|
Engine Model: TD-2. Designer: CMIK. Propellants: Nitric acid/UDMH. Thrust(vac): 1,000.000 kN (224,800 lbf). Burn time: 120 sec. Country: Korea North.
TD-2 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.
|
|