Lobert Ganagobie / Mousebird

Of all wood construction the first Gangobie was designed and built by two brothers, William and James Lobet, in 1953. The result of intensive wind tunnel testing, the prototype got airborne behind a l6hp Clerget engine. Since built in small numbers in North America, and achieved kitset production status as a peanut scale 13” wing span balsa model.

Grounded after 30 hours of flight time by the failure of the nearly 50 year old engine, the Ganagobie concept was given a new lease of life by a Canadian engineer, Mr George Jacquemin. Mr Jacquemin, an aerospace engineer with Lockheed in California, suggested the modification of the design to accommodate the large numbers of war surplus target drone engines available in the mid fifties. The fuselage was given a boost in size to fit a larger framed pilot and a second prototype begun in Toronto, Canada, by an Experimental Aircraft Chapter. Completed by a Mr Pierre Descamps, the American Ganagobie was engined by a 1934 French-built Poinsard 35hp flat four. A subsequent flight report by De Havilland Canada’s chief test pilot gave the design a boost and some ten Ganagobie 03 projects were begun, largely in the United States and Canada. The original Canadian built Ganagobie was later re-engined with a Volkswagen 1200cc engine, standard fare for a number of homebuilts, and led to the latest in the family, the Lobet Ganagobie 05. The one and only Ganagobie 05, begun in Australia in 1974 after James Lobet migrated there, was shipped to New Zealand in 1982.

Gallery

Engine: Citroën AMI8
Wingspan: 24.03 ft
Length: 16.01 ft
Cruise: 169 kph (100 mph)
Stall: 75 kph (47 mph)
ROC: 5m/sec (1,000 fpm).

LJaM 1912 Monoplane

Jerzy Jankowski, Maximilian von Lerche and Francesco Mosca built at workshops of Moscov Aeronautical Society and airplane modeled after Bleriot aircraft with 50hp Gnome engine. It was apparently very well designed and built aircraft that made numerous succesful flights, including one on 14th of May 1912 when Jankowski broke on it Russian flight altitude record of 1775m;

Liverpool University MPAG Liverpuffin

The Liverpool University MPAG bought the remains of Hatfield’s Puffin II in September 1969 and set about a redesign using the main wing structure and thr propellor from the Hatfield project.

The basic layout is a high wing aircraft with a pod-and-boom format fuselage. The wing is of metal structure with expanded polystyrene used to form the leading and trailing edge ribs and cross-pieces. Covering is of ‘Mellinex’. The wing is cranked upwards about mid-span. A conventional tail (tailplane and elevators, fin and rudder) is mounted on the end of a boom projecting from the lower half of the rear fuselage. The pilot is located in the extreme nose, in a totally enclosed canopy. A pusher propellor is mounted aft of the wing, above the boom. Single wheel undercarriage.

First flight was made at RAF Woodvale on 18 March 1972. It then went to Dulles Airport, Washington, USA, where it was exhibited at ‘Transpo 72’.

It is not thought to have flown much since its return, if at all,

Wingspan: 64.00 ft
Wing area: 305 sq.ft
Aspect ratio: 13:1
Empty weight: 140 lb

Littner Whiskey IV / Asso Aerei Whiskey IV

The Whisky IV is a tandem two seat, low wing aircraft designed by Giuseppe Vidor. Construction materials are wood & fabric. The landing gear is a fixed tailwheel configuration.
2009 Complete set of plans $400 (US$)

Engine: Limbach 2000, 80 hp
HP range: 75-100
Wing Span: 26.25 ft.
Wing Area: 120.5 sq. ft.
Length: 21 ft.
Height: 7 ft.
Cockpit Width: 28.3 in.
Aspect Ratio: 5.7
Dihedral Angle: 4°
Wash Out: 1.50°
Empty Weight: 622 lbs.
Gross Weight: 1058 lbs.
Wing Loading: 8.78 lbs./sq. ft.
Power Loading: 13.22 lbs./HP
C.G. Travel: 18.3 to 31% MAC
Fuel Capacity: 13.2 gal. / 79 lbs.
V.N.E: 175 mph.
Max Horizontal Speed: 160 mph.
Cruise 75% Power: 130 mph.
Max Maneuvering Speed: 115 mph.
Max Flap Speed: 84 mph.
Stall Speed Flaps Down: 37 mph.
Stall Speed Flaps Up: 43 mph.
Take-Off Distance: (Solo) 330 ft.
Landing Distance: (Solo) 490 ft.
Fuel Burn 75% Power: 3.17 gal./hr.
Max Range 75% Power: 535 nm
Rate Of Climb: 785 ft./min.
Service ceiling: 12,000 ft
Seats: 2 tandem
Landing gear: retractable tailwheel