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TDU-12/B Skydart

From Wikipedia, the free encyclopedia
Target rocket
TDU-12/B Skydart
TypeTarget rocket
Place of originUnited States
Service history
Used byUnited States Air Force
Production history
Designedc.1958
ManufacturerCurtiss-Wright
Specifications
Mass103 lb (47 kg)
Length6 ft 8 in (2.03 m)
Diameter6.4 in (16 cm)
Wingspan20.8 in (0.53 m)

EngineGCRC/Hercules dual-thrust
620 lbf (2.8 kN) for 2 sec
75 lbf (0.33 kN) for 45 sec
PropellantSolid
Maximum speedMach 2
Guidance
system
Autopilot
Launch
platform
F-100, F-104
ReferencesParsch[1]

TheTDU-12/B Skydart was an unguided target rocket built byCurtiss-Wright for use by theUnited States Air Force. It was used operationally from the late 1950s to the mid-1960s.

Design and development

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Skydart, designated TDU-12/B by the U.S. Air Force,[2] was developed by the Santa Barbara Division ofCurtiss-Wright.[3] It was designed for use as a target for practice withinfrared homingair-to-air missiles such as theAIM-9 Sidewinder andAIM-4 Falcon. It had a small cylindrical body fitted with fourcruciform fins aft for control and fixed forwardscanards to set the rocket's trajectory. Propulsion was by a dual-thrust boost-sustainsolid-propellant rocket supplied by theGrand Central Rocket Company and theHercules Powder Company. Agyroscopic-drivenautopilot stabilized the rocket in flight.[4] Aninfrared flare was installed to provide signature enhancement for training purposes, and the rocket could be equipped with atelemetry system.[1] Skydart was designed to use a common launching rail and electronic connections to the launch aircraft as Sidewinder.[5] Launch would be undertaken at speeds betweenMach 0.8 and 2.0. Design endurance was nominally 90 seconds, but in service 110-second endurance was demonstrated.[3]

Operational history

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A $470,000 contract was awarded to Curtiss-Wright by the USAF for production of Skydart.[5] Launched fromF-100 Super Sabre andF-104 Starfighter fighters, Skydart was used throughout the early-to-mid 1960s, but was out of service before the end of the decade.[1] Proposals for improved versions of Skydart, including a ground-launched version and an enlargedtarget drone, do not appear to have been developed.[5]

References

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Citations

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  1. ^abcParsch 2004
  2. ^Jacobs and Whitney 1962, p. 170.
  3. ^abMissiles and Rockets Volume 5 (1957–1958),p. 28 (a).
  4. ^Ordway and Wakeford 1960, p. ND20.
  5. ^abcMissiles and Rockets Volume 5 (1957–1958),p. 28 (b).

Bibliography

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  • Jacobs, Horace; Eunice Engelke Whitney (1962).Missile and Space Projects Guide 1962. New York: Springer Science+Business Media.ISBN 978-1-4899-6967-5.{{cite book}}:ISBN / Date incompatibility (help)
  • Ordway, Frederick Ira; Ronald C. Wakeford (1960).International Missile and Spacecraft Guide. New York: McGraw-Hill.ASIN B000MAEGVC.
  • Parsch, Andreas (16 June 2004)."Curtiss-Wright TDU-12/B Skydart".Directory of U.S. Military Rockets and Missiles, Appendix 4: Undesignated Vehicles. Designation-Systems.Archived from the original on 2017-10-18. Retrieved2017-12-09.
1955–1962United States Air Force rocket and missile designations
Air-to-air missiles
1955–1961 sequence
1961–1963 sequence
Other types
Undesignated types
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