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SR19
Part of Minuteman
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.
 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. 
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