| Toroid FD |
home
topic index |
|
Engine Model: Toroid FD. Propellants: Lox/LH2. Thrust(vac): 20,015.000 kN (4,499,550 lbf). Isp: 455 sec. Burn time: 408 sec. Chambers: 1. Country: USA. Status: Study 1963. Operational date would have been December 1976. Engines for recoverable stage. Toroid FD used on Rocket Stages
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. |