Marsden Gemini

Chipman Glider Field, the Edmonton Soaring Club, Dr. Dave Marsden’s home club, 1982
(courtesy Bruce Friesen)

Designed by David Marsden and built by Marsden, E. Dumas and M.D. Jones, the side-by-side two-place Gemini, which flew in 1973, has a genuine variable geometry planform. Marsden, who successfully modified the British Operation Sigma Type C variable geometry glider, used a number of the Sigma features in his design. It has full span 35 % chord Fowler flaps which are extended when climbing and retracted when cruising. When extended, a high maximum coefficient of lift of 2.2 is achieved, giving a good climb performance. The flaps also deflects to 80 degree for approach control. It has slotted ailerons for improved roll control.

First flying in October 1973, during the 1970’s the Gemini set seven Canadian multi-place records, including the 500 km speed triangle.

The Gemini is all metal except for GFRP forward fuselage; stainless steel ribs, fittings and control system.

Wing span: 18.5 m / 60.75 ft
Wing area: 11.52 sq.m / 124 sq.ft
Length: 7.77 m / 25 ft 6 in
Height: 1.52 m / 5 ft 0 in
Empty Weight: 356 kg / 785 lb
Payload: 220 kg / 455 lb
Gross Weight: 576 kg / 1240 lb
Wing Load: 50 kg/sq.m / 10 lb/sq.ft
Water Ballast: 0
Stalling speed: 35 kt / 65 km/h
L/D Max: 40 at 119 kph / 64 kt / 74 mph
Best glide ratio: 38 at 60 kt / 110 km/h
Min Sink: 0.63 m/s / 2.08 fps / 1.23 kt
Min sinking: 0.75 m/sec / 2.46 ft/sec at 43 kt / 80 km/h
Aspect ratio: 29.8
Airfoil: Wortmann FX-61-163/35SF mod.
Seats: 2
No. Built: 1

Markwalder Marabu

Designed by Ing. Albert Markwalder and built by Enst Bärfuss circa 1968, the Markwalder Marabu is an all-wood three seater featuring plywood skin over the entire structure. The cantilever wing houses four aluminium/polyester fuel tanks. Wing root fillets and wingtips are of moulded fibreglass the vortex-control tips modelled after those on the Cessna 210. Airfoil at the wing root is an NACA 23012, tapering to NACA 23006 at the tips. Flaps lower to 60 degrees.

The retractable landing gear is manually operated, swings aft into ‘blisters’ under the wings, leaving the tires partially exposed to reduce damage in the event of a gear up landing.

Plans were not offered for sale.

Engine: Lycoming O-320, 150 hp
Prop: Hartzell VP 74 in
Max level speed: 171 mph
Cuise: 152 mph
ROC: 985 fpm
Empty weight: 1430 lb
MAUW: 2200 lb
Wingspan: 31 ft 10 in
Length: 24 ft 3 in
Height: 6 ft 7 in
Fuel capacity: 150 lt / 39.6 USG
Wing area: 150 sq.ft

Markwalder Elfe PM-3

The Elfe series started from a 9 m sailplane designed by W.Pfenninger before World War II. A new design was introduced by him in 1947 to become the Elfe 2, probably the first sailplane with a laminar flow airfoil. Subsequently the series was further developed by Markwalder in 1951 to become the Elfe PM-3 (brought to the US in the sixties).

Markwalder had completed the drawings after Ruedi Sägesser had problems with the construction. Pfenninger came up with the idea of the construction.

Marinavia Farina Srl

Italy
Marinavia Farina Srl was founded in 1946 by industrial designer Domenico Farina with headquarters in Milan. Designed and built several gliders and sailplanes, and prototype QR.14 Levriero four seat touring aircraft, powered by two de Havilland Gipsy Major 10 engines, first flown 1947, in which year it won Coppa dell’Aria at Milan.

Manzolini Libellula II

The Libellula II used a higher powered 105hp Walter Minor 4-III engine and had an enclosed cockpit. This aircraft, I-MANZ, gained an RAI type certificate on October 15, 1962, but no manufacture was undertaken.

Libellula II
Engine: Walter Minor III, 78kW
Main rotor diameter: 9.0m
Fuselage length: 4.75m
Height: 3.30m
Max take-off weight: 650kg
Empty weight: 500kg
Max speed: 109km/h
Hovering ceiling: 1250m
Range: 200km

Manzolini Libellula

Proposed final version

The Libellula was the brainchild of Count Ettore Manzolini. With an open framework fuselage and fixed skid undercarriage, Manzolini devised a coaxial rotor system for the Libellula and flew his ‘stripped’ prototype on 7 January 1952.

A mock-up of a proposed final version was prepared.

Engine: Hirth 105 hp
Rotors: 2 x 2-blade co-axial
Rotor diameter: 26 ft
Loaded weight: 1,430 lb
Cruising speed: 65 mph
Seats: 1