De Havilland Hornet

· De Havilland

Airplanes

Length

10.668 m

Flat Wing Span

13.716 m

Height

4.2672 m

Flat Wing Area

33.538 m²

Cruise Speed

434.5229 km/h

Max Speed

764.4384 km/h

Max Ceiling

12649.2 m

Number of Engines

First Flight

1944-07-28

Entry Into service

1946-01-01

Number Built

383

Maximum Take-Off Weight

8.2781 t (paragliders: kg)

Maximum Range

2381.829 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
De Havilland Hornet	8.2781	2381.829

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Nakajima Ki-201		11.5	13.7		Compare
Piaggio P.136		10.8	13.53		Compare
Saro Cutty Sark	Armstrong Siddeley Genet Major	10.3632	13.716		Compare
Fleet 50 Freighter	Jacobs R-915	10.97	13.72	10	Compare
Hitachi TR.1		10.6	14.1	6	Compare
SIPA S.70	Mathis G.8R	10.2	13.8	8	Compare

All data (23 fields)

Name: De Havilland Hornet
Manufacturer: De Havilland
Description: The de Havilland DH.103 Hornet, developed by de Havilland, is a fighter aircraft driven by two piston engines.
First Flight: 1944-07-28
Entry Into service: 1946-01-01
Service End: 1956-01-01
Designer: De Havilland
Type: Land and naval-based fighter aircraft
Length (m): 10.668
Height (m): 4.2672
Cockpit Crew: 1
Max Speed (km/h): 764.4384
Cruise Speed (km/h): 434.5229
Max Ceiling (m): 12649.2
Armament: 4 × 20 mm (.79 in) Hispano Mk. V cannon (with 190 rpg) in lower fuselage nose; 2 × 1,000 lb (454 kg) bombs under wing, outboard of engines; 8 × 60 lb (27 kg) RP-3 unguided rockets (Hornet F.3)
National Origin: United Kingdom
Number Built: 383
Powerplant Description: 2 × Rolls-Royce Merlin 130 V-12 liquid-cooled piston engines, 1544 kW (2070 hp) each
Primary Users: Royal Air Force, Royal Navy
Wikipedia Article (URL): en.wikipedia.org/wiki/De_Havilland_Hornet
Flat Wing Span (m): 13.716
Flat Wing Area (m²): 33.538
Number of Engines: 2