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