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Engine Model: TX-135. Designer: Thiokol. Gross Mass: 5,000 kg (11,000 lb). Propellants: Solid. Thrust(vac): 2,000.000 kN (449,600 lbf). Burn time: 4.50 sec. Diameter: 0.91 m (2.98 ft). Length: 5.00 m (16.40 ft). Country: USA.
TX-135 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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