| BGM-109G Gryphon (GLCM)1 | |
|---|---|
BGM-109G Gryphon Transporter Erector Launcher (TEL) showing 4 missile launch tubes |
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| Type | long-range, all-weather, subsonic tactical/strategic cruise missile |
| Service history | |
| In service | 1983–1991 |
| Production history | |
| Manufacturer | General Dynamics |
| Unit cost | $1.3 mil |
| Specifications | |
| Weight | 1,200 kilograms (2,600 lb) |
| Length | Without booster:5.56 metres (18.2 ft) |
| Diameter | 0.52 metres (1.7 ft) |
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| Engine | Williams International F107-WR-400 turbofan using TH-dimer fuel and a solid-fuel booster |
| Wingspan | 2.67 metres (8.8 ft) |
| Operational range |
2,500 kilometres (1,600 mi) |
| Speed | Subsonic—880 kilometres per hour (550 mph) |
| Guidance system |
Inertial, TERCOM |
| Launch platform |
Transporter erector launcher |
The Ground Launched Cruise Missile, or GLCM, (officially designated BGM-109G Gryphon) was a ground-launched cruise missile developed by the United States Air Force in the last decade of the Cold War.
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The BGM-109G was developed as a counter to the mobile medium- and intermediate- range ballistic nuclear missiles deployed by the Soviet Union in Eastern Bloc European countries. The GLCM and the U.S. Army's Pershing II were the incentives that fostered Soviet willingness to sign the Intermediate-Range Nuclear Forces Treaty (INF treaty), and thus eventually reduced both the number and the threat of nuclear warheads in Europe. GLCM is also a generic term for any ground-launched cruise missile. Since the US deployed only one modern cruise missile in the tactical role, the GLCM name stuck. The GLCM was built by General Dynamics.
A conventionally-configured cruise missile, the BGM-109 was essentially a small, pilotless flying machine, powered by a turbofan engine. Unlike ballistic missiles, whose aimpoint is usually determined by gravitic trajectories, a cruise missile is capable of complicated aerial manoeuvres, and can fly a range of predetermined flight plans. Also, it flies at much lower altitudes than a ballistic missile, typically with a terrain-hugging flight plan. The trade-off for this low-observability flight is strike time; cruise missiles travel far more slowly than a ballistic weapon, and the GLCM was typical in this regard.
GLCM was developed as a ground-launched variant of the Tomahawk missile in use by the U.S. Navy (along with an undeveloped air-launched version, the Medium Range Air to Surface Missile [MRASM].) Unlike other variants of the Tomahawk, the GLCM carried only a nuclear warhead; no conventional capability was provided. The W84 warhead was a variable-yield kiloton-range weapon. Some estimates put the yield at between 10 and 50 kt. This tactical warhead contrasts with the W80 warhead found on other versions of the Tomahawk, and on the ALCM, which had a yield of 200 kt.2 The Pentagon credited the GLCM with a range of 2000–2500 kilometers. Like other US cruise missiles of this period, accuracy after more than 2000 km of flight was within half the width of a football field or 100 ft (approximately 30 meters). The missile was entirely subsonic, powered by a turbofan engine with a rocket booster assisting at launch.3
Militarily, the GLCM was targeted against fixed targets—at the outer edge of its range, the missile's flight time with its subsonic turbofan was more than 2½ hours. The missiles were launched from an elevated launcher, with the missile ejected from its cannister for about 13 seconds of solid rocket booster flight. The fins extended at 4 seconds, the air inlet and wings deployed at 10 seconds and the jet engine started at the end of the boost phase. Flying at low level, the missile was guided by TERCOM (terrain contour matching) to the target. 3
This contrasted sharply with Pershing II, which had a flight time of 10–15 minutes. However, the range of the GLCM gave it the ability to strike deep within then-Soviet territory, and the weapon's guidance, and low RCS would have made it far more difficult to intercept a GLCM even if the launch were detected in time.
BGM-109G personnel were trained at Davis Monthan AFB, Arizona, by the 868th Tactical Missile Training Squadron from 1 July 1981 to 1 October 1985, when it became the 868th Tactical Missile Training Group. The group was deactivated on 31 May 1990. An area near Fort Huachuca was used for field training for GLCM flights. GLCM testing was conducted at Dugway Proving Ground in Utah, with many of the people involved in the testing going to operational wings as they were activated.
BGM-109G missiles would be based at six locations throughout Europe; in the United Kingdom (at RAF Greenham Common and RAF Molesworth), Belgium, Netherlands, Germany, and Comiso Air Station in Italy. Each location had its own unique problems, but all required extensive construction by the USAF. Initial operating capability (or IOC) occurred in 1983.4
Normal basing was in shelters at military installations. Each BGM-109G station was controlled by a Wing, that consisted of a Tactical Missile Squadron (TMS) which was responsible for operation and deployment of the missiles, and a Tactical Missile Maintenance Squadron (TMMS) which was responsible for the support of the system. Each TMS consisted of several flights, made up of 69 people and 22 vehicles.4
The missile was designed to operate in a flight with sixteen missiles. The flight would be normally on base, with the missiles and vehicles secured in the hardened storage area called the GAMA (GLCM Alert and Maintenance Area).
Four transporter erector launchers (TEL) each carried four BGM-109G missiles in their containers and ready for launch. Two launch control centers (LCC), each with two launch officers, were connected to the TELs and interconnected for launch. Each TEL and LCC was towed by a large MAN AG 8 X 8 tractor and was capable of traversing rough terrain. There were 16 support vehicles for the flight commander, normally a captain, 19 maintenance technicians, a medical technician and 44 security personnel.4
During periods of increased tension, the flights would be deployed to pre-surveyed, classified locations in the countryside away from the base. The members of the flight would dig in, erect camouflage netting to hide the vehicles and prepare for launch. Flight commanders were tasked to survey and select more than one possible deployment site, with all details closely held, and the commander selected the location preferred when the flight deployed from the base. When deployed, the flight was self sustaining, and secured with special intrusion detection radar. The launchers (sans warheads) were sent out on a number of simulated scrambles.4
Although deployed in the face of a range of Soviet IRBMs, including the brand-new and extremely capable SS-20 Saber, the GLCM (sometimes referred to by its phonetic nickname, Glick-em) faced widespread public protest in Europe. Many anti-nuclear Europeans felt that the United States was deploying weapons meant to win a tactical nuclear war, without adequate consideration of the effects that even a 'victory' would bring. Critics also argued that the Reagan Administration was unduly escalating tensions in Central Europe. Between them, GLCM and Pershing II made a lethal combination. GLCM missiles could be launched, undetected, followed 2 hours later by a Pershing strike, which would fly so quickly that it was possible no response could be made before the Pershings struck. Aside from presenting an attractive course of action to NATO commanders in the event of Soviet aggression, it put the Kremlin leaders (in range of the GLCM and possibly the Pershing, even in Moscow) in a position of fearing a decapitating NATO first strike, which could have moved them toward a launch on warning policy as the only way to maintain deterrence.5 However, the USSR did have submarine-launched missiles (i.e. Golf and Hotel class SSBNs armed with R-27 Zyb and SS-N-5s) available during this time, so any fears of a decapitating first strike were not necessarily justified.[1]
Ironically, and despite the protesters' fears to the contrary, the deployment of GLCM actually brought greater stability to Central Europe, and lessened the incentive/need for a tactical nuclear exchange, through the mechanism of the INF treaty. The recognition by Soviet leaders of the threat posed by the GLCM and Pershing II missiles made them far more inclined to agree to negotiate their own intermediate-range weapons, especially the SS-20, out of service, in exchange for the elimination of the threat posed by the GLCM and the Pershing II.6
Unlike SALT II or START I, which set limits to maximum nuclear arsenals, the INF Treaty banned whole categories of intermediate-range tactical nuclear weapons outright. All ground-launched cruise missiles and ballistic missiles with ranges greater than 500 but less than 5500 kilometers were barred to the U.S. and USSR under this treaty. This meant the withdrawal of GLCM and Pershing II on the American side; the Soviets withdrew the SS-4 Sandal, SS-5 Skean, SS-12 Scaleboard, SS-20 Saber, SS-22 Scaleboard B, and SS-23 Spider MRBM/IRBM/LRBM ballistic missiles, in addition to the GLCM's most direct counterpart: the SSC-4 (dubbed the Tomahawksi in the Western press) and its supersonic follow-on, the SSC-X-5 cruise missiles.7
GLCM was removed from Europe beginning in 1988, and over the next three and a half years all units were transported to Davis Monthan AFB and destroyed or converted into displays by 1991. Eight missiles survive for inert static display only. No follow-on design has been authorized.8
Note: Each GLCM squadron was further subdivided into several flights. Each flight included 2 Launch Control Vehicles (LCC) and 4 Transporter Erector Launchers (TEL), totalling 16 missiles per flight. Each TEL could carry 4 missiles. [3][4]
This article incorporates public domain material from websites or documents of the Air Force Historical Research Agency.