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Background Information
- Program:
- Rocket System Launch Program (RSLP)
- First Launch:
- 4rd Quarter FY 1996
- Flight Rate:
- TBD
- Launch Site:
- VAFB, USA and CCAFS, USA
- Capability:
- 300 LB to Polar Orbit
History
-
Minuteman ICBM began launching in early 1960’s
- 450 ICBM missiles are being retired with a 20 year 98% success rate
- Use of these boosters is consistent with Strategic Arms Reduction Treaty (START) and Missile Technology Control Regime (MTCR) guidelines.
- RSLP received it’s SECDEF charter in 1972 and has over 500 successful launches since 1962
- Minuteman will be operational beyond 2010
Description
-
Three-stage Minuteman ICBM launched above ground
- Contains a Velocity Control System to circularize orbit and provide final atitude control
- Stage 1 Thiokol solid rocket motor generating 178,200 lb of thrust
- Stage 2 Aerojet Solid rocket motor generating 60,300 lb of thrust
- Stage 3 United Technologies solid rocket motor generates 34,200 lb thrust
Profile
-
Length:
- 72 ft
- Launch Weight:
- 75,400 lb
- Diameter:
- 5.5 ft( Stage 1)
- Liftoff Thrust:
- 178,200 lb
- Payload Fairing:
- 12.5 x 3.3 ft
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