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Republic SD-4 Swallow

From Wikipedia, the free encyclopedia
Canceled reconnaissance drone project
SD-4 Swallow
General information
TypeReconnaissance drone
National originUnited States
ManufacturerRepublic Aviation
Primary userUnited States Army
Number built0

TheRepublic SD-4 Swallow was an early high-speedreconnaissance drone developed byRepublic Aviation for theUnited States Army. Intended for use by theU.S. Army Signal Corps to targettactical ballistic missiles, it was cancelled before the first prototype could be completed, and did not see operational service.

Design and development

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Contracts were awarded by the U.S. Army in 1960 for development of a high-speed, long-range reconnaissance drone to gather targeting information for the Army'stactical ballistic missile force; competing designs for the requirement were developed by Republic Aviation, which proposed a 'clean-sheet' aircraft given the designation SD-4 Swallow, andFairchild Aircraft, which developed a variant of theBull Goose decoy missile as theSD-5 Osprey.[1]

Given the full designationAN/USD-4 for its overall system,[2] the SD-4 was oftailless delta configuration,[1] with power provided by aPratt & Whitney J60 turbojet, the military version of the civilian JT12 engine;[3] two Arrow 2jet-assisted takeoff-type rocket boosters allowing forzero-length launch from a specially designed trailer.[4]

In a similar fashion to Republic's smallerSD-3 drone, the Swallow was equipped withan interchangeable nose section allowing foraerial photography,infrared photography, orradar systems to be installed depending on mission needs.[4] Capable of operating in any weather conditions,[5] recovery following the completion of the SD-4's mission was to be byparachute.[4]

Before any flight test vehicles were constructed,[1] the program was cancelled in January of 1961 due to cost constraints.[6]

Specifications

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Data from Parsch 2004[2]

General characteristics

  • Crew: None
  • Length: 30 ft 5 in (9.27 m)
  • Wingspan: 11 ft 6 in (3.51 m)
  • Gross weight: 3,500 lb (1,588 kg)
  • Powerplant: 1 ×Pratt & Whitney J60-3turbojet, 2,900 lbf (13 kN) thrust

PerformanceNewcome states the SD-4 and SD-5 were subsonic.[1]

  • Maximum speed: Mach 1.5
  • Range: 300 mi (480 km, 260 nmi)
  • Service ceiling: 60,000 ft (18,000 m)

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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Citations

  1. ^abcdNewcome 2004, p.75.
  2. ^abParsch 2004
  3. ^Aviation Week & Space Technology volume 73 (1960),p. 361.
  4. ^abcOrdway and Wakeford 1960, p.USA51.
  5. ^Jane's 1959–1960, p.377.
  6. ^Stanfield 1961, p.25.

Bibliography

  • Newcome, Lawrence R. (2004).Unmanned Aviation: A Brief History of Unmanned Aerial Vehicles. Reston, Virginia: American Institute of Aeronautics and Astronautics.ISBN 978-1-56347-644-0.
  • Ordway, Frederick Ira; Ronald C. Wakeford (1960).International Missile and Spacecraft Guide. New York: McGraw-Hill.ASIN B000MAEGVC.
  • Parsch, Andreas (5 May 2004)."Republic SD-4 Swallow".Directory of U.S. Military Rockets and Missiles, Appendix 4: Undesignated Vehicles. Designation-Systems. Retrieved2017-12-15.
  • Stanfield, Robert I. (March 1961)."America's First Corporate Jet".Flying. Vol. 68, no. 3. New York: Ziff-Davis Publishing. Retrieved2017-12-15.
  • Taylor, John W.R. (1960).Jane's All the World's Aircraft 1959–1960. London: Sampson Low, Marston & Co.ASIN B002G60XF8.
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