Length
10.0584 m
Flat Wing Span
10.9728 m
Height
3.048 m
Flat Wing Area
19.8534 m²
Max Speed
774.0945 km/h
Max Ceiling
12192 m
Number of Engines
1
Aircraft Engine
First Flight
1967-10-26
Number Built
146
Maximum Take-Off Weight
5.2163 t (paragliders: kg)
Total Fuel Capacity
1663.869
Maximum Range
2224.113 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
BAC Strikemaster 5.2163 1663.869 2224.113

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m)
Canadair CT-114 Tutor General Electric J85 9.7536 10.9728 Compare
Bell P-63 Kingcobra 9.7536 11.5824 Compare
AIDC T-CH-1 10.26 12.19 Compare
Epic Victory Pratt & Whitney Canada PW600 10.19 11.08 Compare
Douglas O2D 9.7536 10.9728 Compare
Arado Ar 80 10.3 10.89 Compare
All data (27 fields)
Name
BAC Strikemaster
Manufacturer
British Aircraft Corporation
Description
The BAC 167 Strikemaster is a jet-powered training and light attack aircraft designed and produced by the British Aircraft Corporation.
ICAO Code
STRK
First Flight
1967-10-26
Production End
1983-01-01
Service End
1993-01-01
Designer
British Aircraft Corporation
Type
Attack aircraft, Jet trainer
Length (m)
10.0584
Height (m)
3.048
Max Speed (km/h)
774.0945
Min Speed (km/h)
157.7157
Max Ceiling (m)
12192
Rate of Climb (m/s)
26.67
Armament
2× 7.62 mm machine guns with 550 rounds each; Four (two per wing)
National Origin
United Kingdom
Number Built
146
Powerplant Description
1 × Rolls-Royce Viper Mk.535 turbojet
Primary Users
Royal Saudi Air Force, Ecuadorian Air Force , Kenya Air Force , Royal New Zealand Air Force
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/BAC_Strikemaster
Flat Wing Span (m)
10.9728
Flat Wing Area (m²)
19.8534
Wake Category
L
Aircraft Engine
Armstrong Siddeley Viper
Number of Engines
1