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Bell XP-83


Jet-Powered Escort Fighter Aircraft Prototype


United States | 1945



"The ultimately-cancelled Bell XP-83 Escort Fighter was developed from the disappointing Bell P-59 Airacomet series during the immediate post-World War 2 years."



Authored By: Staff Writer | Last Edited: 02/06/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.
In 1942, with World War in full swing across Europe and the Pacific, work began on an American turbo jet-powered aircraft to keep pace with developments around the world. This formally became the Bell P-59 "Airacomet" which achieved first flight on October 1st, 1942, becoming the first American jet-powered aircraft in history. However, it was deemed limited from a performance standpoint and production lasted just 66 total units.

In March of 1944, the war was reaching feverish pitches and jet programs were evolving along all fronts - particularly in Germany and in Britain. The United States Army Air Forces (USAAF) contracted Bell once again, this time to build a new jet-powered aircraft for the fighter escort role. By this time, American bomber raids were a regular occurrence over enemy held territory and piston-engined mounts were being used in defense of these masses of bomber formations being sent against enemy targets daily. A jet-powered fighter escort would provide technological superiority and allow for unheard of performance gains if the design could be harnesses properly and optimized to the extreme. The USAAF charged Bell with two prototype aircraft on July 31st, 1944.

The main challenge of the era concerning turbojet powered flight was in the rather thirsty nature of the new engine technology. Turbojets allowed for unprecedented performance gains to be sure but they proved short-term creatures that severely limited many tactical benefits. Bell took their underperforming P-59 and had attempted to introduce longer operational ranges as the "Model 40" company product. It was this derivative that the company would further into the XP-83. The XP-83 was slightly reminiscent of the original P-59 design with various aerodynamic and structural differences to clearly differentiate the types. Overall, however, the P-59 origins could clearly be identified in the Model 40 to the discerning student. Wings remained straight appendages while the empennage was capped by a conventional tail surface. Construction of the aircraft included metal skin left in an unfinished silver - consistent with many experimental aircraft of the 1940s and 1950s. The pilot managed a rather excellent view from his cockpit position at the front of the aircraft under a tear-drop style canopy. Design of the XP-83 was attributed to Charles Rhodes and the engine of choice became 2 x General Electric J33-GE-5 turbojets of 4,000lbs thrust each.

After some initial ground testing, the prototype achieved first flight on February 25th, 1945. Overall, the flight was a modest success but after-mission reports detailed the design as lackluster, underperforming and requiring much management. A follow-up prototype given a new tail assembly was debuted t o correct instability issues encountered by the first. In either case, the XP-83 was severely lacking in most respects. The type survived the end of the war in September of 1945 and continued on as a ramjet testbed into 1946. In 1947, with the war years over and many-a-production-contract slashed or outright cancelled, the XP-83 project died. The American military ultimately invested $4.2 million dollars into the cancelled program that yielded all but two prototypes. The straight-wing, jet-powered Lockheed P-80 Shooting Star - adopted in 1945 - was firmly entrenched as the primary jet-powered fighter of American forces for the time being until replaced by the North American F-86 Sabre during the Korean War.

All told, the XP-83 would see a top speed of 522 miles per hour and range was 1,700 miles on internal fuel though external drop tanks could be fitted for an increase of 2,000 miles. Its operational service ceiling was 45,000 feet which of course required use of a pressurized cockpit. Rate-of-climb was 5,600 feet per minute.

Over her short development cycle, the XP-83 was envisioned to stock a variety of armament options for the production versions. These included 6 x 12.7mm M2 Browning heavy machine guns as standard. The 15.2mm T17E3 prototype heavy machine gun was also considered as were 4 x 20mm Hispano cannons. A 37mm cannon could also have been fitted in the nose assembly for a truly potent offensive punch.

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Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Bell XP-83 Jet-Powered Escort Fighter Aircraft Prototype.
2 x General Electric J33-GE-5 turbojet engines developing 4,000 lb thrust each.
Propulsion
522 mph
840 kph | 454 kts
Max Speed
45,932 ft
14,000 m | 9 miles
Service Ceiling
1,731 miles
2,785 km | 1,504 nm
Operational Range
5,650 ft/min
1,722 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Bell XP-83 Jet-Powered Escort Fighter Aircraft Prototype.
1
(MANNED)
Crew
44.8 ft
13.67 m
O/A Length
53.0 ft
(16.15 m)
O/A Width
15.3 ft
(4.65 m)
O/A Height
14,110 lb
(6,400 kg)
Empty Weight
27,558 lb
(12,500 kg)
MTOW
Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.
RANGE
ALT
SPEED
Armament
Available supported armament and special-mission equipment featured in the design of the Bell XP-83 Jet-Powered Escort Fighter Aircraft Prototype .
PROPOSED:
6 x 12.7mm Browning heavy machine guns
6 x 15.2mm T17E3 heavy machine guns
4 x 20mm Hispano cannons
1 x 37mm cannon in nose
Variants
Notable series variants as part of the Bell XP-83 family line.
XP-83 - Base Series Designation; two prototypes completed.
Operators
Global customers who have evaluated and/or operated the Bell XP-83. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 2 Units

Contractor(s): Bell Aircraft - USA
National flag of the United States

[ United States ]
Relative Max Speed
Hi: 750mph
Lo: 375mph
Aircraft Max Listed Speed (522mph).

Graph Average of 563 MPH.
Era Crossover
Pie graph section
Pie graph section
Showcasing Aircraft Era Crossover (if any)
Max Alt Visualization
Small airplane graphic
Production Comparison
2
36183
44000
Entry compared against Ilyushin IL-2 (military) and Cessna 172 (civilian) total production.
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Aviation Timeline
EarlyYrs
WWI
Interwar
WWII
ColdWar
Postwar
Modern
Future
1 / 1
Image of the Bell XP-83
Right side front under view of the Bell XP-83 jet-powered fighter escort prototype in flight; 1945

Mission Roles
Some designs are single-minded in their approach while others offer a more versatile solution to airborne requirements.
AIR-TO-AIR COMBAT
INTERCEPTION
X-PLANE
Recognition
Some designs stand the test of time while others are doomed to never advance beyond the drawing board; let history be their judge.
Going Further...
The Bell XP-83 Jet-Powered Escort Fighter Aircraft Prototype appears in the following collections:
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