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(詳細はLGM-30 Minuteman intercontinental ballistic missile, acquisition and operational. ==Program chronology== *1956 * *Von Neumann Committee approved Ballistic Missile feasibility program * *R&D programs and contracts authorized *1957 * *ICBM improvements studies started * *Minuteman configuration studies started * 1958 * *Minuteman R&D program authorized *1959 * *First R&D firing from silo - inert second and third stage *1960 * *First contract for operational wing facilities at Wing I * *Missile production *1961 * *First all-up missile launch from pad at Eastern Test Range * *First missile launch from silo at Eastern Test Range *1962 * *First missile launch from Western Test Range * *Minuteman-I operational flight turnover at Wing I *1963 * *First wing turnover at Wing I, Wing II turnover * *Force Mod program approved * *First motor static test firing to verify reliability *1964 * *Wing III and Wing IV turnover * *New features approved * *Minuteman-II flight test * *GIANT BOOST *1965 * *Wing V turnover * *Vulnerability improvements * *Minuteman fully operational at Wing II, Wing III *1966 * *Wing IV turnover * *Minuteman-III approval * *Aging surveillance program initiated * *Minuteman-II operational at Wing VI * *ERCS deployed *1967 * *Squadron 20 turnover * *Force Mod at Wing IV *1968 * *Hard rock silo program started * *First Minuteman-III R&D flight *1969 * *Force Mod rate decrease * *Force Mod at Wing I complete * *Service Star testing began for RSs *1970 * *First Minuteman-III at Wing III (Hotel Flight/H-02) * *Upgrade silo and CDB programs started * *First MOM test at Wing VI *1971 * *Minuteman-III dust program started * *Force Mod at Wing III completed *1972 * *Minuteman-III deployed at Wing VI * *First dust-hardened Minuteman-III deployed at Wing VI * *Minuteman ordnance service life analysis program developed * *Responsibility for service life testing transferred to Ogden Air Logistics Center (OO-ALC), Hill Air Force Base, Utah *1973 * *Upgrade silo and CDB IOC at Wing V * *Force Mod and upgrade silo completed at Wing II * *Last MOM at Wing III *1974 * *Full Force upgrade silo approved * *MK12A and Pave Pepper programs started * *SSAS was deployed for Minuteman II *1975 * *Upgrade silo and CDB completed at Wing V * *Upgrade silo and CDB start at Wing III * *Simulated Electronic Launch Minuteman (SELM) program started * *Minuteman bench test program concept developed by OO-ALC * *Minuteman-III fully deployed * *Minuteman program management responsibility transfer (PMRT) *1976 * *Upgrade silo and CDB completed at Wing III * *Upgrade silo and CDB completed at Wing VI * *Long range service life analysis performed for propulsion system * *Hybrid explicit implemented for Minuteman III * *Minuteman II MGS vibration test program initiated * *New calibration schedule implemented to correct MGS startup transients * *Minuteman II Stage 3 lot 16 motor igniters replaced *1977 * *Minuteman III missile production terminated * *Inertial performance data began to be collected for guidance system fault isolation * *Began implementation of ILCS at Minuteman II wings *1978 * *GIP implemented at Minuteman III * *Thrust termination port investigation began *1979 * *Minuteman II stage 2 motor remanufacturing program began to correct degraded liner/Minuteman III stage 3 degraded liner investigation initiated * *USAF advisory board recommended that carbon-carbon nose tips be developed for MK12 RVs *1980 * *Upgrade silo and CDB completed at Wing VI * *Minuteman II accuracy/reliability investigation conducted * *VRSA replacement design started * *Diagnostic data package hardware delivered to provide re-entry/separation data for Minuteman II flights *1981 * *MGS electronics investigation completed * *Accuracy, Reliability, Supportability Improvement Program (ARSIP) program began *1982 * *Minuteman III guidance upgrade program implemented * *MK12A re-entry vehicle FOC * *Special operational test program began - Minuteman II * *Hardness critical items identified and procured *1983 * *Minuteman-III MGS vibration test program initiated * *Special operational test program complete - accuracy improvements verified *1984 * *Minuteman Extended Survivable Power IOC * *GUP implemented for Minuteman III *1985 * *Rivet MILE (Minuteman Integrated Life Extension) program began *1986 * *LGM-118A Peacekeeper deployment initiated *1987 * *Integrated Nuclear Effects Assessment (INEA) * *ARSIP implemented for Minuteman II * *Piece-parts manufacturing for diminished manufacturing sources * *Rivet MILE began Improved Minuteman Physical Security System (IMPSS) installation *1988 * *Minuteman-III Stage 2 washout/Stage 3 replacement * *Comprehensive reliability investigations conducted * *Peacekeeper fully operational at Wing V *1989 * *Rapid Execution and Combat Targeting (REACT) program initiated * *Rocket Motor Transporter replacement * *Code Change Verifier replacement * *Transporter-Erector replacement *1990 *1991 * *Minuteman II removed from SIOP *1992 * *Minuteman II deactivation initiated * *MESP discontinued * *Rivet MILE completes IMPSS installation * *SRV Program initiated * *Rivet ADD initiated * *Missile Transporter replacement * *Missile Transporter (PT III) replacement *1993 * *GRP contract awarded *1994 * *PRP initial contracts awarded *1995 * *REACT consoles begin deployment * *Minuteman-II deactivation complete * *BRAC decision to close Wing VI by 1998 *1996 * *REACT deployment complete *1998 * *Wing VI deactivation complete * *Wing VI Minuteman IIIs moved to Wing I * *AF awards ICBM Prime contract to TRW team for ICBM engineering *1999 * *First NS-50 MGS deployed * *Congress establishes the Minuteman Missile National Historic Site *2000 *2001 * *PRP deployment initiated *2005 * *Peacekeeper deactivation complete〔(Air Force Link: "Air Force says farewell to most powerful ICBM", 15 Sep 2005 )〕 *2007-08 * *(Deactivation and removal of 50 Minuteman III's at Malmstrom AFB, MT ). 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「LGM-30 Minuteman chronology」の詳細全文を読む スポンサード リンク
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