|
Engine Model: REA 22-16. Designer: Marquardt. Propellants: Hydrazine. Thrust(vac): 130 N (20 lbf). Chambers: 1. Country: USA. Status: In Production.
Engine Model: REA 22-17. Designer: Marquardt. Propellants: Hydrazine. Thrust(vac): 178 N (40 lbf). Chambers: 1. Country: USA. Status: In Production.
Engine Model: REA 22-2. Designer: Marquardt. Propellants: Hydrazine. Thrust(vac): 90 N (20 lbf). Chambers: 1. Country: USA. Status: In Production.
Engine Model: REA 22-5. Designer: Marquardt. Propellants: Hydrazine. Thrust(vac): 50 N (11 lbf). Chambers: 1. Country: USA. Status: In 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.
|
|