Missile Histories
Short histories of the missiles built for the three USAF Missiles project are listed below by their project type and operational dates. Multiple on-line sources were used, mostly from Wikipedia.
Douglas PGM-17 Thor IRBM was the first operational USAF ballistic missile. It had a liquid propelled Rocketdyne engine, with a height of 65 feet and diameter of 8 feet. Thor had a range of 2,300 miles and was operational from 1954-1963. It carried the W49 (1.44 megaton) warhead. Thor was deployed to and operated at Royal Air Force at sites in the United Kingdom. Thor was much more deployable than the Jupiter and could be transported in the Douglas C-124 Globemaster II and C-133 Cargomaster aircraft. Thor would later have a stellar career as a NASA booster rocket for multiple space programs.
Chrysler PGM-19 Jupiter IRBM was developed by the US Army Redstone Arsenal and the US Navy and was to be capable of being launched from a submarine. Navy involvement resulted in the final shape of the missile. The Navy withdrew from the Jupiter project and instead began development of the Polaris missile. Both the Jupiter and Thor IRBMs were produced after the launch of Sputnik by the USSR. Jupiter was later transferred from the US Army over to the USAF. Jupiter had a liquid propelled Rocketdyne engine, with a height of 60 feet and diameter of 8.75 feet. Jupiter had a range of 1,700 miles and was operational from 1956-1961. It carried the W38 (3.75 megaton) or W49 warhead. It used a “flower petal shelter” of wedge-shaped panels and was not easily transportable, resulting in its early phase-out in favor of the Thor. Jupiter was based at sites in Italy and Turkey.
Convair/General Dynamics SM-65 Atlas ICBM was the first operational ICBM developed by the USAF. It had two liquid-prolled Rocketdyne booster engines in a “skirt stage” and one central sustainer engine. Atlas had a height of 75 feet and diameter of 16 feet. Atlas was originally designated as the XB-65 experimental bomber. In 1955 it was redesignated SM-65 (“Strategic Missile 65”) and in 1962 became CGM-16. The A, B and C versions were developmental rockets, with the D, E and F being operational versions. The Atlas D carried the W49 warhead in the Mk 2 and 3 RV and the Atlas E and F carried the W38 warhead in the Mk 4 RV. Atlas had a range of 9,000 miles and was operational from 1959-1965. The Atlas booster was used by NASA for the four Mercury-Atlas manned flights during the Project Mercury space program.
Martin LGM-25C Titan ICBM program was begun as a back-up in case there were delays with the SRM‑65 Atlas missile. SM-68A/HGM-25A Titan I was the USAF’s first multi-stage ICBM and had liquid-propelled Aerojet engines. It was originally designated as the B-68 bomber, which was changed to the SM-68 Titan and then later to HGM-25A. Titan I had a Mk 4 re-entry vehicle containing a W38 warhead and was deployed in five western states. Titan had a height of 103 feet and diameter of 10 feet. It was in service from 1959 to 1962, being replaced by the improved LGM-25C Titan II. The Titan’s major improvement over Atlas was being stored vertically in underground silos. The Titan II used hypergolic propellants that could be stored in the missile, unlike the Titan I that had to be fueled immediately before launch. The Titan II doubled the load of the Titan I and carried six W53 warheads, and had a range of 10,000 miles. It was in service from 1962 to 1987 at locations in four states, being phased-out when the Minuteman came on board. Titan I boosters were all scrapped, except for museum missiles. The Titan II booster was used by NASA for ten Gemini-Titan manned flights during the Project Gemini space program and also multiple reconnaissance satellites and interplanetary probes throughout the solar system. “LGM” stands for silo-launched (L), ground targets (G), and guided missile (M). 108 Titan II ICBMs were produced.
Boeing LGM-30 Minuteman ICBM was the USAF’s first solid-propelled ICBM and had three stages. The LGM‑30A and B Minuteman I were in service from 1962 to 1969 at one USAF base, carried one W59 warhead, and had a range of 5,500 miles. The LGM-30F Minuteman II was in service from 1965 to 1994 at four USAF bases, carried one W56 warhead, was 57.6 feet tall, and had a range of 6,300 miles. The final and current LGM-30G Minuteman III version entered service in 1970, can carry up to three Mk 12 multiple independently-targetable RVs (MIRV) with W62, W78, or W87 warheads, is 59.9 feet tall, and has a range of 8,700 miles. Under the START Treaty the Minuteman III carries only one warhead. There are currently 450 Minuteman IIIs operational at three USAF bases.
Boeing LMG-118 Peacekeeper ICBM was a three-stage solid-propelled ICBM deployed by the U.S. from 1985 to 2005. It was originally known as the “MX” for Missile, Experimental. The missile was MIRV-capable and could carry up to twelve Mark 21 RVs (normally carried ten) each armed with a 300-kiloton W87 warhead, plus decoys. It was 72 feet tall and had a range of 6,000 miles. Initial plans called for building and deploying 100 Peacekeepers, but budgetary concerns eliminated the final procurement and only 50 entered service. It was based in re-fitted Minuteman silos at Francis E. Warren AFB in Wyoming. Disarmament treaties signed after the Peacekeeper’s development led to its withdrawal from service in 2005. The W87 warheads were re-used on Minuteman IIIs.