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MGM-13 Mace

The Martin Mace was a ground-launched cruise missile developed from the earlier Martin TM-61 Matador. It used a new self-contained navigation system that eliminated the need to get updates from ground-based radio stations, and thereby allowed it to fly further beyond the front lines. To take advantage of this longer practical range, Mace was larger than Matador and could travel a longer total distance.

CGM/MGM-13 Mace
CGM-13 test launch at Cape Canaveral
Role Cruise missile
Manufacturer Glenn L. Martin Company
First flight 1956
Introduction 1959
Retired Early 1970s
Status Retired
Primary user United States Air Force
Developed from MGM-1 Matador

The original A model used a ground-mapping radar system which required the missile to fly at low to medium altitudes. In 1959 a new inertial navigation system was introduced that offered similar accuracy but had no altitude limitation. By flying at higher altitudes the missile's range almost doubled with no other changes. This led to the B model of 1961, which was limited to fixed launching sites, unlike the A model's mobile trailers.

Mace was replaced by the MGM-31 Pershing missile by then Secretary of Defence Robert McNamara, and later in its role as a cruise missile for West Germany, by the BGM-109G Ground Launched Cruise Missile.[1]

Introduced during a period of changing nomenclature, they were originally designated TM-76A and TM-76B for "tactical missile" until 1963, then as MGM-13A for Mobile Ground-launched Missile and CGM-13 for Coffin Ground-launched Missile.

History edit

Matador edit

The MGM-1 Matador was essentially an updated version of the V-1 flying bomb, replacing the V-1's pulsejet with a much more efficient turbojet engine. This allowed the missile to travel much longer distances. At the time, inertial navigation systems (INS) could not provide the desired 1 mile (1.6 km) accuracy at these longer distances, so Matador used a simple autopilot that was updated with corrections radioed to it from ground-based radar stations spread along its path. This system had the obvious disadvantage that it could only attack targets within a certain range of the ground-based stations; as the missile continued on its last path it would grow increasingly inaccurate. While this made it useful for attacks against targets near the front, like troop concentrations, it meant more important targets beyond the front, like airbases, might be too far to effectively attack. It also meant the system was subject to enemy jamming as well as more mundane issues with radio reception.

Mace A edit

In the early 1950s, Goodyear Aircraft Corporation began the development of the ATRAN (Automatic Terrain Recognition And Navigation) navigation system. This was based on taking photographs of a radar display at key points along the flight path of a radar-equipped aircraft. The photographs were automatically taken at timed intervals using a 35mm film movie camera. The film was then placed in the missile, which was equipped with the same radar system. At timed intervals, the movie would advance a frame while being moved horizontally across the radar display. At some point during the movement, the light output is maximized, indicating the position where the film most closely matches the display. The angle of the film at that instant indicates the direction the missile needs to turn to return to its pre-planned route.

ATRAN had the advantage that it was not subject to a maximum range or jamming issues, and in theory, could attack any target within range of the missile. It had the significant disadvantage that it could only attack pre-selected targets, unlike the radio system which would be directed at any target at any time. Any particular missile could be directed at a selected target by changing the film, but targets of opportunity could not be attacked unless they happened to lie along an existing path. Moreover, as the system compared the radar image to one made prior to flight, it was difficult to make maps much beyond the peacetime borders. This was later addressed by developing a method that used small models based on topographical maps to produce the films for any given flight, allowing the missile to follow paths that could not be pre-flown.

The ATRAN system was experimentally fit to a Matador beginning in August 1952. This led to a production contract in June 1954 for what was initially known as TM-61B Matador B. To take advantage of the potential range, Matador was modified with a longer fuselage to hold more fuel and modified the wings to be shorter. All-up weight increased to 18,750 pounds (8,500 kg) and range increased to 800 miles (1,300 km). To enhance mobility, Martin designed the Mace's wings to fold for transport, whereas the Matador's wings were transported separately and then bolted on for flight. Flight testing began in 1956, and the missile received its new name in early 1958.

USAF deployed the Mace "A" in West Germany in 1959 at Sembach Air Base, where it briefly served alongside the Matador before the latter was phased out of service in 1962. A total of 6 active missile squadrons were eventually equipped with the Mace "A" at Sembach Air Base and Hahn Air Base under the 38th Tactical Missile Wing. In South Korea, the 58th Tactical Missile Group became combat-ready with 60 TM-61s in January 1959. It ceased operations in March 1962, a few months after the 498th Tactical Missile Group in December 1961 took up positions in semi-hardened sites on Okinawa.

Mace B edit

Rapid development in guidance systems quickly rendered ATRAN obsolete. In 1959, a modified version replacing ATRAN with the AC Spark Plug AChiever INS was developed as TM-76B. A major advantage was that the ATRAN radar system scanned the horizon in front of the missile and thus had to fly at low altitudes in order to produce enough vertical relief. By moving to a pure INS, there was no longer any limitation on altitude and by flying higher the range increased to about 1,300 miles (2,100 km) with no other changes. The downside to the INS approach is that it requires an accurate survey of the launch point, so the system could no longer be mobile. This led to the B models being launched from hardened "coffin" launchers. The first TM-76B launch was on 11 July 1960.

Mace "B" missiles began were first deployed to Okinawa in 1961[2] and remained operational in Europe and the Pacific. The two squadrons of TM-76B/CGM-13C continued on active duty in USAFE until December 1969. After being taken offline, some missiles were used as target drones because their size and performance resembled crewed aircraft.

Variants edit

YTM-61B Matador B
Development missiles. Redesignated YTM-76 Mace in 1958, and later MGM-13A Mace in 1963 (not to be confused with the 1964 MGM-13A).[3]
QYTM-61B Matador B
Recoverable test vehicles. The "Q for drone" mission modifier before the "Y for test" status prefix was unusual, but appeared on official documents.[3]
TM-76A Mace A
First production version, equipped with ATRAN terrain-matching radar navigation. Redesignated MGM-13B in 1963, and later MGM-13A in 1964.[3]
TM-76B Mace B
Version with an inertial navigation system and increased range. Redesignated CGM-13C in 1963, and later CGM-13B in 1964.[3]

Locations edit

Mace A and B types have been deployed in Japan and former West-Germany

  • Japan, Okinawa island: 873d Tactical Missile Squadron kept 32 Mace missiles on constant alert in underground bunkers at 4 Okinawa launch sites assigned to Kadena Airbase and located at Bolo Point in Yomitan, Onna Point, White Beach and at Kin just north of Camp Hansen.
  • West Germany: 38th Tac Msl Wing kept 90 missiles on alert at above and underground launcher sites assigned to Sembach Airbase (sites at Mehlingen, Enkenbach and Grünstadt); to Hahn Airbase (sites at Wüscheim, Kirchberg and Hundheim) and to Bitburg Airbase (sites at Steinborn, Idenheim and Rittersdorf)

Survivors edit

 
Mace at Warner Robins Museum of Aviation, Georgia
 
Mace at Belleview Park in Englewood, Colorado

Below is a list of locations which have a Mace missile in their collection or on display:

Specifications edit

General characteristics

  • Length: 44 ft 6 in;13.6 m
  • Diameter: 4 ft 6 in;1.4 m

Engine

Technical information

Performance

  • Cruise speed: 650 mph (570 kn, 1,000 km/h)
  • Operating altitude: 750 to 40,000 ft (230 to 12,000 m)
  • Range: 1,400 mi (1,200 nmi, 2,300 km)

Warhead

  • Warhead: W28 thermonuclear warhead

See also edit

Related development

  • MGM-1 Matador – (United States)

Related lists

References edit

  • Mindling, George, and Bolton, Robert, 'U.S. Air Force Tactical Missiles 1949–1969 The Pioneers', 2008, Lulu Press
  1. ^ Lanning, Randall L. (15 April 1992). United States Air Force Ground Launched Cruise Missiles: A Study in Technology, Concepts, and Deterrence. Air War College, United States Air Force. AD-A258 351.
  2. ^ . Air Force Space and Missile Museum. Archived from the original on 7 December 2014. Retrieved 5 December 2014.
  3. ^ a b c d "Martin MGM/CGM-13 Mace". www.designation-systems.net. Retrieved 25 May 2023.
  4. ^ "MARTIN MGM-13A "MACE"", , Museum of Aviation, archived from the original on 24 June 2016.
  5. ^ US Air Force Museum Foundation. US Air Force Museum. p. 94.
  6. ^ Indiana Military Museum.
  7. ^ "Martin TM-76 Mace - Englewood, Colorado - Static Aircraft Displays on Waymarking.com". www.waymarking.com.
  8. ^ "Matador, Mace", , archived from the original on 21 January 2013, retrieved 4 January 2013.
  9. ^ "Mildred, PA - MGM-13 Mace Missile". RoadsideAmerica.com.
  10. ^ "CGM-13B Mace Missile Historical Marker". www.hmdb.org. Retrieved 27 August 2020.

External links edit

  • Directory of U.S. Military Rockets and Missiles
  • Part One - The Development of the Matador and Mace Missiles
  • Part Two - History of the Matador and Mace Missiles
  • Part Three - Matador and Mace Missile Guidance and Flight Controls
  • The FWD MM-1 Teracruzer
  • Sembach Missileers - 38th TAC Missile Wing Missileers stationed at Sembach AB, Germany, 1959-1966
  • TAC Missileers - Tactical Missile Warriors of the Cold War
  • Mace - Federation of American Scientists

mace, this, article, about, 1960, force, ground, launched, nuclear, cruise, missile, planned, navy, launched, conventional, cruise, missile, multi, mission, affordable, capacity, effector, this, article, includes, list, general, references, lacks, sufficient, . This article is about the 1960 s era U S Air Force ground launched nuclear cruise missile For the planned U S Navy air launched conventional cruise missile see Multi mission Affordable Capacity Effector This article includes a list of general references but it lacks sufficient corresponding inline citations Please help to improve this article by introducing more precise citations September 2021 Learn how and when to remove this message The Martin Mace was a ground launched cruise missile developed from the earlier Martin TM 61 Matador It used a new self contained navigation system that eliminated the need to get updates from ground based radio stations and thereby allowed it to fly further beyond the front lines To take advantage of this longer practical range Mace was larger than Matador and could travel a longer total distance CGM MGM 13 Mace CGM 13 test launch at Cape Canaveral Role Cruise missile Manufacturer Glenn L Martin Company First flight 1956 Introduction 1959 Retired Early 1970s Status Retired Primary user United States Air Force Developed from MGM 1 Matador The original A model used a ground mapping radar system which required the missile to fly at low to medium altitudes In 1959 a new inertial navigation system was introduced that offered similar accuracy but had no altitude limitation By flying at higher altitudes the missile s range almost doubled with no other changes This led to the B model of 1961 which was limited to fixed launching sites unlike the A model s mobile trailers Mace was replaced by the MGM 31 Pershing missile by then Secretary of Defence Robert McNamara and later in its role as a cruise missile for West Germany by the BGM 109G Ground Launched Cruise Missile 1 Introduced during a period of changing nomenclature they were originally designated TM 76A and TM 76B for tactical missile until 1963 then as MGM 13A for Mobile Ground launched Missile and CGM 13 for Coffin Ground launched Missile Contents 1 History 1 1 Matador 1 2 Mace A 1 3 Mace B 2 Variants 3 Locations 4 Survivors 5 Specifications 6 See also 7 References 8 External linksHistory editMatador edit The MGM 1 Matador was essentially an updated version of the V 1 flying bomb replacing the V 1 s pulsejet with a much more efficient turbojet engine This allowed the missile to travel much longer distances At the time inertial navigation systems INS could not provide the desired 1 mile 1 6 km accuracy at these longer distances so Matador used a simple autopilot that was updated with corrections radioed to it from ground based radar stations spread along its path This system had the obvious disadvantage that it could only attack targets within a certain range of the ground based stations as the missile continued on its last path it would grow increasingly inaccurate While this made it useful for attacks against targets near the front like troop concentrations it meant more important targets beyond the front like airbases might be too far to effectively attack It also meant the system was subject to enemy jamming as well as more mundane issues with radio reception Mace A edit In the early 1950s Goodyear Aircraft Corporation began the development of the ATRAN Automatic Terrain Recognition And Navigation navigation system This was based on taking photographs of a radar display at key points along the flight path of a radar equipped aircraft The photographs were automatically taken at timed intervals using a 35mm film movie camera The film was then placed in the missile which was equipped with the same radar system At timed intervals the movie would advance a frame while being moved horizontally across the radar display At some point during the movement the light output is maximized indicating the position where the film most closely matches the display The angle of the film at that instant indicates the direction the missile needs to turn to return to its pre planned route ATRAN had the advantage that it was not subject to a maximum range or jamming issues and in theory could attack any target within range of the missile It had the significant disadvantage that it could only attack pre selected targets unlike the radio system which would be directed at any target at any time Any particular missile could be directed at a selected target by changing the film but targets of opportunity could not be attacked unless they happened to lie along an existing path Moreover as the system compared the radar image to one made prior to flight it was difficult to make maps much beyond the peacetime borders This was later addressed by developing a method that used small models based on topographical maps to produce the films for any given flight allowing the missile to follow paths that could not be pre flown The ATRAN system was experimentally fit to a Matador beginning in August 1952 This led to a production contract in June 1954 for what was initially known as TM 61B Matador B To take advantage of the potential range Matador was modified with a longer fuselage to hold more fuel and modified the wings to be shorter All up weight increased to 18 750 pounds 8 500 kg and range increased to 800 miles 1 300 km To enhance mobility Martin designed the Mace s wings to fold for transport whereas the Matador s wings were transported separately and then bolted on for flight Flight testing began in 1956 and the missile received its new name in early 1958 USAF deployed the Mace A in West Germany in 1959 at Sembach Air Base where it briefly served alongside the Matador before the latter was phased out of service in 1962 A total of 6 active missile squadrons were eventually equipped with the Mace A at Sembach Air Base and Hahn Air Base under the 38th Tactical Missile Wing In South Korea the 58th Tactical Missile Group became combat ready with 60 TM 61s in January 1959 It ceased operations in March 1962 a few months after the 498th Tactical Missile Group in December 1961 took up positions in semi hardened sites on Okinawa Mace B edit Rapid development in guidance systems quickly rendered ATRAN obsolete In 1959 a modified version replacing ATRAN with the AC Spark Plug AChiever INS was developed as TM 76B A major advantage was that the ATRAN radar system scanned the horizon in front of the missile and thus had to fly at low altitudes in order to produce enough vertical relief By moving to a pure INS there was no longer any limitation on altitude and by flying higher the range increased to about 1 300 miles 2 100 km with no other changes The downside to the INS approach is that it requires an accurate survey of the launch point so the system could no longer be mobile This led to the B models being launched from hardened coffin launchers The first TM 76B launch was on 11 July 1960 Mace B missiles began were first deployed to Okinawa in 1961 2 and remained operational in Europe and the Pacific The two squadrons of TM 76B CGM 13C continued on active duty in USAFE until December 1969 After being taken offline some missiles were used as target drones because their size and performance resembled crewed aircraft Variants editYTM 61B Matador B Development missiles Redesignated YTM 76 Mace in 1958 and later MGM 13A Mace in 1963 not to be confused with the 1964 MGM 13A 3 QYTM 61B Matador B Recoverable test vehicles The Q for drone mission modifier before the Y for test status prefix was unusual but appeared on official documents 3 TM 76A Mace A First production version equipped with ATRAN terrain matching radar navigation Redesignated MGM 13B in 1963 and later MGM 13A in 1964 3 TM 76B Mace B Version with an inertial navigation system and increased range Redesignated CGM 13C in 1963 and later CGM 13B in 1964 3 Locations editMace A and B types have been deployed in Japan and former West Germany Japan Okinawa island 873d Tactical Missile Squadron kept 32 Mace missiles on constant alert in underground bunkers at 4 Okinawa launch sites assigned to Kadena Airbase and located at Bolo Point in Yomitan Onna Point White Beach and at Kin just north of Camp Hansen West Germany 38th Tac Msl Wing kept 90 missiles on alert at above and underground launcher sites assigned to Sembach Airbase sites at Mehlingen Enkenbach and Grunstadt to Hahn Airbase sites at Wuscheim Kirchberg and Hundheim and to Bitburg Airbase sites at Steinborn Idenheim and Rittersdorf Survivors edit nbsp Mace at Warner Robins Museum of Aviation Georgia nbsp Mace at Belleview Park in Englewood Colorado Below is a list of locations which have a Mace missile in their collection or on display Air Force Space amp Missile Museum Cape Canaveral Air Force Station Florida TM 76B CGM 13B AF Ser No 60 0715 but restored and marked as AF Ser No 59 4871 Originally assigned to the U S Air Force Tactical Missile School 4504th Missile Training Wing Orlando Air Force Base Florida Air Force Armament Museum Eglin Air Force Base Florida CGM 13 AF Ser No 59 4860 Museum of Aviation Robins Air Force Base Georgia MGM 13A AF Ser No 58 1465 4 National Museum of the United States Air Force Wright Patterson Air Force Base Dayton Ohio This Mace B was based on Okinawa prior to its delivery to the museum in 1971 5 Indiana Military Museum Vincennes Indiana CGM 13B AF Ser No 59 4871 This Mace B was assigned to the 4504th Missile Training Wing Orlando AFB Florida 6 Belleview Park Englewood Colorado Elevated outdoor display AF Serial Number is unknown Donated to the city by the Martin Company in the 1960s for use as playground equipment 7 White Sands Missile Range Museum New Mexico 8 Flagler Memorial Park Flagler Colorado Mace A elevated and fenced display AF Ser No 58 1463 McDermott Post 452 American Legion Mildred Pennsylvania 9 Ida County Veterans Memorial Ida Grove IA 10 Specifications editGeneral characteristics Length 44 ft 6 in 13 6 m Diameter 4 ft 6 in 1 4 m Engine First stage 1 Thiokol solid rocket booster 100 000 lbf 445 kN Thrust Second stage 1 Allison J33 A 41 turbojet 5 200 lbf 23 kN Thrust Technical information Launch platform MGM 13A transporter erector launcher CGM 13B underground bunker Performance Cruise speed 650 mph 570 kn 1 000 km h Operating altitude 750 to 40 000 ft 230 to 12 000 m Range 1 400 mi 1 200 nmi 2 300 km Warhead Warhead W28 thermonuclear warheadSee also editRelated development MGM 1 Matador United States Related lists List of military aircraft of the United States List of missilesReferences editMindling George and Bolton Robert U S Air Force Tactical Missiles 1949 1969 The Pioneers 2008 Lulu Press Lanning Randall L 15 April 1992 United States Air Force Ground Launched Cruise Missiles A Study in Technology Concepts and Deterrence Air War College United States Air Force AD A258 351 Mace B Air Force Space and Missile Museum Archived from the original on 7 December 2014 Retrieved 5 December 2014 a b c d Martin MGM CGM 13 Mace www designation systems net Retrieved 25 May 2023 MARTIN MGM 13A MACE Aircraft collection Museum of Aviation archived from the original on 24 June 2016 US Air Force Museum Foundation US Air Force Museum p 94 Indiana Military Museum Martin TM 76 Mace Englewood Colorado Static Aircraft Displays on Waymarking com www waymarking com Matador Mace WSMR History archived from the original on 21 January 2013 retrieved 4 January 2013 Mildred PA MGM 13 Mace Missile RoadsideAmerica com CGM 13B Mace Missile Historical Marker www hmdb org Retrieved 27 August 2020 External links edit nbsp Wikimedia Commons has media related to Martin Mace Directory of U S Military Rockets and Missiles Part One The Development of the Matador and Mace Missiles Part Two History of the Matador and Mace Missiles Part Three Matador and Mace Missile Guidance and Flight Controls The FWD MM 1 Teracruzer Sembach Missileers 38th TAC Missile Wing Missileers stationed at Sembach AB Germany 1959 1966 TAC Missileers Tactical Missile Warriors of the Cold War Mace Federation of American Scientists Retrieved from https en wikipedia org w index php title MGM 13 Mace amp oldid 1221131142, 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