Hawker Siddeley HS.141

The Hawker Siddeley HS.141 was a 1970s design study and submission for a British V-STOL airliner requirement. Designed by Hawker Siddeley Aviation and tested in wind tunnels neither prototypes nor production aircraft were produced.

The Hawker Siddeley HS.141 was a 1970s design study and submission for a British V/STOL airliner requirement.1
* Hawker Siddeley HS.141 – Information and images – www.aiaa.2

Made by Hawker Siddeley.

comerciales VTOL, como el Hawker Siddeley HS.141, con el que se quería obtener prestaciones de un reactor que operase desde el centro de las ciudades, pero este concepto era impracticable.3
Height Main
909.3199999999999
Height Alt
9 m
Engine(jet)
Rolls-Royce RB.220
Length Alt
36.63 m
Max Takeoff Weight Main
134200.0
Thrust Main
27000
Jet Or Prop
both
Lists
*List of civil aircraft
Range Main
1
200 miles
Max Speed Alt
806.0
Type Of Prop
Lift jet
Introduced
Intended 1978-9
Max Speed Main
435
Capacity
102
Cruise Speed Main
375
Max Takeoff Weight Alt
60872.0
Number Built
None
Crew
Not given
Thrust Alt
120.0
Cruise Speed Alt
695.0
Area Main
1060.0
Span Alt
22.86 m
Plane Or Copter?
plane
Power Alt
4670.0
Engine(prop)
Rolls-Royce RB.202
Manufacturer
Hawker Siddeley
First Flight
Not flown
Number Of Jets
2
Span Main
75.0
Power Main
10300
Number Of Props
16
Type of jet
turbofan
Empty Weight Alt
50031.0
Length Main
3662.68
Area Alt
98.47
Range Alt
1931.0
Similar Aircraft
* Armstrong Whitworth AW.681* Dornier Do 31
Empty Weight Main
110300.0
Category
British airliners 1970-1979
Hawker Siddeley aircraft

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