|
Minuteman 2-2
|
|
Gross Mass: 7,032 kg (15,502 lb). Empty Mass: 795 kg (1,752 lb). Thrust (vac): 267.700 kN (60,181 lbf). Isp: 288 sec. Burn time: 66 sec. Propellants: Solid. Propellant Formulation: ANB-3066. Diameter: 1.33 m (4.36 ft). Span: 1.33 m (4.36 ft). Length: 4.12 m (13.51 ft). Country: USA. No Engines: 1. Engine: SR-19. Status: In production. First Flight: 2000. Last Flight: 2006. No Launched: 5. Second stage of Minuteman 2. Used as second stage of Minotaur launch vehicle and various SDI targets in 1980's.
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.
|
|
|
|