AAM-N-4 Oriole

Last updated
AAM-N-4 Oriole
AAM-N-4 Oriole.png
Type Air-to-air missile
Place of originUnited States
Service history
In service1950–1955
Used by United States Navy
Production history
Designed1947
Manufacturer Martin
Specifications
Mass1,500 pounds (680 kg)
Length11 feet 7 inches (3.53 m)
Diameter11 inches (280 mm)

Warhead High explosive
Warhead weight25 pounds (11 kg)

Wingspan3 ft 2.8 in (0.986 m)
Operational
range
10 miles (16 km)
Flight altitudeMax at launch, 10 miles (16 km)
Maximum speed Mach 2.5
Guidance
system
Active radar homing

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.

Contents

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]

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References

Citations

  1. Gunston 1979, p.221.
  2. Friedman 1982, p.150.
  3. 1 2 3 Parsch 2005
  4. Haley 1959, p.130.
  5. Peck 1950, p.264.
  6. Bowman 1957, p.169.
  7. 1 2 Hemsch 1992, p.17.
  8. "Aircraft Armament, Part 2: Missiles and Projectiles". Flight International, 28 January 1955, p.118.
  9. 1 2 USPMTC 1989, p.52-53
  10. Fahey 1958, p. 32.

Bibliography

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  • 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.
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  • 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. Chicago: Popular Mechanics Company. 94 (6). 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.