| Revision as of 19:39, 28 January 2006 edit198.178.132.253 (talk) →External links← Previous edit | Revision as of 02:55, 30 January 2006 edit undo68.6.90.73 (talk)No edit summaryNext edit → | ||
| Line 23: | Line 23: | ||
| == See also == | == See also == | ||
| *] | |||
| *] | *] | ||
| *] | *] | ||
Revision as of 02:55, 30 January 2006
The RQ-5 Hunter unmanned aerial vehicle (UAV) was originally intended to serve as the United States Army's Short Range UAV system for division and corps commanders. It took off and landed (using arresting gear) on runways. It used a gimbaled EO/IR sensor to relay its video in real time via a second airborne Hunter over a C-band line-of-sight data link. The RQ-5 is based on the Hunter UAV that was developed by Israel Aircraft Industries.
Hunter deployed in 1999 to Kosovo to support NATO operations. Although production was cancelled in 1996, seven low rate initial production (LRIP) systems of eight aircraft each were acquired, four of which remained in service: one for training and three for doctrine development and exercise and contingency support. Hunter was to be replaced by the RQ-7 Shadow.
The "R" is the Department of Defense designation for reconnaissance; "Q" means unmanned aircraft system. The "5" refers to it being the fifth of a series of purpose-built unmanned reconnaissance aircraft systems.
General characteristics
- Primary Function: division- and corp-level reconnaissance
- Contractor: TRW, Israel Aircraft Industries
- Power Plant: 2 Moto Guzzi twin cylinder, 4 stroke engines
- Length: 7 m (23 ft)
- Height:
- Weight: 727 kg (1600 lb)
- Wingspan: 8.9 m (29.2 ft)
- Speed:
- Range: 11.6 hours at 260 km (144 nautical miles)
- Ceiling: 4600 m (15,000 ft)
- Fuel Capacity:
- Payload: 90 kg (200 lb)
- System Cost:
- Inventory:
See also
External links
| Aviation lists | |
|---|---|
| General | |
| Military | |
| Accidents / incidents | |
| Records | |