TDU-12/B Skydart: Difference between revisions
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==Design and development== |
==Design and development== |
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Skydart, designated TDU-12/B by the U.S. Air Force,<ref>Jacobs and Whitney 1962, p. 170.</ref> was developed by the Santa Barbara Division of [[Curtiss-Wright]].<ref name="MR1">''Missiles and Rockets'' Volume 5 (1957–1958), [https://books.google.com/books?id=nOMiAQAAMAAJ&dq=%22TDU-12%22+Skydart&focus=searchwithinvolume&q=Skydart p. 28] (a).</ref> It was designed for use as a target for practice with [[infrared homing]] [[air-to-air missile]]s such as the [[AIM-9 Sidewinder]] and [[AIM-4 Falcon]] |
Skydart, designated TDU-12/B by the U.S. Air Force,<ref>Jacobs and Whitney 1962, p. 170.</ref> was developed by the Santa Barbara Division of [[Curtiss-Wright]].<ref name="MR1">''Missiles and Rockets'' Volume 5 (1957–1958), [https://books.google.com/books?id=nOMiAQAAMAAJ&dq=%22TDU-12%22+Skydart&focus=searchwithinvolume&q=Skydart p. 28] (a).</ref> It was designed for use as a target for practice with [[infrared homing]] [[air-to-air missile]]s such as the [[AIM-9 Sidewinder]] and [[AIM-4 Falcon]]. It had a small cylindrical body fitted with four [[cruciform]] fins aft for control and fixed forwards [[canard (aeronautics)|canards]] to set the rocket's trajectory. Propulsion was by a dual-thrust boost-sustain [[solid-propellant rocket]] supplied by the [[Grand Central Rocket Company]] and the [[Hercules Powder Company]]; a [[gyroscopic]]-driven [[autopilot]] stabilized the rocket in flight.<ref name="Ord">Ordway and Wakeford 1960, p. ND20.</ref> An [[Flare (countermeasure)|infrared flare]] was installed to provide signature enhancement for training purposes, and the rocket could be equipped with a [[telemetry]] system.<ref name="DS">Parsch 2004</ref> Skydart was designed to use a common launching rail and electronic connections to the launch aircraft as Sidewinder.<ref name="MR2">''Missiles and Rockets'' Volume 5 (1957–1958), [https://books.google.com/books?id=nOMiAQAAMAAJ&dq=%22TDU-12%22+Skydart&focus=searchwithinvolume&q=%22TDU-12%22 p. 28] (b).</ref> Launch would be undertaken at speeds between [[Mach number|Mach]] 0.8 and 2.0; design endurance was nominally 90 seconds, but in service 110-second endurance was demonstrated.<ref name="MR1"/> |
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==Operational history== |
==Operational history== |
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Revision as of 04:31, 4 February 2018
| TDU-12/B Skydart | |
|---|---|
 | |
| Type | Target rocket |
| Place of origin | United States |
| Service history | |
| Used by | United States Air Force |
| Production history | |
| Designed | c.1958 |
| Manufacturer | Curtiss-Wright |
| Specifications | |
| Mass | 103 lb (47 kg) |
| Length | 6 ft 8 in (2.03 m) |
| Diameter | 6.4 in (16 cm) |
| Wingspan | 20.8 in (0.53 m) |
| Engine | GCRC/Hercules dual-thrust 620 lbf (2.8 kN) for 2 sec 75 lbf (0.33 kN) for 45 sec |
| Propellant | Solid |
| Maximum speed | Mach 2 |
Guidance system | Autopilot |
Launch platform | F-100, F-104 |
| References | Parsch[1] |
The TDU-12/B Skydart was an unguided target rocket built by Curtiss-Wright for use by the United States Air Force. It was used operationally from the late 1950s to the mid 1960s.
Design and development
Skydart, designated TDU-12/B by the U.S. Air Force,[2] was developed by the Santa Barbara Division of Curtiss-Wright.[3] It was designed for use as a target for practice with infrared homing air-to-air missiles such as the AIM-9 Sidewinder and AIM-4 Falcon. It had a small cylindrical body fitted with four cruciform fins aft for control and fixed forwards canards to set the rocket's trajectory. Propulsion was by a dual-thrust boost-sustain solid-propellant rocket supplied by the Grand Central Rocket Company and the Hercules Powder Company; a gyroscopic-driven autopilot stabilized the rocket in flight.[4] An infrared flare was installed to provide signature enhancement for training purposes, and the rocket could be equipped with a telemetry 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 between Mach 0.8 and 2.0; design endurance was nominally 90 seconds, but in service 110-second endurance was demonstrated.[3]
Operational history
A $470,000 contract was awarded to Curtiss-Wright by the USAF for production of Skydart.[5] Launched from F-100 Super Sabre and F-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 enlarged target drone, do not appear to have been developed.[5]
References
Citations
Bibliography
- Jacobs, Horace; Eunice Engelke Whitney (1962). Missile and Space Projects Guide 1962. New York: Springer Science+Business Media. ISBN 978-1-4899-6967-5.
- 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. Retrieved 2017-12-09.