Lockheed P-7

P-7
P-7 LRAACA drawing
Role Maritime patrol aircraft
National origin United States
Manufacturer Lockheed Corporation
Status Cancelled
Number built none
Program cost US$915 million[1]
Unit cost
est. US$56.7 million
Developed from P-3 Orion

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 cancelled in the early 1990s as a cost-cutting measure following the end of the Cold War.

Development

In the mid-1980s, the U.S. Navy made plans to replace the large number of Lockheed P-3 aircraft which would reach the end of their useful service lives during the 1990s. To limit costs the U.S. Navy envisioned a modified P-3 with increased payload and updated avionics. This aircraft became known as the "P-3G" of which 125 should be procured over a period of five years up to 2001. However, the U.S. Navy was unwilling to select Lockheed's P-3G without any competition and issued the final "request for proposal (RFP)" in January 1987. For the airplane named "LRAACA" (Long-Range Air ASW-Capable Aircraft), Lockheed's competitors were:

In October 1988, the U.S. Navy announced that Lockheed won the competition, as the company's proposal was significantly lower than that of the competitors. The U.S. Defense Acquisition Board (DAB) recommended a full-scale development of the LRAACA on 4 January 1989. The costs were planned to be about $600 million, with a maximum cost limit of $750 million. However, already in November 1989, Lockheed announced a cost overrun of $300 million, due to the tight schedule and design problems. On 20 July 1990, the U.S. Navy stopped the P-7A program contract for default, "citing Lockheed's inability to make adequate progress toward completion of all contract phases".[1] The program was finally cancelled by the DAB in late 1990.

Design

The P-7 was designed as an enlarged version of the original P-3C. The fuselage, of similar cross-section to that of the P-3, was lengthened by 2.40 m (8 ft), and the wingspan by 2.10 m (7 ft). The wing center section was increased in length, which moved the engines farther away from the fuselage to reduce noise levels in the cabin. The tailplane was increased by about 25% in area, but shortened in height compared to that of the P-3. The P-7A was to be powered by four General Electric T407-GE-400 turboprops with 5-blade propellers.

Initial plans included the Update IV electronics equipment of the P-3C. The cockpit was to be fitted with eight CRT displays and a stowable HUD for weapons delivery.[3] Other equipment included search radar, MAD, decoy flare launchers, electro-optical detector, radar warning receivers, IR suppression on the engine exhausts and laser deflection screens on the windows. The primary submarine detection sensor was to be the sonobuoy, of which 112 were carried internally; 38 more could be stowed for in flight reloading. Another 150 could be carried in 10 underwing pods.

The design had an internal bomb bay for a maximum of 3,400 kg of weapons and 12 underwing pylons.[4]

Specifications (P-7A, as designed)

General characteristics

Performance

See also

Related development
Aircraft of comparable role, configuration and era

References

  1. 1 2 https://fas.org/programs/ssp/man/uswpns/air/asw/p7.html
  2. ↑ Flight International, 2 July 1988 Lockheed woos Germany over LRAACA
  3. ↑ U.S. Navy Naval Aviation News January/February 1989, pp.20-21
  4. ↑ Bowers, Peter M. United States Navy Aircraft since 1911. Annapolis, MD: Naval Institute Press, 1990, pp. 313-314. ISBN 0-87021-792-5.
This article is issued from Wikipedia - version of the Monday, August 31, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.