Shorts Sherpa Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
4 October 1953 |
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Sherpa: |
1 - Shorts, Belfast |
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Type Specification | |
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Applies to: |
Shorts S.B.4 Sherpa |
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Type: |
Experimental tailless monoplane |
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Wing: |
High wing, cantilever monoplane. Wing construction is mainly of wood. Leading edge is swept and wing tapers |
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Fuselage: |
Fuselage of light alloy construction |
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Tail Unit: |
No horizontal tail surfaces, single fin and rudder |
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Landing Gear: |
Fixed tricycle landing gear attached to fuselage |
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Power Plant: |
Two 350 lb thrust Turbomeca Palas turbojets in fuselage. Intake is on top of wing with jet outlets on either side of trailing edge |
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Accommodation: |
Single seat for pilot in enclosed cockpit in nose |
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Dimensions | |
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Span: |
38 ft |
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Length: |
31 ft 10 in |
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Height: |
Unknown |
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Wing Area: |
230 sq ft |
Weights | |
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Empty: |
3,000 lb |
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All-up: |
3,300 lb |
Performance | |
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Max Speed: |
170 mph |
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Duration: |
50 min |
Preserved in British Museums | |
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Sherpa: |
G-36-1 - Norfolk and Suffolk Aviation Museum, Flixton - Fuselage |
Web Sites | |
None known | |