XP-56 Black Bullet – The strange looking WWII fighter interceptor that you may not know of
Ultimately, it was unsuccessful and did not enter series production. sourceThe XP-56 was essentially a hybrid flying wing to which was added a stubby fuselage to house the pilot and engine.
The
Northrop XP-56 Black Bullet was a unique prototype fighter interceptor
built by the Northrop Corporation. It was one of the most radical of the
experimental aircraft built during World War II. Ultimately, it was
unsuccessful and did not enter series production.
The initial idea
for the XP-56 was quite radical for 1939. It was to have no horizontal
tail, only a small vertical tail, used an experimental engine, and be
produced using a novel metal. The aircraft was to be a wing with a small
central fuselage added to house the engine and pilot. The hope was that
this configuration would have less aerodynamic drag than a conventional
airplane.
The
idea for this single-seat aircraft originated in 1939 as the Northrop
N2B model. It was designed around the Pratt & Whitney liquid-cooled
X-1800 engine in a pusher configuration driving contra-rotating
propellers. The U.S. Army ordered Northrop to begin design work on 22
June 1940, and after reviewing the design ordered a prototypeaircraft on
26 September 1940. Shortly after design work had begun, Pratt &
Whitney, however, stopped development of the X-1800. The Pratt &
Whitney R-2800 engine was substituted, although it was considered not
entirely suitable. Although the new engine was more powerful (2,000 hp
vs 1,800 hp) it had a larger diameter and required a larger fuselage to
house it. This change delayed the program by five months. The
initial idea for the XP-56 was quite radical for 1939. It was to have
no horizontal tail, only a small vertical tail, used an experimental
engine, and be produced using a novel metal. The aircraft was to be a
wing with a small central fuselage added to house the engine and pilot. sourceIt
was expected that the new engine would require a 2,000 lb weight
increase and cost 14 mph in top speed. Since this tailless design was
novel and considered high risk, it was decided to construct a small,
lightweight plane of similar configuration for testing called the Model
N-1M. In parallel with the design of the XP-56, successful flight trials
of the configuration were conducted utilizing this airframe, confirming
the basic layout. Two small Lycoming engines powered this aircraft.
These trials confirmed the stability of the radical design and, upon
review, the Army decided to construct a second prototype, which was
ordered on 13 February 1942. Taxi
tests of the XP-56 began on 6 April 1943 and showed a serious yaw
problem. At first, it was thought to be caused by uneven wheel brakes,
and considerable effort was placed into fixing this problem. sourceNorthrop
constructed the XP-56 using magnesium alloy for the airframe and skin,
because aluminium was forecast to be in short supply due to wartime
demands. At the time there was little experience with magnesium aircraft
construction. Because magnesium cannot be easily welded using
conventional techniques, Northrop hired Vladimir Pavlecka to develop the
heliarc welding technique for magnesium alloy. (Later it was discovered
that in the 1920s General Electric had already developed similar
techniques.
41-786 – crashed during high-speed ground run in 1943. sourceFirst
engine runs in the aircraft were conducted in late March 1943, but
excessive propeller shaft flex caused the engine to fail. Pratt &
Whitney did not send another engine until August, causing a five-month
delay.
Taxi
tests of the XP-56 began on 6 April 1943 and showed a serious yaw
problem. At first, it was thought to be caused by uneven wheel brakes,
and considerable effort was placed into fixing this problem. Manual
hydraulic brakes were installed and the aircraft flew on 30 September
1943 at Muroc Air Base in southern California. Eventually, the yaw
problem was traced to a lack of aerodynamic stability, and to fix this
the upper vertical stabilizer was enlarged from a mere stub, to one
virtually matching the ventral unit in shape and area.
After a
number of flights, the first XP-56 was destroyed 8 October 1943 when the
tire on the left gear blew out during a high-speed (~130 mph) taxi
across Muroc Dry Lake. The pilot, John Myers, survived with minor
injuries which he credited to his innovative wearing of a polo player’s
helmet. Myers was the test pilot for many of Northrop’s radical designs
during the war. Wreckage of the first XP-56. Note the missing left main tire. sourceA
number of changes were made to the second prototype, including
re-ballasting to move the center-of-gravity forward, increasing the size
of the upper vertical tail, and reworking the rudder control linkages.
This second prototype was not completed until January 1944. The aircraft
flew on 23 March 1944. The pilot had difficulty lifting the nose wheel
below 160 mph . Myers
actually flew XP-56 Ship No. 1 twice on the type’s inaugural day of
flight testing. The first flight was really just a hop in the air. Using
caution as a guide, Myers flew only 5 feet off the deck in a 30 second
flight that covered a distance on the order of 1 mile. The aircraft
registered a top speed 130 mph. While the XP-56 exhibited a nose-down
pitch tendency as well as lateral-directional sensitivities, Myers was
able to complete the flight. sourceHe
also reported extreme yaw sensitivity. This flight lasted less than
eight minutes, but subsequent flights were longer, and the nose
heaviness disappeared when the landing gear was retracted. Only
relatively low speeds were attained, however. While urging NACA to
investigate the inability to attain designed speeds, further flight
tests were made. On the 10th flight, the pilot noted extreme tail
heaviness, lack of power, and excessive fuel consumption. Flight testing
was then ceased as too hazardous, and the project was abandoned after a
year of inactivity. By 1946, the U.S. Army Air Forces was developing
jet-powered fighters, and had no need for a new piston-powered fighter
aircraft.
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