TDU-12/B Skydart
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,
Operational history
A $470,000 contract was awarded to Curtiss-Wright by the USAF for production of Skydart.
References
Citations
Bibliography
- Jacobs, Horace; Eunice Engelke Whitney (1962). Missile and Space Projects Guide 1962. New York: Springer Science+Business Media. )
- 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. Retrieved 2017-12-09.