Northrop XP-56 Black Bullet

Pursuit Fighter Prototype [ 1943 ]

The Northrop XP-56 Black Bullet was another U.S. Army Air Corps proposal to research the benefits of pusher-propeller design - this time within a flying wing arrangement.

Authored By: Staff Writer | Last Edited: 04/26/2016 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

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The XP-56 "Black Bullet" was a "pursuit fighter" designed by the Northrop Corporation to a United States Army Air Corps (USAAC) proposal known as the "R-40C". The compact fighter became yet another advanced World War 2-era fighter entry for the Americans and focused on a flying wing concept mated to a "pusher-type" propulsion configuration. The pusher arrangement was in contrast to the widely accepted "puller-type" arrangements found on many conventional piston-powered aircraft of the period. The proposal (and subsequent flyable aircraft) sought to define inherent benefits (if any) in the pusher-type configuration. Unfortunately for the Black Bullet, very little value was revealed and the aircraft was never adopted for serial production.

The XP-56 was fitted with large-area wings, cranked downwards at their outboard sections, and attached to a rather stubby fuselage. Aspiration for the the engine was through intakes integrated directly into the mainplane leading edges to feed the engine buried in the aft section of the fuselage. A sole vertical fin was seated over the rear of the aircraft and there was also a ventral protrusion. The cockpit was mounted at front which gave the pilot a commanding view over the nose with his view to the rear obstructed by the raised fuselage spine. A tricycle undercarriage (wholly retractable) rounded out the list of modern design features.

Power was derived from a single Pratt & Whitney R-2800-29 engine developing 2,000 horsepower and driving a three-bladed propeller unit.

Proposed armament was 2 x 20mm cannons coupled with 4 x 0.50 caliber heavy machine guns, presumably all mounted in the nose or wings or spread across both.

The Black Bullet was initially flown in prototype form on September 23, 1943 though this aircraft was eventually lost during a high-speed ground run exercise that same year. A second prototype followed on March 23, 1944 and incorporated some improvements to the original design including a yaw control system and a larger-area vertical stabilizer. This example underwent a battery of tests only to finally reveal that the aircraft offered no real performance benefits in its unique design and layout when compared to conventionally arranged prop-driven fighters. Additionally, advanced being made in bringing jet-powered fighters along helped to doom such programs.

As such, the XP-56 program was limited to just the two prototype examples, the second ending her days as a museum piece. All development ended on the XP-56 in January of 1946.

As completed, the XP-56 held dimensions that included a length of 27.5 feet, a wingspan of 42.5 feet, and a height of 11 feet. Its empty weight was 8,700lb against a Maximum Take-Off Weight (MTOW) of 12,145lb. Performance specifications with the PW engine in place included a maximum speed of 465 miles per hour, a range out to 660 miles, a service ceiling up to 33,000 feet, and a rate-of-climb of 3,125 feet-per-minute.©MilitaryFactory.com

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Specifications

Service Year

1943

Origin

United States

Crew

1

Production

2
UNITS

Northrop Corporation - USA

(View other Aviaton-Related Manufacturers)

United States (cancelled)

(OPERATORS list includes past, present, and future operators when applicable)

✓ Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.

✓ X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

Length

27.6 ft
(8.40 m)

Width/Span

42.5 ft
(12.94 m)

Height

11.0 ft
(3.35 m)

Empty Wgt

8,699 lb
(3,946 kg)

MTOW

11,349 lb
(5,148 kg)

Wgt Diff

+2,650 lb
(+1,202 kg)

(Showcased structural values pertain to the base Northrop XP-56 Black Bullet production variant)

Installed: 1 x Pratt & Whitney R-2800-29 engine developing 2,000 horsepower driving a three-bladed propeller unit in "pusher" configuration.

Max Speed

465 mph
(748 kph | 404 kts)

Ceiling

32,999 ft
(10,058 m | 6 mi)

Range

662 mi
(1,065 km | 1,972 nm)

Rate-of-Climb

3,125 ft/min
(952 m/min)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Northrop XP-56 Black Bullet 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)

PROPOSED (never fitted):
2 x 20mm cannons
4 x 0.50 caliber heavy machine guns

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)

Hardpoint Mountings: 0

XP-56 "Black Bullet" - Prototype Model Series Designation; 2 examples produced with first prototype lost to accident; second prototype featured larger-area vertical stabilizer, improved wingtip design and yaw control flight system.

P-56 - Assumed production model designation

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Images Gallery

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Image of the Northrop XP-56 Black Bullet

Image from the Public Domain.

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Image from the Public Domain.

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