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IRCM
Subtopics
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A8 German ballistic missile. Planned stretched version of the V-2 with storable propellants. Never reached the hardware stage, but design continued after the war in France as the 'Super V-2'. |
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A6 German intermediate range cruise missile. The A6 designation was applied to a version of the A5 subscale V-2 using alternate propellants. It also seems to have been applied to a manned, ramjet-powered version of the A9 winged V-2. |
BQ-3 American intermediate range cruise missile. In October 1942, Fairchild received a contract to build two XBQ-3 prototype unmanned assault drones based on the AT-21 Gunner twin-engined trainer design. |
BQ-4-TDR Early family of American unmanned remotely-controlled aircraft for use in combat. |
BQ-8 American intermediate range cruise missile. In 1944 the USAAF intended to convert some worn-out Consolidated B-24D/J Liberator bombers to BQ-8 radio-controlled assault drones for use against heavily defended targets on Japanese islands in the Pacific. The concept was the same as used for the B-17 Flying Fortress conversions in the BQ-7 Aphrodite project. |
Aphrodite American intermediate range cruise missile. In July 1944, the USAAF implemented the idea to convert "war-weary" B-17 Flying Fortress bombers to radio-controlled assault drones. About 25 B-17s, mostly B-17F, were converted to BQ-7 configuration under program Aphrodite. The BQ-7 was to be flown from Great Britain against very hardened or heavily defended German targets - submarine pens or V-1 missile sites. |
F6F-5K American intermediate range cruise missile, modification of F6F fighter. |
BQM-6C American intermediate range cruise drone. Drone version. |
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Navaho SSM-A-2 American intermediate range cruise missile. The first version of the Navaho developed in 1946-1950 was a Mach-3 ramjet vehicle with an integral rocket booster. Completion of the vehicle was cancelled in 1950 but the engine was used to power the Redstone ballistic missile. |
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Matador American intermediate range cruise missile by Glenn L. Martin. |
Taurus SSM-N-4 Interim long-range cruise missile considered by the US Navy in 1946-1948, an unmanned version of the AJ-1 Savage carrier-based bomber. |
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G-3 German aerodynamicist Albring designed the G-3 missile for the Russians in October 1949. This would use a rocket-powered Groettrup-designed G-1 as the first stage. The cruise stage would have an aerodynamic layout like that of the Saenger-Bredt rocket-powered antipodal bomber of World War II. Cruising at 13 km altitude, the supersonic missile would carry a 3000 kg warhead to a range of 2900 km. |
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Navaho X-10 American intermediate range cruise missile. Reusable, conventional airfield takeoff-and-landing aerodynamic test vehicle for Navaho missile. |
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Navaho G-26 American intermediate range cruise missile. The Navaho G-26 was a 2/3 scale test version of the operational Navaho G-38. The Navaho program was cancelled on 13 July 1957, but already-built G-26 test missiles were flown to the end of 1958. |
MGM-1A American intermediate range cruise missile. |
MGM-1B American intermediate range cruise missile. |
MGM-1C American intermediate range cruise missile. |
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EKR Russian intermediate range cruise missile. B Chertok of NII-8 took the preliminary German R-13 cruise missile design and elaborated it, including consideration of the key problem of long-range automatic astronavigation. By 1951 to 1953 Korolev's design bureau had prepared an experimental design, the EKR. I Lisovich had developed a prototype astronavigation system that met the necessary specifications, and solution of basic problems in use of steel and titanium hot airframe technology had been solved at VIAM (All-Union Institute of Aviation Materials) and MVTU Bauman Institute. An expert commission in 1953 examined the EKR design and felt that there were still many technical problems to be solved, most of which were better handled by an aircraft designer rather than Korolev. |
Rigel SSM-N-6 American Navy pioneering cruise missile project. Development started in 1943. Program cancelled in 1953. |
RS Russian intermediate range cruise missile. Soviet Mach 3 manned air-launched ramjet aircraft, developed in 1954-1961, but cancelled before the first full-scale test article could be flown. |
Triton US Navy ship- and sub-to-surface cruise ramjet-powered supersonic missile. Development started in 1946. Program cancelled in 1957. |
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Regulus 2 American supersonic sub-to-surface intermediate-range cruise missile, development started in 1953. Program cancelled in 1958 in deference to Polaris project. |
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Hound Dog First American air-launched cruise missile to become operational. Based on Navaho technology. |
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Mace American intermediate range cruise missile. Intermediate range cruise missile. Only Cape Canaveral launches are listed here, but over 30 launches were also conducted from Launch Area Able-51 by Detachment 1, 4504th CCTW at Holloman AFB, New Mexico from October 1959 through 1963. |
CGM-13A American intermediate range cruise missile. |
AGM-28A American intermediate range cruise missile. |
Tu-121 Russian intermediate range cruise missile. Mach 3 intermediate range cruise missile, tested in 1958-1960 before cancellation. |
AGM-28B American intermediate range cruise missile. |
CGM-13B American intermediate range cruise missile. |
P-205 Russian intermediate range cruise missile. Development of a family of long-range cruise missiles was begun in 1956 by Ilyushin. The P-205 was a land-based strategic cruise missile based on the P-20 antiship missile. The land-launch version was developed for the VVS in 1958-1960. There were two submarine projects for the missile, 627A and 653, both designed by OKB-143. Construction of the 627A submarine began at Severodvinsk, but the work on the submarine was cancelled in November 1961. |
P-6 Russian intermediate range cruise missile. |
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Regulus 1 American intermediate range subsonic cruise missile. The Regulus was the first strategic long-range nuclear-armed guided missile deployed by the US Navy. |
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BGM-110 American intermediate range cruise missile. Losing design in Sea-Launched Cruise Missile competition. Nuclear warhead version with warhead mass of 120 kg. |
Senior Prom American intermediate range stealth cruise missile. US Air Force program with test flights in 1978-1981. |
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Meteorit Russian intermediate range cruise missile. Development of three variants of this cruise missile was authorized on 9 December 1976. The Meteorit-M strategic version would be deployed from 667M submarines with 12 launchers per boat. The air-launched Meteorit-A would be launched from Tu-95 bombers. The land-based version was designated Meteorit-N. The missile was also sometimes referred to by the code-name Grom. The first test launch, on 20 May 1980, was unsuccessful, as were the next three attempts. The first successful flight did not come until 16 December 1981. The first launch from a 667M submarine took place on 26 December 1983 from the Barents Sea. However all variants were cancelled in 1988 as a result of the INF Treaty. |
Mikoyan 301 Russian intermediate range cruise missile. The 301 was designed as a military bomber, with a Mach 4 / 4,250 km/hr cruise capability at 25,000 to 27,000 m altitude. It was equipped with two turboramjets, had a gross takeoff mass of 80 metric tons, of which half was fuel. It may be related to the first stage of the MIGAKS two-stage vehicle. |
P-750 Russian intermediate range cruise missile. IOC in 1988 est 1992+. SS-C-5 GLCM banned in INF. |
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ASMP French cruise missile. Tactical nuclear. ASMP-A is improved version expected to enter service in 2008. |
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