Slingsby T.65 Vega
Страна: Великобритания
Год: 1977

M.Hardy. Gliders & Sailplanes of the world

M.Hardy. Gliders & Sailplanes of the world

Vickers-Slingsby Vega

  This 15m Contest Class single-seater is the first sailplane, of entirely Slingsby design to appear since the liquidation of the former Slingsby Aircraft Co in July 1969 and its reorganisation as part of the Vickers group; it is now known as Slingsby Engineering Ltd (Aircraft Division). The Vega was designed to take advantage of the change in Standard Class rules permitting camber-changing flaps to be installed in this class after 1976. The cantilever mid-set wings are designed for optimum performance and have combined flaps/air brakes inboard and the ailerons outboard; the latter can be operated independently or in conjunction with the flaps. The wings have a unique single-lever operation for the flap and air brake system instead of using two separate levers as in other types; in the Vega the lever moves fore and aft in the usual way for air brake movement but is rotated by wrist action to select the flap positions which range from -12° to +12°. The air brakes are hinged to the flaps with continuous flexible straps. The Vega prototype first flew on 3 June 1977 and, after some initial problems resulting from stiffness of the single-lever flap/air brake control, resumed test flights in November that year; the first production delivery was in April 1978, by which time 48 had already been ordered. By the beginning of 1980 34 Vegas had been delivered. The wings are of foam plastics sandwich construction with a single carbon-fibre main spar, which keeps the weight of each wing down to only about 130lb; the Wortmann wing section and carbon-fibre spar allow a constant 15% thickness/chord ratio from root to tip, giving performance benefits at the higher speeds. The wing tips are turned downwards to reduce tip stalling and are protected by inset metal rubbing strakes, and a convenient feature is that all controls are automatically coupled on rigging, leaving only the centre pin to be inserted. The wings also hold up to 195lb of water ballast in shaped plastic bags, thus avoiding any leakage which may occur when the wing itself is used as a tank. The fuselage is a conventional semi-monocoque plastics structure, and is gently 'waisted' to reduce the possibility of airflow separation over the wing/fuselage junction; the tow hook is carried on the frame that carries the monowheel, and retracts with it. The latter has a brake, and an unusual feature for a sailplane is that the Vega's tailwheel retracts as well. The pilot sits upright under a long one-piece canopy which opens forwards and upwards, and is jettisonable. The cantilever T-tail has a tailplane of symmetrical Wortmann section with a carbon-fibre spar and a separate elevator with a spring trimmer. The T65C Sport Vega first flew on 18 December 1979, and this version differs from the Vega in having a glassfibre main spar, rotating trailing edge air brakes instead of flaps, and a fixed monowheel and tailwheel. There is no provision for water ballast.

Span: 49 ft 2 1/2 in
Length: 22 ft 0 1/2 in
Height: 4 ft 11 in
Wing area: 108.2 sqft
Aspect ratio: 22.4
Empty weight: 515 lb
Max weight: 970 lb
Max speed: 155 mph (in smooth air)
Max aero-tow speed: 92 mph
Min sinking speed: 2.21 ft/sec at 51 mph
Best glide ratio: 42:1 at 69 mph
The elegant lines of the Vega are well portrayed in the photograph. In an effort to improve airflow over the juncture of wing and fuselage, the latter has been gently waisted. Low-speed control is good.
Vickers-Slingsby Vega
Slingsby is tooling up for production of the Vickers-Slingsby Vega sailplane, seen during recent evaluation in the Lake District. Performance of the prototype is promising throughout the speed range. Further pre-production prototypes of the design, which features a retractable tailwheel, should be completed by the spring. The prototype first flew on June 3 last year.