E-1

E-1
Credit - Boeing / Rocketdyne

Manufacturer Name: E-1. Designer: Rocketdyne. Developed in: 1957. Propellants: Lox/Kerosene. Thrust(vac): 1,884.592 kN (423,673 lbf). Thrust(sl): 1,689.600 kN (379,837 lbf). Isp: 290 sec. Isp (sea level): 260 sec. Chambers: 1. Country: USA. Status: Study 1957.

Developed by USAF in late 1950's. Cancelled and decision to go direct to 1,500,000 lbf F-1 as next step. Booster applications. Gas generator, pump-fed.

E-1 used on Rocket Stages

Used on stage: Super-Jupiter. on launch vehicle: Super-Jupiter.

Used on stage: Super-Jupiter-2.

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.

Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z