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Vultee XP-81

Mixed-Power Fighter Prototype Aircraft

Vultee XP-81

Mixed-Power Fighter Prototype Aircraft

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



The Vultee XP-81 was a combination fighter powered by both turboprop and turbojet powerplant technology.
National Flag Graphic
ORIGIN: United States
YEAR: 1945
STATUS: Cancelled
MANUFACTURER(S): Vultee / Consolidated / Convair - USA
PRODUCTION: 2
OPERATORS: United States (cancelled)
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Vultee XP-81 model. Common measurements, and their respective conversions, are shown when possible.
CREW: 1
LENGTH: 44.91 feet (13.69 meters)
WIDTH: 50.49 feet (15.39 meters)
HEIGHT: 14.01 feet (4.27 meters)
WEIGHT (EMPTY): 12,798 pounds (5,805 kilograms)
WEIGHT (MTOW): 19,500 pounds (8,845 kilograms)
ENGINE: 1 x General Electric XT-31-GE-1 turboprop engine developing 2,300 horsepower and 1 x General Electric J33-GE-5 turbojet engine developing 3,750 lb of thrust.
SPEED (MAX): 506 miles-per-hour (815 kilometers-per-hour; 440 knots)
RANGE: 2,500 miles (4,023 kilometers; 2,172 nautical miles)
CEILING: 35,499 feet (10,820 meters; 6.72 miles)
RATE-OF-CLIMB: 4,500 feet-per-minute (1,372 meters-per-minute)




ARMAMENT



PROPOSED:
6 x 12.7mm machine guns (never installed)
VARIANTS



Series Model Variants
• XP-81 - Prototype versions consisting of S/N 44-91000 and 44-91001.


HISTORY



Detailing the development and operational history of the Vultee XP-81 Mixed-Power Fighter Prototype Aircraft.  Entry last updated on 7/13/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The Consolidated Vultee XP-81 was a proposed long-range, high-altitude fighter design that was to be the answer for bomber escorting in Europe but, more importantly, throughout the island hopping campaign of the Pacific. The XP-81 melded together the power of the ever-evolving turbojet engines and the development of America's first turboprop engine.

The single-seat, twin engine fighter was designed around the complicated General Electric powerplant creations that would never live up to expectations with the XP-81 design. To feed the two-engine idea, the aircraft itself was to be of a rather large design for a fighter when compared to its contemporaries in the P-51 Mustang, P-38 Lightning and the P-47 Thunderbolt.

The pilot sat forward of the wing assemblies, offering up tremendous visibility from the bubble canopy overlooking the front part of the aircraft. A four-blade propeller sat at front, powered by the turboprop assembly in the nose. The laminar flow wings sat directly in the center of the design with a low tricycle landing gear system underneath the massive spread. Twin intakes were mounted just aft of the cockpit on the top portion of the fuselage. These intakes were placed as such to feed the single turbojet engine jettisoning exhaust through the rear under the rudder and tail assemblies.

On paper, the design was sound. Estimated capabilities proposed that the system would be able to achieve over 500 miles per hour and reach over 35,000 feet. As impressive ranges were a part of the American aircraft pedigree throughout the war (British and German aircraft seldom were long-range threats to one another), the XP-81 was to have a distance of 2,500 miles - more than enough to keep up with the B-17 and B-29 bomber formations pounding The Reich and the Empire of Japan.

Alas, troubles with the powerplant forced the only flying prototype to be fitted with a P-51 engine alternative. When the turboprop did arrive and was installed, the system produced well under expectations - a full 1,000 horsepower under proposed capabilities in fact. With the war in Europe now held in check by the existing breed of fighter escorts and the island hopping campaigns of the Pacific progressing equally well - though slow-going and costly to US ground forces - the XP-81 project was cancelled along with the order of 13 YP-81 developmental models.

Though envisioned with an armament array of 6 x .50 caliber machine guns, the weapons were never fitted to the aircraft. Provisions for drop tanks or bombs can be assumed. The two surviving prototypes were later found scrapped of most anything of value and, as of this writing, are awaiting their fate with the USAF - perhaps seeing fit to restore at least one model for the USAF Museum in Dayton, Ohio. A sound concept nonetheless, the twin engine creation never really got off the ground.




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.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 750mph
Lo: 375mph
    This entry's maximum listed speed (506mph).

    Graph average of 562.5 miles-per-hour.
City-to-City Ranges
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  SYD
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  NYC
Graph showcases the Vultee XP-81's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
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Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
2
2

  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


Altitude Visualization
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Supported Roles
A2A
Interception
UAV
Ground Attack
CAS
Training
ASW
Anti-Ship
AEW
MEDEVAC
EW
Maritime/Navy
SAR
Aerial Tanker
Utility/Transport
VIP
Passenger
Business
Recon
SPECOPS
X-Plane/Development
A2A=Air-to-Air; UAV=Unmanned; CAS=Close Support; ASW=Anti-Submarine; AEW=Airborne Early Warning; MEDEVAC=Medical Evac; EW=Electronic Warfare; SAR=Search-Rescue