Oldershaw O-3
Страна: США
Год: 1967
Планер

M.Hardy. Gliders & Sailplanes of the world
Фотографии

M.Hardy. Gliders & Sailplanes of the world

Oldershaw O-3

  The original O-3 single-seat sailplane was designed and built by Mr Vernon W. Oldershaw of Bakersfield, California, in 15 months for a cost of $4,000, and it made its first flight in June 1967. He then began to develop a retractable powerplant installation which was added to a second O-3 completed in 1975, the engine being used primarily for take-off and climb to soaring height. It is a 31 hp Yamaha Snowmobile SW433 two-stroke 'flat twin' driving a two-blade fixed-pitch wooden pusher propeller, the pylon-mounted propeller retracting forwards into the fuselage behind closed doors to lie over the engine, which is behind the cockpit. There is a single aluminium fuel tank in the fuselage of 2.5 US gallons capacity. The O-3 is of all-wood construction with cantilever shoulder wings and a V-tail; the wings have a spruce spar and plywood ribs and skins, with wooden ailerons and air brakes on the trailing edges. The ellipitcal-section fuselage is built up from plywood bulkheads, the front portion from the nose to the wing trailing edge having a glassfibre outer shell and the remainder being plywood-covered. The tail surfaces, which are slightly swept back, are of similar construction to the wings. There is a retractable rubber-sprung monowheel and a tailskid. The pilot sits under a one-piece flush-fitting cockpit canopy.


Span: 55 ft 0 in
Length: 23 ft 0 in
Height: 4 ft 8 in
Wing area: 125.0 sqft
Aspect ratio: 24.1
Empty weight: 780 lb
Max weight: 1,000 lb
Max speed: 125 mph (in smooth air, power off)
Max cruising speed: 95 mph (power on)
Min sinking speed: 2.30 ft/sec at 55 mph
Best glide ratio: 37:1 at 68 mph
Take-off run: 900 ft
Range with max fuel: 50 miles
Oldershaw O-3.