Miller Tern
Страна: США
Год: 1965
Планер

Single-seat high-performance sailplane
M.Hardy. Gliders & Sailplanes of the world
Фотографии

M.Hardy. Gliders & Sailplanes of the world

Miller Tern

  The Tern high performance single-seater was designed by Mr W. Terry Miller of Furlong, Pennsylvania, for amateur construction and the prototype, which was built in a total of 1,180 working hours, made its first flight in September 1965. An improved version, known as the Tern II, made its first flight in August 1968; this featured a wing span increased by 4ft 6in to 55ft 6in, increasing the aspect ratio from 20 to 22, and giving an improved best glide ratio and minimum sinking speed. During 1968 brake parachutes were fitted to the prototype Tern, and two types of these were later made available for installation in both versions of the Tern in the base of the rudder, namely a 6ft diameter cross parachute or a 5ft diameter guide surface parachute. By May 1970 nearly 100 Terns and 12 Tern IIs were under construction not only in the USA, but by amateurs in Africa, Australia, South America and Canada. Of conventional all-wood construction, the Tern has unswept cantilever shoulder wings which are two-piece two-spar spruce structures, entirely plywood covered. There are no flaps and the plain ailerons are also all wood; there are wooden spoilers in the wing lower surface used for approach and glide slope control. The semi-monocoque wooden fuselage has a plastic-reinforced glassfibre nose and plywood skinning aft of the cockpit. The cantilever all-wood tail unit has modified NACA laminar flow sections and special hinge-line contours to reduce drag and increase control effectiveness at large angles of deflection; there are no elevator or rudder tabs. Landing gear consists of a non-retractable monowheel forward of the cg housed in a streamlined pod, and skids under the nose and tail; there is a brake lever for applying pressure directly to the tyre. The pilot sits in a semi-reclining seat under a thre-epiece canopy, the centre portion of which hinges sideways for entrance and exit, and radio can be fitted.


Data: Tern II
Span: 55 ft 6 in
Length: 21 ft 3 1/2 in
Height: 5 ft 0 in
Wing area: 140 sq ft
Aspect ratio: 22.0
Empty weight: 550 lb
Max weight: 800 lb
Max speed:120 mph (smooth air)
Max aero-tow speed: 88 mph
Min sinking speed: 1.95 ft/sec at 48 mph
Best glide ratio: 38:1 at 60 mph
Miller Tern single-seat sailplane built by Mr Alex Stuart of Phoenix, Arizona
Miller Tern II built by Mr Charles Wieland of Huntington Beach, California
Miller Tern built by Mr George Allen of Weatherford, Texas, with a special 52 ft span wing and cockpit canopy from a Bryan (Schreder) HP-14