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Lockheed XP-49

High-Altitude Fighter Prototype [ 1942 ]

Intended as a successor to the classic Lockheed P-38 Lightning twin-boom fighter of World War 2, the XP-49 proposal failed in most respects forcing the Army to look elsewhere.

Authored By: Staff Writer | Last Edited: 05/11/2016 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

The XP-49 was a development of the Lockheed Corporation during World War 2 (1939-1945) as a possible successor to the classic P-38 "Lightning" twin boom fighter of 1941. The XP-49 was to be a high-altitude performer with the established capabilities of the original. The project came about due to growing concern on the part of the U.S. Army in the rising costs of the most recent P-38 production model. After review of several proposed entries from various manufacturers, the Army settled on the new Lockheed design - the Model 522.

The XP-49 was visually similar in most respects to the P-38. The twin-boom design was found to be effective even for a fighter as in the P.38 and the XP-49 would follow suit. Beyond sharing this key physical characteristic, the XP-49 was of an new design. The aircraft was to feature a pair of Pratt & Whitney's new "X-1800" engine capable of an impressive 2,300 horsepower, offering the XP-49 airframe a maximum speed reaching nearing 500 miles per hour.

The single prototype was completed and first flown in November of 1942, sans all of its proposed armament to expedite development. The proposed weapons suite centered on 2 x 20mm cannons supported by 4 x 0.50 caliber Browning heavy machine guns - an improvement over the P.38's single 20mm cannon and 4 x .50 caliber gun array. As in the P-38, the XP-49 carried its armament concentrated at the nose section, ahead of the pilot's position.

While the XP-49 was being drawn up as a single-seat fighter, a second cockpit was added for an observer behind the pilot for flight testing.

New engines - the Continental XI-1430 - were then selected to succeed the intended (and now cancelled) Pratt & Whitney engines. This led to a reduction in estimated speed by as much as 75 miles per hour. The shift added to the project's woes which was beginning to lose steam as the war continued to turn to the favor of the Allies and the current stock of Army fighters were more than up to the task.

As such, the XP-49 led a very brief test life before running into further engine issues. As with the Pratt & Whitney engines, the developmental Continental engines were also cancelled. A crash landing during a flight test also took place when a landing gear failed to lower - such were the signs against the XP-49. With the cancellation of both intended engines, U.S. Army authorities eventually looked elsewhere, effectively leaving the XP-49 project dead on arrival.

In its final "moment of glory", the XP-49 airframe was subjected to brutish force-testing by being dropped at heights against a concrete floor. The tests were conducted to see the extent of damage caused by G-forces upon a modern aircraft fuselage. The XP-49 remains were later on display before being cannibalized and, ultimately, scrapped.©MilitaryFactory.com
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Service Year

United States national flag graphic
United States



National flag of the United States United States (cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Ability to intercept inbound aerial threats by way of high-performance, typically speed and rate-of-climb.
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

40.0 ft
(12.20 m)
52.0 ft
(15.85 m)
9.9 ft
(3.02 m)
Empty Wgt
15,399 lb
(6,985 kg)
18,827 lb
(8,540 kg)
Wgt Diff
+3,428 lb
(+1,555 kg)
(Showcased structural values pertain to the base Lockheed XP-49 production variant)
Installed: EARLY: 2 x Pratt & Whitney X-1800 inline piston engines developing 2,300 horsepower; LATE: 2 x Continental XI-1430-1 inline piston engines developing 1,600 horsepower each.
Max Speed
404 mph
(650 kph | 351 kts)
30,003 ft
(9,145 m | 6 mi)
680 mi
(1,095 km | 591 nm)
3,500 ft/min
(1,067 m/min)

♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030

(Showcased performance specifications pertain to the base Lockheed XP-49 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD (proposed):
2 x 20mm cannons in the nose
4 x 12.7mm machine guns in the nose

Supported Types

Graphical image of an aircraft medium machine gun
Graphical image of an aircraft heavy machine gun
Graphical image of an aircraft automatic cannon

(Not all ordnance types may be represented in the showcase above)

XP-49 - Series Designation; single airframe completed and later scrapped.
Model 522 - Model designation

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Images Gallery

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Image of the Lockheed XP-49
Image from the Public Domain.

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