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    The LGM-30 Minuteman is a United States nuclear missile, a land-based intercontinental ballistic missile (ICBM). As of 2006, it is the only land-based ICBM in service in the United States. It is complemented by the sea-launched Trident missile SLBM and by nuclear weapons carried by long-range strategic bombers; see current status of United States nuclear weapons.

    The “L” indicates that the missile is silo-launched; the “G” indicates that it is designed to attack surface targets; the “M” indicates that it is a guided missile.

    The name “Minuteman” comes from the Revolutionary War’s Minutemen.


        LGM-30 Minuteman
            Current model
                Guidance Replacement Program (GRP)
                Propulsion Replacement Program (PRP)
                Single Reentry Vehicle (SRV)
                Safety Enhanced Reentry Vehicle (SERV)
            Organization
            Operator
            History
                Minuteman I (LGM-30A/B or SM-80/HSM-80A)
                Minuteman-II (LGM-30F)
                Minuteman-III (LGM-30G)
            Weapon system programs
            Influences
            Mobile Minuteman program
            Emergency Rocket Communications System (ERCS)
            Satellite launching role
            Missile Defense
            Minuteman chronology
            Related content
    NameLGM-30G Minuteman III Missile
    image
    FunctionIntercontinental ballistic missile
    ContractorBoeing
    Unit Cost$7,000,000
    Deployment1962 (Minuteman I), 1965 (Minuteman II), 1970...
    InventoryActive force, 500; Reserve, 0; ANG, 0
    EngineThree solid-propellant rocket motors; first s...
    Launch Mass79,432 lb (36,030 kg)
    Length59.9 ft (18 m)
    Diameter5.5 feet (1.67 m)
    SpeedApproximately 15,000 mph (Mach 23, or 24,000 ...
    Range6,000-plus miles (5,200 nautical miles, or 10...
    Flying Altitude700 miles (1,120 kilometers)
    WarheadNuclear W62, W78, or (2006-) W87
    LoadRe-entry vehicle: Lockheed Martin Missiles an...
    GuidanceInertial
    Launch PlatformSilo

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    Current model
    The current Minuteman force consists of 500 Minuteman-III missiles in missile silos around F.E. Warren Air Force Base, Wyoming, Malmstrom Air Force Base, Montana, and Minot Air Force Base, North Dakota.

    It is a guided missile, with three solid-fuel stages, and in addition, in the post-boost stage (“bus”), a liquid-fuel propulsion system rocket engine used to fine-tune the trajectory of the reentry vehicle and/or dispense individual warheads to separate targets across a broad area. The missile has a gimballed inertial guidance system.

    The third stage has precision shutdown ports which, when opened, reduce the chamber pressure so abruptly that the interior flame is blown out. This allows a more precise trajectory which improves targeting accuracy. The post-boost stage carries, in addition to the warheads, penetration aids such as chaff and decoys.

    With START II’s ban on multiple independently targetable reentry vehicles (MIRVs) now a dead letter, earlier plans to reduce the number of warheads per missile to one have been revised: the United States is now considering keeping 800 warheads on the Minuteman force.

    The Minuteman-III missile entered service in 1970, with weapon systems upgrades included during the production run from 1970 to 1978 to increase accuracy and payload capacity. 1998 USAF plans are to operate it until 2025.

    The LGM-118A Peacekeeper MX ICBM, which was to have replaced the Minuteman, was retired by 2005. The Peacekeeper suffered from controversy over various mobile basing schemes, but the original Peacekeeper basing plan included being deployed on railroad cars.

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    Guidance Replacement Program (GRP)
    The Guidance Replacement Program (GRP) replaces the NS20A Missile Guidance Set with the NS50A Missile Guidance Set. The newer system extends the service life of the Minuteman missile beyond the year 2020 by replacing aging parts and assemblies with current, high reliability technology while maintaining the current accuracy performance.

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    Propulsion Replacement Program (PRP)
    The Propulsion Replacement Program extends the life, maintains the performance, and improves the reliability of the operational ICBM force by replacing the old solid propellant boosters (downstages) with new “environmentally friendly” booster.

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    Single Reentry Vehicle (SRV)
    The Single Reentry Vehicle (SRV) modification allows the United States ICBM force to abide by START treaty requirements by reconfiguring Minuteman-III missiles from three reentry vehicles down to one.

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    Safety Enhanced Reentry Vehicle (SERV)
    Beginning in 2006, Mk-21/W87 RVs from the deactivated LGM-118A Peacekeeper missile will be placed on the Minuteman-III force under the Safety Enhanced Reentry Vehicle (SERV) program. The older W78 currently used is not equipped with important safety features. In addition to adding additional safety features into at least a portion of the future Minuteman-III force, the decision to transfer W87s onto the missile is based on two features that will improve the targeting capabilities of the weapon: more fusing options which will allow for greater targeting flexibility and the most accurate reentry vehicle available which provide a greater probability of damage.

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    Organization
    The basic tactical unit of a Minuteman wing is the squadron, consisting of five flights. Each flight consists of ten unmanned launch facilities (LFs) which are remotely controlled by a manned launch control center (LCC). The five flights are interconnected and status from any LF may be monitored by any of the five LCCs. Each LF is located at least three nautical miles (5.6 km) from any LCC. Control does not extend outside the squadron (i.e. The 319th Missile Squadron’s five LCCs cannot control the 320th Missile Squadron’s 50 LFs). Each Minuteman wing is assisted logistically by a nearby Missile Support Base (MSB).

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    Operator
    : The United States Air Force is the only operator of the Minuteman-III, with three operational wings and one test squadron operating the LGM-30G:

        10th Missile Squadron — “First Aces”
        12th Missile Squadron — “Red Dawgs”
        490th Missile Squadron — “Farsiders”
        564th Missile Squadron — “Deuce”
      Wing Two: 44th Strategic Missile Wing — Ellsworth Air Force Base, South Dakota — “Black Hills Bandits” — Deactivated
        66th Missile Squadron
        67th Missile Squadron
        68th Missile Squadron
        508th Missile Squadron
        509th Missile Squadron
        510th Missile Squadron
        446th Missile Squadron
        447th Missile Squadron
        448th Missile Squadron

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    History

    The Minuteman-I and Minuteman-II were in service from 1960 until 1997. The Minuteman-III was first deployed in 1969 and with the latest upgrades is expected to remain in service through the year 2025.

    The Minuteman had two innovations that gave it a long practical service life: a solid rocket booster, and a digital flight computer. This computer was one of the very first recognizably modern embedded systems.

    The solid rocket booster made the Minuteman faster to launch than other ICBMs, which used liquid fuels. A crucial innovation in this area was to include a valve to release the booster pressure, and permit effective throttling of the booster.

    A reprogrammable inertial guidance system was a major risk in the original program. When first proposed, no one had built a digital computer that would fit in a missile. One program, the SM-64 Navaho, had already failed to produce such a system.

    A digital computer was essential to obtain the accuracy gains that kept this weapon effective throughout the Cold War. As the Defense Mapping Agency (now part of National Geospatial-Intelligence Agency) more accurately mapped mass concentrations in the Earth, the inertial guidance software could be updated and loaded into the missiles to make them ever more accurate by having them compensate for these sources of gravity. Another gain that persuaded program managers to accept the risk of the computer was that the computer could also be used to test the missile. This saved a large amount of weight in cables and connectors.

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    Minuteman I (LGM-30A/B or SM-80/HSM-80A)


    The LGM-30A Minuteman-I entered into the Strategic Air Command’s arsenal in 1962, at Malmstrom Air Force Base, Montana; the “improved” LGM-30B became operational at Ellsworth Air Force Base, South Dakota, Minot Air Force Base, North Dakota, F.E. Warren Air Force Base, Wyoming, Grand Forks Air Force Base, North Dakota, and Whiteman Air Force Base, Missouri in 1963. All 800 Minuteman-I missiles were delivered by June 1965. Each of the bases had 150 missiles emplaced, except for F.E. Warren Air Force Base, which had 200 missiles.

    The Minuteman-I Autonetics D-17 flight computer used a rotating air bearing magnetic disk holding 2,560 “cold-stored” words in 20 tracks (write heads disabled after program fill) of 24 bits each and one alterable track of 128 words. The time for a D-17 disk revolution was 10 ms. The D-17 also used a number of short loops for faster access of intermediate results storage. The D-17 computational minor cycle was three disk revolutions or 30 ms. During that time all recurring computations were performed. For ground operations the inertial platform was aligned and gyro correction rates updated. During flight, filtered command outputs were sent each minor cycle to the engine nozzles. Unlike modern computers, which use descendants of that technology for secondary storage on hard disk, the disk was the active computer memory. The disk storage was considered hard to radiation from nearby nuclear explosions, making it an ideal storage medium. To improve computational speed, the D-17 borrowed an instruction look-ahead feature from the Autonetics-built Field Artillery Data Computer (FADAC) that permitted simple instruction execution every word time.

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    Minuteman-II (LGM-30F)





    The LGM-30F Minuteman-II was an improved version of the Minuteman-I missile. Development on the Minuteman-II began in 1962 as the Minuteman-Is entered the Strategic Air Command’s nuclear force. Minuteman-II production and deployment began in 1965 and completed in 1967. It had an increased range, payload and guidance system with better azimuthal coverage, providing military planners with better accuracy and a wider range of targets. Some missiles also carried penetration aids, allowing higher probability of kill against Moscow’s antiballistic missile system. The payload consisted of a single Mk-11C reentry vehicle containing a W56 nuclear warhead with a yield of 1.2 megatons of TNT (5 PJ). Performance improvements realized in Minuteman-II include greater range, increased throw weight, improved accuracy and reliability, multiple target selection, and greater penetration capability.

      The major new features provided by Minuteman-II were:
        An improved first-stage motor to increase reliability.
        A new-technology, single, fixed nozzle with liquid injection thrust vector control (TVC) on a larger second stage motor to increase missile range. Additional motor improvements to increase reliability.
        An improved guidance system, incorporating semiconductor integrated circuits and miniaturized discrete electronic parts. Minuteman-II was the first program to make a major commitment to these new devices. Their use made possible multiple target selection, greater accuracy and reliability, a reduction in the overall size and weight of the guidance system, and an increase in the survivability of the guidance system in a nuclear environment.
        A penetration aids system to camouflage the warhead during its reentry into an enemy environment.
        A larger warhead in the reentry vehicle (RV) to increase kill probability.

    System modernization was concentrated on launch facilities and command and control facilities. This provided decreased reaction time and increased survivability when under nuclear attack. Final changes to the system were performed to increase compatibility with the LGM-118A, as these latter missiles were introduced into modified Minuteman silos.

    The Minuteman-II program was economically crucial to the development of integrated circuits. It was the first mass-produced system to use a computer constructed from integrated circuits, and used most of the production of such circuits from 1962 through 1967. The other major customer of these circuits was the Apollo Guidance Computer, which had similar weight and ruggedness constraints. The Minuteman-II flight computer continued to use rotating magnetic disk for primary storage.

    A total of 450 LGM-30F missiles were emplaced at Ellsworth Air Force Base, South Dakota (44th Strategic Missile Wing), Grand Forks Air Force Base, North Dakota (321st Strategic Missile Wing), Malmstrom Air Force Base, Montana (341st Strategic Missile Wing), and Whiteman Air Force Base, Missouri (351st Strategic Missile Wing).


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    Minuteman-III (LGM-30G)





    The LGM-30G Minuteman-III program started in 1966, and included several improvements that distinguish it from the LGM-30F Minuteman-II. Most modifications related to the final stage and reentry system, with the third stage improved with a new fluid-injected motor, giving finer control than the previous four nozzle system.
    Performance improvements realized in Minuteman-III include increased flexibility in reentry vehicle (RV) and penetration aids deployment, increased survivability after a nuclear attack, and increased payload capacity.

      Minuteman-III contains the following distinguishing features:
        A larger third-stage motor to increase range.
        A fixed nozzle with a liquid injection TVC system on the new third-stage motor (similar to the second-stage Minuteman-II nozzle) to increase range.
        A RS capable of deploying penetration aids (chaff) and up to three RVs to increase payload delivery.
        An added post-boost propulsion system (the Propulsion System Rocket Engine, or PSRE) to increase range and maneuver the RS. This maneuverability allows the RS to be positioned at selected locations prior to the deployment of its RVs and penetration aids.
        Improved electronics in the guidance system to provide more computer memory and greater accuracy, and to reduce vulnerability to a nuclear environment.

    The Minuteman-III Honeywell HDC-701 flight computer used NDRO (non-destructive read out) plated wire memory instead of rotating magnetic disk for primary storage.

    The Guidance Replacement Program (GRP), initiated in 1993, flight computer uses radiation-resistant semiconductor RAM.



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    Weapon system programs
      Rivet MILE — Minuteman Life Extension
      Rivet ADD — Modification of Minuteman-II launch facilities to hold MM III missiles
      Missile Defense - Kinetic Energy Interceptor (KEI, “space bullet”)

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    Influences
    The author Thomas Pynchon worked as a technical writer for the field support unit for the Minuteman missile, something that is probably reflected in the narrative of his novels The Crying of Lot 49 and ''Gravity’s Rainbow''.

    The Minuteman Missile National Historic Site in South Dakota has recently been created. It preserves a Launch Control Facility and a missile silo complex under the control of the National Park Service.

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    Mobile Minuteman program
    While the silo-based Minuteman was in development, the United States Air Force released details about a rail-based counterpart. On October 12 1959, details on the system, called the “Mobile Minuteman,” were released to the public. The system used the United States railroad network to help increase the system's survivability during nuclear attack. A performance test, code named Operation Big Star, was conducted from June 20 to August 27 1960 at Hill Air Force Base, Utah. The United States Air Force then activated the 4062nd Mobile Missile Wing on December 1 1960. The wing was to have three missile train squadrons, each with ten trains and each train carrying three missiles (30 missiles per squadron). Lack of support by the Kennedy Administration killed the Mobile Minuteman Program; on December 1 1961, the Department of Defense deleted the three mobile missile squadrons from its budget. The USAF officially deactivated the 4062nd Mobile Missile Wing on February 20 1962.

    The idea for a rail-based missile system was kept alive through the LGM-118A Peacekeeper Rail Garrison and the Soviet Union’s SS-24 Scalpel rail-based ICBM.

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    Emergency Rocket Communications System (ERCS)
    An additional part of the National Command Authority communication relay system was called the emergency rocket communication system (ERCS). Specially designed rockets called BLUE SCOUT carried radio-transmitting payloads high above the continental United States, to relay messages to units within line-of-sight. In the event of a nuclear attack, ERCS payloads would relay preprogrammed messages giving the “go-order” to SAC units. BLUE SCOUT launch sites were located at Wisner, West Point and Tekamah, Nebraska. These locations were vital for ERCS effectiveness due to their centralized position in the US, within range of all missile complexes. Later ERCS configurations were placed on the tops of modified Minuteman-II ICBMs (LGM-30Fs) under the control of the 510th Strategic Missile Squadron located at Whiteman Air Force Base, Missouri.

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    Satellite launching role
    The U.S. Air Force has considered using some decommissioned Minuteman missiles in a satellite launching role. These missiles would be stored in silos, for launch upon short notice. The payload would be variable, and would have the ability to be replaced quickly. This would allow a surge capability in times of emergency.

    See also Minotaur (rocket).

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    Missile Defense
    Minutemen modifications are being produced at Prime Machine in Salt Lake City, Utah as part of the Alliant Kinetic Energy Interceptor (KEI, a guided “space bullet”) portion of the USA’s missile defense program.

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    Minuteman 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 IV turnover
        New features approved
        Minuteman-II flight test
        GIANT BOOST
      1965
        Wing V turnover
        Vulnerability improvements
        Minuteman fully operational at Wing II, 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 electronics 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 Life Extension) 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
      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
      2000
      2001
        PRP deployment initiated


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