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Engine Model: Gamma 301. Designer: Saunders-Roe. Propellants: H2O2/Kerosene. Thrust(vac): 75.000 kN (16,860 lbf). Burn time: 140 sec. Country: UK.
Gamma 301 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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