|
Shuttle Super Lightweight Tank
|
|
Gross Mass: 748,000 kg (1,649,000 lb). Empty Mass: 27,000 kg (59,000 lb). Isp: 453 sec. Burn time: 522 sec. Propellants: Lox/LH2. Isp(sl): 361 sec. Diameter: 8.40 m (27.50 ft). Span: 8.70 m (28.50 ft). Length: 47.00 m (154.00 ft). Country: USA. No Engines: 0. Engine: None. Status: In production. Other designations: Super Lightweight External Tank. The Super Lightweight Tank used 2195 Aluminium-Lithium alloy as the main structural material in place of the 2219 aluminium alloy of the original design. This saved 3,500 kg in empty mass, increasing shuttle payload by the same amount. This change was made in anticipation of Shuttle-Mir and Shuttle-ISS flights to high inclination 51.6 degree orbits. The tank was first used on STS-91 in June 1998.
Used on Launch Vehicles:
|
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 - 2007 except where otherwise noted.
|
|
|
|