Manuel Hawk
| Hawk | |
|---|---|
| Role | Glider |
| National origin | United Kingdom |
| Designer | W.L. Manuel |
| First flight | 25 November 1972 |
| Number built | 1 |
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The Manuel Hawk was a homebuilt single-seat glider designed and constructed in the UK around 1970. Only one example was flown.
Design and development
W.L. "Bill" Manuel, who had designed and built a glider as early as 1929 and was later responsible for the Willow Wren, designed the Hawk during his retirement. It was a single-seat aircraft intended for soaring in weak thermals.[1] He built the Hawk himself during 1968 and 1969[2] before taking it to the College of Aeronautics at Cranfield for structural analysis.[1]
The Hawk was an all-wood, cantilever shoulder wing monoplane. The centre section of the three-piece wing was of constant chord and fitted with parallel-ruler type, upper surface airbrakes positioned at 28.26% of the half-span and at 42% chord. The outer panels were tapered with rounded tips and carried the ailerons. The wing had an angle of incidence of 3° and the outer panels had 3° of dihedral. Structurally, the wings had a spruce main spar at 33% chord with a plywood-covered torsion box ahead of it and fabric covering aft.[1]
The fuselage was a semi-monocoque spruce structure with plywood covering. The fin was also plywood-covered, carrying a fabric-covered rudder which reached from the underside of the T-tail to the bottom of the fuselage. The fixed-incidence tailplane was likewise plywood-covered and the elevator fabric-covered. The latter carried a Flettner-type trim tab on its starboard edge. The Hawk's single seat was forward of the wing and under a hinged, framed canopy. It landed on a single fixed wheel assisted by a tailskid.[1]
The first flight was on 25 November 1972, piloted by Howard Torode of the Cranfield Institute. Tests showed a lack of rudder power, quickly cured by an increase in area, but no other concerns.[1]
Operational history
Only one Hawk was built. It was certified as BGA 1778 by February 1973.[3] In July that year it was at the Sywell PFA weekend, where it gained third place in a competition amongst homebuilt aircraft.[4]
Specifications
Data from Jane's All the World's Aircraft 1973/74[1]
General characteristics
- Crew: 1
- Length: 20 ft 6 in (6.25 m)
- Wingspan: 42 ft 0 in (12.80 m)
- Height: 4 ft 8 in (1.41 m)
- Wing area: 149 sq ft (13.8 m2)
- Aspect ratio: 12
- Airfoil: Wortmann FX6-184 inboard, FX-61-210 tip
- Empty weight: 407 lb (185 kg) equipped
- Max takeoff weight: 640 lb (290 kg)
Performance
- Maximum speed: 91 mph; 79 kn (146 km/h) in smooth air. Like the following performance figures, this speed is for maximum take-off weight
- Stall speed: 36 mph (31 kn; 58 km/h)
- G limits: +4
- Maximum glide ratio: best 25:1 at 41.5 mph (36 kn, 66.5 km/h)
- Rate of sink: 152 ft/min (0.77 m/s) minimum at 38 mph (33 kn, 61 km/h)
- Wing loading: 11.8 lb/sq ft (58 kg/m2) maximum
References
- 1 2 3 4 5 6 Taylor, John W R (1973). Jane's All the World's Aircraft 1973/74. London: Jane's Yearbooks. pp. 576–7. ISBN 0-354-00117-5.
- ↑ Ellison, Norman (1971). British Gliders and Sailplanes. London: A & C Black Ltd. p. 142. ISBN 978-0-7136-1189-2.
- ↑ "UK register". Air Britain Digest 2 (4): 139. July–August 1973.
- ↑ "Flying is Popular.". Flight. Vol. 104 no. 3358. 19 July 1973. p. 92.
External links
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