Hawker 800 (Raytheon)

· Raytheon

Airplanes

Length

15.5448 m

Flat Wing Span

15.5448 m

Height

5.1816 m

Flat Wing Area

34.7457 m²

Cruise Speed

740.7994 km/h

Max Speed

844.5113 km/h

Max Ceiling

13106.4 m

Number of Engines

First Flight

1983-06-26

Number Built

650

Maximum Take-Off Weight

12.4284 t (paragliders: kg)

Total Fuel Capacity

5673.521

Maximum Range

4778.16 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Hawker 800 (Raytheon)	12.4284	5673.521	4778.16

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Mikoyan-Gurevich I-320	Klimov VK-1	15.775	14.2		Compare
Douglas F3D Skyknight		13.716	15.24		Compare
Grumman F7F Tigercat		13.716	15.5448		Compare
Bell XP-83		13.4112	16.1544		Compare
British Aerospace 125	Armstrong Siddeley Viper	15.24	14.3256	8	Compare
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All data (27 fields)

Name: Hawker 800 (Raytheon)
Manufacturer: Raytheon
Description: The Hawker 800 is a mid-size twinjet corporate aircraft.
ICAO Code: H25B
First Flight: 1983-06-26
Production End: 2013-01-01
Designer: Raytheon
Type: Mid-size business jet
Length (m): 15.5448
Height (m): 5.1816
Cockpit Crew: 2
Max Speed (km/h): 844.5113
Cruise Speed (km/h): 740.7994
Min Speed (km/h): 170.3839
Max Ceiling (m): 13106.4
Rate of Climb (m/s): 15.748
Capacity Description: 8 / 2000 lb maximum payload
National Origin: United Kingdom
Number Built: 650
Powerplant Description: 2 × Honeywell TFE731-5BR turbofan engines
Primary Users: Japan Air Self-Defense Force, Brazilian Air Force , Royal Saudi Air Force
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Hawker_800
Flat Wing Span (m): 15.5448
Flat Wing Area (m²): 34.7457
Wake Category: M
Number of Engines: 2