Lobber
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| Lobber | |
|---|---|
| Type | Cargo missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Army |
| Production history | |
| Designer | Convair |
| Designed | 1958 |
| Unit cost | $1,000 (projected) |
| No. built | 27 |
| Specifications | |
| Mass | 135 lb (61 kg) |
| Length | 9 ft (2.7 m) |
| Diameter | 10 in (250 mm) |
| Warhead | Cargo |
| Warhead weight | 50 lb (23 kg) |
| Engine | Rocket |
| Propellant | Solid fuel |
Operational range | 8 mi (13 km) |
| Flight ceiling | 10,000 ft (3,000 m) |
| Maximum speed | 1,500 mph (2,400 km/h) |
Guidance system | Ballistic |
| Accuracy | ~100 yd (91 m) |
The Lobber was a surface-to-surface cargo missile developed during the mid 1950s by Convair for use by the United States Army. Intended to deliver supplies to troops in combat, it was successfully tested, but failed to go into production.