Lockheed P-7

From Wikipedia, the free encyclopedia

The Lockheed P-7 was a four turboprop-engined patrol aircraft ordered by the U.S. Navy as a replacement for the P-3 Orion. The external configuration of the aircraft was to be very similar to that of the P-3. Development had not progressed very much before the development was canceled in early 1990s as a cost cutting measure following the breakup of the Soviet Union.

[edit] Specifications (P-7A, as designed)

[edit] General characteristics

• Crew:
• Length: 112 ft 8 in (34.35 m)
• Wingspan: 106 ft 7 in (32.49 m)
• Height: 32 ft 11 in (10.04 m)
• Wing area: 1,438 ft² (133.7 m²)
• Empty: 105,000 lb (47,627 kg)
• Loaded: 165,000 lb (74,843 kg)
• Maximum takeoff: 171,350 lb (77,723 kg)
• Powerplant: 4× General Electric T407 turboprops, 6,000 shp (4,475 kW) each

[edit] Performance

• Maximum speed: mph ( km/h)
• Range: miles ( km)
• Service ceiling: ft ( m)
• Rate of climb: ft/min ( m/min)
• Wing loading: 115 lb/ft² (560 kg/m²)
• Power/mass: 0.14 hp/lb (0.24 kW/kg)

[edit] See also

Related development

• P-3 Orion
  

Comparable aircraft

• P-8 Poseidon
• Kawasaki P-1
  

Related lists

• List of active United States military aircraft
  

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