AAM-N-4 Oriole
Air-to-air missile
Maximum speed Guidance
system
system
The AAM-N-4 Oriole was an early American air-to-air missile, developed by the Glenn L. Martin Company for the United States Navy. Designed for launch from carrier-based aircraft, the missile programme was cancelled before flight testing began, and the missiles produced were utilized as test vehicles.
Design and development
Development of the AAM-N-4 Oriole began in 1947, when a development contract was awarded by the United States Navy's Bureau of Ordnance to the Glenn L. Martin Company to develop a heavy air-to-air missile,[1] utilizing active radar homing for fire and forget operation,[2] for launch from aircraft operating from aircraft carriers.[3] Oriole was intended to utilize a rocket[4] or rocket-ramjet propulsion system; the intended range of the weapon was 20 miles (32 km),[5] however as tested it was limited to a range of approximately 10 miles (16 km).[3] Ready for launch, the missile weighed 1,500 pounds (680 kg),[6] and used cruciform fins at the missile's midbody and at the tail for flight control.[7] Flight speed was originally intended to be above Mach 3.[8]
In 1948, the Oriole contract was redefined to be a guidance development program instead of a project to develop an operational missile; the program to construct test vehicles resumed in 1950 for research and development purposes,[9] the missiles being redesignated RTV-N-16.[3] Flight testing began shortly thereafter at the Naval Air Missile Test Center at Point Mugu, California; testing continued through 1953, with 56 flight tests being conducted throughout the program;[9] as built the missile proved to be capable of Mach 2.5.[7] The Oriole program was terminated at the end of 1953.[10]
References
Citations
- ^ Gunston 1979, p.221.
- ^ Friedman 1982, p.150.
- ^ a b c Parsch 2005
- ^ Haley 1959, p.130.
- ^ Peck 1950, p.264.
- ^ Bowman 1957, p.169.
- ^ a b Hemsch 1992, p.17.
- ^ "Aircraft Armament, Part 2: Missiles and Projectiles". Flight International, 28 January 1955, p.118.
- ^ a b USPMTC 1989, p.52-53
- ^ Fahey 1958, p. 32.
Bibliography
- Bowman, Norman John (1957). The Handbook of Rockets and Guided Missiles. Chicago: Perastadion Press. ASIN B0007EC5N4.
- Fahey, James Charles (1958). The Ships and Aircraft of the U.S. Fleet (7th ed.). Washington, DC: Ships and Aircraft Publishers. ISBN 9780870216466.
- Friedman, Norman (1982). U.S. Naval Weapons: every gun, missile, mine, and torpedo used by the U.S. Navy from 1883 to the present day. Annapolis, MD: Naval Institute Press. ISBN 978-0-87021-735-7.
- Gunston, Bill (1979). The Illustrated Encyclopedia of the World's Rockets and Missiles. London: Salamander. ISBN 978-0861010295.
- Haley, Andrew Gallagher (1959). Rocketry and Space Exploration. Princeton, NJ: D. Van Nostrand Company. ASIN B000GB0580.
- Hemsch, Michael (1992). Tactical Missile Aerodynamics: General Topics. Progress in Astronautics and Aeronautics. Reston, VA: American Institute of Aeronautics and Astronautics. ISBN 978-1563470158.
- Nichols, Gina (2011). The Navy at Point Mugu. Charleston, SC: Arcadia Publishing. ISBN 978-0-7385-7532-2.
- Parsch, Andreas (2005). "Martin AAM-N-4 Oriole". Directory of U.S. Military Rockets and Missiles Appendix 1: Early Missiles and Drones. designation-systems.net. Retrieved 21 January 2013.
- Peck, James L.H. (January 1950). "How Fast Can We Fight?". Popular Mechanics. 94 (6). Chicago: Popular Mechanics Company. Retrieved 21 January 2013.
- United States Navy Pacific Missile Test Center (1989). Days of Challenge, Years of Change: a Technical History of the Pacific Missile Test Center. Washington, CC: Government Printing Office. ASIN B000S75AFK.
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