Super-Jupiter-2 E-1 Engine Credit - © Mark Wade Gross Mass: 96,700 kg (213,100 lb). Empty Mass: 7,200 kg (15,800 lb). Thrust (vac): 1,884.592 kN (423,673 lbf). Isp: 290 sec. Burn time: 133 sec. Propellants: Lox/Kerosene. Isp(sl): 260 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 18.00 m (59.00 ft). Country: USA. No Engines: 1. Engine: E-1. Status: Development 1958.                   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 - 2007 except where otherwise noted.

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