LE-3 home
topic index
LE-3
Credit - Boeing / Rocketdyne
Engine Model: LE-3. Designer: Rocketdyne. Developed in: 1970. Propellants: N2O4/Aerozine-50. Thrust(vac): 53.340 kN (11,991 lbf). Isp: 285 sec. Country: Japan.

MHI(Japan)/Rocketdyne Upper Stage. Pressure-fed.

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.