|
Engine Model: TX-174. Designer: Thiokol. Gross Mass: 2,000 kg (4,400 lb). Propellants: Solid. Thrust(vac): 117.000 kN (26,302 lbf). Burn time: 39 sec. Diameter: 1.02 m (3.34 ft). Length: 2.80 m (9.10 ft). Country: USA.
TX-174 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.
|
|