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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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