|
Engine Model: TX-30. Designer: Thiokol. Gross Mass: 2,000 kg (4,400 lb). Propellants: Solid. Thrust(vac): 44.500 kN (10,004 lbf). Burn time: 29 sec. Diameter: 0.79 m (2.59 ft). Length: 5.40 m (17.70 ft). Country: USA.
TX-30 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.
|
|