Short SB.1
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Short SB1 | |
---|---|
Type | experimental glider |
Manufacturer | Short Brothers |
Designed by | David Keith-Lucas |
Maiden flight | 14 July, 1951 |
Number built | 1 |
Contents |
[edit] History
The Short Brothers Short SB.1 was a tailless glider designed by David Keith-Lucas and Professor G.T.R.Hill and built by Shorts as a private research venture, to test the concept of the aero-isoclinic wing.
For the first flight on 14 July, 1951 the SB1 was winch-launched and the gliding characteristics were found by Shorts' Chief Test Pilot Tom Brooke-Smith to be satisfactory.
Further test flights were followed on 30 July, 1951 by the first towed launch: the SB1 was towed behind a Short Sturgeon to a height of 10,000 ft, and the flight was completed successfully. Brooke-Smith experience the problems inherent in flying a light aircraft in the turbulence caused by the towing aircraft, and the second flight (with a longer towline, which was intended to alleviate the problem) almost ended catastrophically: Brooke-Smith had to cast off at low altitude and force-landed, injuring himself seriously and damaging the aircraft.
The company persevered with the project, however, redesigning the aircraft and adding two small turbojet engines. The result was the Short SB.4 Sherpa
[edit] Specifications
[edit] General characteristics
- Crew: one
- Length: ft in (m)
- Wingspan: ft (m)
- Height: ft in (m)
- Wing area: ft² (m²)
- Empty: lb ( kg)
- Loaded: ( kg)
- Maximum takeoff: lb ( kg)
- Powerplant: none
[edit] Performance
- Maximum speed: mph ( kph)
- Endurance: minutes
- Range: mi ( km)
- Service ceiling: ft ( m)
- Rate of climb: ft/min ( m/min)
- Wing loading: lb/ft² ( kg/m²)
- Power/Mass: hp/lb ( kW/kg)