|
Engine Model: T-55. Designer: Thiokol. Empty Mass: 12 kg (26 lb). Propellants: Solid. Thrust(vac): 21.000 kN (4,720 lbf). Burn time: 1.30 sec. Diameter: 0.15 m (0.49 ft). Length: 1.50 m (4.90 ft). Country: USA.
T-55 used on Rocket Stages
- Used on stage: T-55. on launch vehicle: Jason.
- Used on stage: T-55. on launch vehicle: Nike.
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.
|
|