Search
Close this search box.

Curtiss XP-37 & YP-37

The Curtiss P-37 was an American fighter aircraft made by Curtiss-Wright in 1937 for the US Army Air Corps.

A development of the Curtiss P-36 Hawk to use an inline engine instead of the radial engine of the P-36 the fuselage was lengthened, and the cockpit moved back.

A small number of YP-37 aircraft was built for Air Corps evaluation.

The expected top speed was not achieved, and the project terminated in favour of the Curtiss P-40 Hawk.

In early 1937, after realizing the P-36 Hawk was inferior to more modern European designs, the USAAC ordered Curtiss to adapt one P-36 to the new liquid-cooled turbo-supercharged Allison V-1710.

The prototype Hawk was fitted with a turbo-supercharged 1,150 hp (860 kW) Allison V-1710-11 as the XP-37 (company designation Model 75I).

The cockpit was moved back towards the tail to make room for the massive turbo-superchargers, and the engine was cooled by two radiators on either side of the nose.

Armament was one 0.30 in (7.62 mm) M1919 Browning machine gun and one 0.50 in (12.70 mm) M2 Browning heavy machine gun mounted in the nose.

Although the turbo-supercharger was extremely unreliable and visibility from the cockpit on take-off and landing was virtually non-existent, the USAAC was sufficiently intrigued by the promised performance to order 13 service test YP-37s and spares at a contract cost of $531,305.12 in 1938. 

These aircraft were powered by an improved V-1710-21 with a more reliable supercharger mounted in a lengthened nose.

However, reliability problems and poor visibility continued to plague the YP-37, and the project was cancelled in favour of a parallel development, the P-40 Warhawk.

Variants

XP-37

One aircraft built with a V-1710-11 engine.

YP-37

13 aircraft built with a V-1710-21 engines and extended fuselage.

 Specifications

YP-37

Crew

1

Length

32 ft 11.5 in (10.046 m)

Wingspan

37 ft 3.5 in (11.367 m)

Height

11 ft 1 in (3.38 m)

Wing area

236 sq ft (21.9 m2)

Airfoil

Root

NACA 2215 

Tip

NACA 2209

Empty weight

5,592 lb (2,536 kg)

Gross weight

6,700 lb (3,039 kg)

Powerplant

1 × Allison V-1710-21 V-12 liquid-cooled piston engine,

1,000 hp (750 kW)

Propellers

3-bladed Curtiss electric constant-speed propeller

Performance

Maximum speed

340 mph (550 km/h, 300 kn) at 10,000 ft (3,000 m)

331 mph (288 kn; 533 km/h) at 20,000 ft (6,100 m)

Cruise speed

305 mph (491 km/h, 265 kn)

Range

570 mi (920 km, 500 nmi)

Service ceiling

34,000 ft (10,000 m)

Rate of climb

2,920 ft/min (14.8 m/s)

Time to altitude

20,000 ft (6,100 m) in 8 minutes 30 sec

Armament

Guns

1 x 0.30 in (7.62 mm) M1919 Browning machine gun 

&

1 x 0.50 in (12.7 mm) M2 Browning machine gun.

Share on facebook