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SR19

Encyclopedia Astronautica
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SR19
Part of Minuteman Family
Aerojet solid rocket engine. Second stage of Minuteman 2. Surplus motors were used in a variety of anti-ballistic missile test target missiles from the 1980's.
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AKA: LRALT-2; Minuteman 2-2; SR-19. Status: In production. Date: 1959-1962. Number: 5 . Thrust: 267.70 kN (60,181 lbf). Gross mass: 7,032 kg (15,502 lb). Unfuelled mass: 795 kg (1,752 lb). Specific impulse: 288 s. Burn time: 66 s. Height: 4.12 m (13.51 ft). Diameter: 1.33 m (4.36 ft).

Subtopics
ait American target missile. The ait vehicles were developed to support the USAF Airborne Intercept Technology program. They consisted of a Minuteman SR19AJ1 first stage (the basic ait version) or Thiokol Castor IVB first stage (designated ait-2), and a Minuteman II M57A1 second stage. A front-end module housed the payloads, the control system, GPS, and inertial guidance electronics.
Country: USA. Launch Vehicles: Minuteman 2, Minuteman 3, M55E1, SR19 1999, Hera, Storm-2, Minuteman 2 PLV, ait, SR19/SR19, Minotaur 1, Minotaur 2, LRALT. Propellants: Solid. Stages: SR19. Agency: Aerojet. More at: 9709.
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