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Model: 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. Motor: SR-19. Status: Active. First Flight: 1998. Last Flight: 2007. No Launched: 32. Second stage of Minuteman 2. Used as second stage of Minotaur launch vehicle and various SDI targets in 1980's. Model: LRALT-2. Gross Mass: 7,032 kg (15,502 lb). Empty Mass: 795 kg (1,752 lb). Thrust (vac): 267.700 kN (60,181 lbf). Burn time: 66 sec. Propellants: Solid. Diameter: 1.32 m (4.33 ft). Length: 4.10 m (13.40 ft). Country: USA. No Engines: 1. Motor: SR19. Status: Active. Used as: SR19. Release conditions: Aerojet.
Used on Launch Vehicles:
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