Overview
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.
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.
YEAR: 1943
MANUFACTURER(S): Northrop Corporation - USA
PRODUCTION: 2
OPERATORS: United States (cancelled)
Technical Specifications
Unless otherwise noted the presented statistics below pertain to the Northrop XP-56 Black Bullet model. Common measurements, and their respective conversions, are shown when possible.
Unless otherwise noted the presented statistics below pertain to the Northrop XP-56 Black Bullet model. Common measurements, and their respective conversions, are shown when possible.
CREW: 1
POWER: 1 x Pratt & Whitney R-2800-29 engine developing 2,000 horsepower driving a three-bladed propeller unit in "pusher" configuration.
ADVERTISEMENTS
LENGTH
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HEIGHT
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EMPTY WGT
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M.T.O.W.
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SPEED (MAX)
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CEILING
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RANGE
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CLIMB RATE
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meters-per-minute
Armament
PROPOSED (never fitted):
2 x 20mm cannons
4 x 0.50 caliber heavy machine guns
PROPOSED (never fitted):
2 x 20mm cannons
4 x 0.50 caliber heavy machine guns
Variants / Models
• 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
• 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
History
Detailing the development and operational history of the Northrop XP-56 Black Bullet Pursuit Fighter Prototype. Entry last updated on 4/26/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
Detailing the development and operational history of the Northrop XP-56 Black Bullet Pursuit Fighter Prototype. Entry last updated on 4/26/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
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.
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.
Media
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed
Hi: 500mph
Lo: 250mph
This entry's maximum listed speed (465mph).
Graph average of 375 miles-per-hour.
City-to-City Ranges
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Graph showcases the Northrop XP-56 Black Bullet's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production (2)
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
2
2
Altitude Visualization
