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HS.141

Hawker Siddeley · Cold War (1970–1991)

HS.141 — Fixed Wing
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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.

Specifications

Category
Fixed Wing
Domain
Civil
Era
Cold War (1970–1991)
Manufacturer
Hawker Siddeley
Service Entry
1978
Engine
2× turbofan engines
Thrust / Power
27000 lbf each
Length (ft)
120
Wingspan (ft)
75
Empty Weight (lb)
110300
MTOW (lb)
134200
Range (mi)
1200
Max Speed (mph)
432
Max Speed (Mach)
0.92