Bell P-63 Kingcobra

Bell P-63 Kingcobra

Successor to the P-39 Airacobra

The P-63 was developed by Bell Aircraft to address the shortcomings of the P-39, particularly its poor high-altitude performance.

First flight

December 7, 1942—symbolically one year after Pearl Harbour.

Key improvements

Laminar flow wing for better aerodynamics.

A more powerful Allison V-1710 engine with a remotely mounted supercharger.

Heavier armament

37 mm cannon through the propeller hub and four .50-calibre machine guns.

U.S. Army Air Forces

Limited Use

Rejected for combat

Despite its improvements, the P-63 was not accepted for combat by the USAAF.

Training role

It was used stateside for training and target practice, including as a target aircraft for gunnery training due to its robust construction.

Soviet Air Force

Primary Combat Operator

Lend-Lease deliveries

Over 2,400 P-63s were shipped to the USSR under the Lend-Lease programme, making the Soviets its main wartime user.

Combat role

Eastern Front

Used primarily in ground-attack missions and close air support.

Far East

Saw action against Japanese forces in the closing months of the war.

Tank buster reputation

The powerful nose-mounted cannon made it effective against armoured targets, earning it a reputation as a Soviet tank buster.

Production and Legacy

Total built

3,303 units between 1943 and 1945.

Variants

Included the P-63A, C, and E models, with incremental improvements.

Postwar use

Continued service in Soviet and French air forces after WWII.

The Variants

XP-63 (Model 24)

Original Prototype

Quantity

2 aircraft

Serials

41-19511 and 41-19512

Purpose

Initial development prototypes for the Kingcobra series

Notes

These aircraft featured a mid-engine layout with tricycle landing gear and were powered by the Allison V-1710-93 engine.

Both were lost in accidents during early testing, prompting design revisions and the creation of the XP-63A.

XP-63A

Merlin Testbed

Quantity

1 aircraft

Serial

42-78015

Purpose

Replacement prototype, originally intended to test the Rolls-Royce Merlin engine for the proposed P-63B variant

Notes

Though the Merlin-powered concept was abandoned, the XP-63A served as a critical test platform for aerodynamic refinements and structural improvements that informed the P-63A production series.

P-63A (Model 33)

First Production Series

Quantity

1,725 aircraft

Engine

Allison V-1710-93 or -95, ~1,325 hp

Armament

1 × 37 mm M4 cannon firing through the propeller hub,

2 × .50-cal machine guns in the nose,

and

2 × .50 cal. wing-mounted guns (varied by sub-mark)

Sub-marks

Included A-1 through A-10, with incremental improvements in armor, radio equipment, and engine cooling

Notes

Widely exported under Lend-Lease, especially to the Soviet Union, where it saw extensive combat service.

The P-63A retained the general layout of the P-39 but featured improved performance and survivability.

P-63C

Refined Combat Variant

Quantity

1,227 aircraft

Engine

Allison V-1710-117, 1,500 hp

(1,800 hp with water injection)

Wing

Reduced span by 10 inches (250 mm) for improved roll rate

Notes

Introduced a four-blade propeller and enhanced engine cooling.

The C-series was the most powerful production variant and was also heavily exported to the USSR.

Despite its improvements, it was never adopted as a front-line fighter by the USAAF.

P-63D

High-Speed Prototype

Quantity

1 aircraft (43-11718)

Engine

Allison V-1710-109 (E22), 1,425 hp

Wing

Increased span to 39 ft 2 in (11.94 m); wing area expanded to 255 sq ft (23.7 m²)

Canopy

Introduced a rearward-sliding bubble canopy for improved visibility

Notes

Designed for superior high-altitude performance, but the series was cancelled in 1945 due to shifting priorities and the emergence of jet aircraft.

P-63E

Modified D-Series

Quantity

13 aircraft

Differences

Retained the P-63D’s wing and engine but reverted to the standard framed cockpit and added a ventral fin extension for stability

Notes

Served primarily as test aircraft; never entered mass production or combat service.

P-63F (Model 43)

Tail-Heavy Prototype

Quantity

2 aircraft (43-11719 and 43-11722)

Engine

Allison V-1710-135

Tail

Enlarged vertical stabilizer for improved directional control

Notes

Intended to address stability issues at high speeds.

The variant was cancelled before further development due to the end of the war and lack of demand.

RP-63A/C “Pinball”

Armored Target Aircraft

Quantity

5 RP-63A conversions + 95 RP-63 A production-line modification: 200 RP-63C production aircraft

Purpose

Used as manned flying targets for gunnery training with frangible ammunition

Features

Armored skin, reinforced canopy, and sensors that triggered lights when hit

Redesignation

Surviving aircraft were redesignated QF-63A and QF-63C in 1948

Notes

Despite their role as “targets”, many were used as target tugs.

Their durability and unique role made them a distinctive sub-series in the Kingcobra lineage.

RP-63G “Pinball”

Dedicated Target Variant

Quantity

2 prototypes (43-11723 and 43-11724) + 30 production aircraft

Features

Flush dorsal air inlet, improved hit-detection lighting system

Redesignation

Remaining aircraft redesignated QF-63G in 1948

Notes

These were purpose-built flying targets, not conversions.

Their specialised design made them ideal for safe gunnery training with frangible rounds.

L-39

Naval Research Aircraft

Quantity

2 aircraft (converted from surplus P-63Cs)

Purpose

Contracted by the U.S. Navy for aerodynamic testing

Focus

Studied low-speed and stall behavior of high-speed wing designs

Notes

These aircraft contributed to postwar research into swept-wing and transonic flight characteristics, influencing early jet development.

Specifications (P-63A)

Crew

One

Length

32 ft 8 in (9.96 m)

Wingspan

38 ft 4 in (11.68 m)

Height

12 ft 7 in (3.84 m)

Wing area

248 sq ft (23.0 m²)

Airfoil

Root

NACA 66-116

Tip

NACA 66-216

Empty weight

6,800 lbs (3,084 kg)

Gross weight

8,800 lbs (3,992 kg)

Max takeoff weight

10,700 lbs (4,853 kg)

Powerplant

1 × Allison V-1710-117 V-12 liquid-cooled piston engine,

1,800 hp (1,300 kW)

Propellers

4-bladed constant-speed propeller

Performance

Maximum speed

410 mph (660 km/h, 360 kn) at 25,000 ft (7,600 m)

Range

450 mi (720 km, 390 nmi)

Ferry range

2,200 mi (3,500 km, 1,900 nmi)

Service ceiling

43,000 ft (13,000 m)

Rate of climb

2,500 ft/min (13 m/s)

Wing loading

35.48 lbs./sq ft (173.2 kg/m²)

Power/mass

0.20 hp/lbs (0.33 kW/kg)

Armament

Guns

1 × 37 mm (1.5 in) M4 cannon firing through the propeller hub.

From the A-9 version of the aircraft onward,

the M4 gun was replaced with the slightly improved M10 37 mm cannon.

which used a disintegrating link ammunition belt,

Increasing the ammo capacity to 58 rounds, the M10 also had a slightly higher rate of fire.

4 × 0.50 in (12.7 mm) M2 Browning machine guns.

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