Curtiss YP-37

Airplanes

Length

9.7536 m

Flat Wing Span

11.2776 m

Height

3.3528 m

Flat Wing Area

21.9251 m²

Cruise Speed

490.8499 km/h

Max Speed

547.177 km/h

Max Ceiling

10363.2 m

Number of Engines

First Flight

1937-04-01

Entry Into service

1939-01-01

Number Built

Maximum Range

917.3261 km

Pictures

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Aircraft	Maximum Range (km)
Curtiss YP-37	917.3261

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
CAC Mustang		9.83	11.28	Compare
Blackburn Nautilus	Rolls-Royce Kestrel	9.65	11.27	Compare
Bell P-63 Kingcobra		9.7536	11.5824	Compare
Canadair CT-114 Tutor	General Electric J85	9.7536	10.9728	Compare
Curtiss P-40 Warhawk		9.4488	11.2776	Compare
Aeromarine AS		9.4	11.2776	Compare

All data (23 fields)

Name: Curtiss YP-37
Manufacturer: Military designations USAAS/USAAF/USAF
Description: The Curtiss YP-37 was an American fighter aircraft developed by Curtiss-Wright in the late 1930s for the United States Army Air Corps (USAAC).
First Flight: 1937-04-01
Entry Into service: 1939-01-01
Designer: Military designations USAAS/USAAF/USAF
Length (m): 9.7536
Height (m): 3.3528
Cockpit Crew: 1
Max Speed (km/h): 547.177
Cruise Speed (km/h): 490.8499
Max Ceiling (m): 10363.2
Rate of Climb (m/s): 14.8336
Armament: 1 × 0.30 in M1919 Browning machine gun and 1 × 0.50 in M2 Browning machine gun
National Origin: United States of America
Number Built: 14
Powerplant Description: 1 × Allison V-1710-21 V-12 liquid-cooled piston engine, 746 kW (1000 hp) each
Primary Users: United States Army Air Corps
Status: Canceled
Wikipedia Article (URL): en.wikipedia.org/wiki/Curtiss_YP-37
Flat Wing Span (m): 11.2776
Flat Wing Area (m²): 21.9251
Number of Engines: 1