Hawker Siddeley Nimrod

Length
38.4048 m
Flat Wing Span
34.7472 m
Height
9.4488 m
Flat Wing Area
197.0501 m²
Cruise Speed
788.9513 km/h
Max Speed
925.9992 km/h
Max Ceiling
13411 m
Number of Engines
4
Aircraft Engine
First Flight
1967-05-23
Entry Into service
1969-10-02
Number Built
49
Maximum Take-Off Weight
87.0897 t (paragliders: kg)
Maximum Range
8335.852 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Hawker Siddeley Nimrod 87.0897 8335.852

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Kawasaki P-1 38 35.4 Compare
British Aerospace Nimrod AEW3 Rolls-Royce Spey 41.7576 35.052 Compare
Tupolev Tu-110 Lyulka AL-7 38.3 37.5 100 Compare
McDonnell Douglas YC-15 Pratt & Whitney JT8D 37.9 33.6 150 Compare
Martin P6M SeaMaster 40.8432 31.0896 Compare
Handley Page Victor 34.7472 33.528 Compare
All data (24 fields)
Name
Hawker Siddeley Nimrod
Manufacturer
British Aerospace
Description
The Hawker Siddeley Nimrod is a retired maritime patrol aircraft developed and operated by the United Kingdom.
First Flight
1967-05-23
Entry Into service
1969-10-02
Service End
2011-06-28
Designer
British Aerospace
Length (m)
38.4048
Height (m)
9.4488
Cockpit Crew
13
Max Speed (km/h)
925.9992
Cruise Speed (km/h)
788.9513
Max Ceiling (m)
13411
Armament
2× under-wing pylon stations and an internal bomb bay
Capacity Description
13,500 lb
National Origin
United Kingdom
Number Built
49
Powerplant Description
4 × Rolls-Royce Spey turbofan engines
Primary Users
Royal Air Force
Wikipedia Article (URL)
en.wikipedia.org/wiki/Hawker_Siddeley_Nimrod
Flat Wing Span (m)
34.7472
Flat Wing Area (m²)
197.0501
Aircraft Engine
Rolls-Royce Spey
Number of Engines
4