| 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.