Neha Patil (Editor)

DRS RQ 15 Neptune

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Top speed
  
160 km/h

Length
  
1.83 m

Wingspan
  
2.13 m

DRS RQ-15 Neptune wwwdesignationsystemsnetdusrmapp2rq15ajpg

The DRS RQ-15 Neptune is a reconnaissance UAV developed in the United States in the early years of the 21st century. The design is optimized for operations over water, and is capable of water landings on its flying boat–like hull. The 11.2 kW (15 hp) pusher engine is mounted high to keep it dry during takeoffs and landings. The Neptune can also be launched off a pneumatic catapult and land on a skid. In 2007 one was unsuccessfully launched off the USS Nashville (LPD-13), crashing into the water less than two seconds after lift off.

Specifications

General characteristics

  • Crew: None
  • Capacity: 20 lb (9 kg) payload
  • Length: 6 ft 0 in (1.83 m)
  • Wingspan: 7 ft 0 in (2.13 m)
  • Gross weight: 80 lb (36 kg)
  • Powerplant: 1 × piston engine, 15 hp (11 kW)
  • Performance

  • Maximum speed: 100 mph (160 km/h)
  • Endurance: 4 hours
  • Service ceiling: 8,000 ft (2,400 m)
  • References

    DRS RQ-15 Neptune Wikipedia