kg (94 lb). Propellants: Solid. Thrust(vac): 24.400 kN (5,485 lbf). Burn time: 7.70 sec. Diameter: 0.20 m (0.65 ft). Length: 2.70 m (8.80 ft). Country: USA. TE-388 used on Rocket Stages Used on stage: Iroquois. on launch vehicle: Nike. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.