| LH2 2000/3000 Ibf thrust |
home
topic index |
|
Engine Model: LH2 2000/3000 Ibf thrust. Manufacturer Name: LH2 2000/3000 Ibf thrust. Designer: Aerojet. Developed in: July 1946. Propellants: Lox/LH2. Thrust(sl): 13.330 kN (2,997 lbf). Country: USA. Development begun July 1946. Engine R&D, hydrogen production 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. |