Volmer VJ-24 SunFun

VJ-24E

The VJ-24 is Volmer Jensen’s hang glider design built from aluminum. This motorglider is constructed of aluminum tubing plus fabric, and originated as a foot-launched glider. SunFun is made from pop riveted aircraft aluminium with the wings leading edge formed in styrene foam. Covering is polyester aircraft fabric doped. Control is by aileron, elevator and rudder. A permanent seat is built into the hanger structure.

Volmer VJ-24 SunFun Article

The VJ-24 was first flown in about 1975 and showed excellent controllability with a joystick. Plans were available from Volmer Aircraft for $100.00. Materials have been estimated at $2400, with a building time of 250 hours.

The VJ-24 uses pip pins and thumb screws to assemble in 10 minutes without tools.

Designated the VJ-24E, the Sunfun is essentially a simplified version of the Swingwing hang glider or powered hang glider. The wings are fabric-covered aluminum tube and are a rectangular-planform type braced by V struts. The two wheels are for ground handling only, so the Sunfun is foot-launched and foot-landed. A 10-hp engine and fuel tank are installed beneath the wing and behind the pilot so that takeoff can be performed without benefit of a steep hill. Wingspan is 36 feet 6 inches, and total weight is 110 pounds. The Volmer VJ 24E Sunfun has a useful load of about 200 pounds, burns about 1.5USG per hour.

A minimum powered glider, the VJ-24W is a modified version of VJ-24E Sun Fun hang glider with wheeled landing gear, tractor engine, independent rudder control, manufactured by Airway Aircraft Inc., 905 Airway Ave., Glendale, CA 91201, USA.

Fairing behind pilot cuts drag. Independent three-axis controls. Construction is all metal with Dacron cover. Yamaha KT100 or McCulloch 101 engine. Two main wire wheels, tail skid undercarriage.

Gallery

VJ-24
Wingspan: 36 ft
Wing chord: 4 ft 6 in
Wing area: 160 sq.ft
Empty weight: 110 lb
Speed range: 18-25 mph

VJ-24
Speed max: 40 mph
Cruise: 30 mph
Range: 30 sm
Stall: 17 mph
ROC: 350 fpm
Take-off dist: 100 ft
Landing dist: 100 ft
Engine: Yamaha, 15 hp
Fuel cap: 1.5 USG
Weight empty: 210 lbs
Gross: 410 lbs
Height: 5.75 ft
Length: 198.5 ft
Wing span: 36 ft
Wing area: 163 sq.ft
Seats: 1
Landing gear: tail wheel

VJ-24W Sun Fun
Wing span: 36.5 feet
Wing area: 163 square feet
Empty weight: 165 pounds
Max gross weight: 345
Engine: Yamaha KT-100, 97.6cc, 15 hp.
Reduction unit: 2,75:1
Prop: 57 in
Wingspan: 36 ft
Wing area: 160sq.ft
Aspect ratio: 8:1
Length 18’
Empty weight 200 lbs
Payload 200 lbs
Gross weight 400 lbs
Wing loading 2.5 lbs/sq.ft
L/D 10:1
Cruise speed 30mph
Stall speed 18mph
Vmax 40 mph
Takeoff run 100’
Landing roll 100’
Climb Rate 350 fpm
Fuel Capacity 1.5 USG

Chord length: 4.5 ft
Wing span: 36.5 ft
Wing area: 163 sq,ft
Aspect ratio: 6.75
Weight: 110 lb
Pilot weight: 160-200 lb
Takeoff speed: 13 mph
Stall speed: 15 mph
Max speed: 30 mph
Best glide ratio (L/D): 9.5
Best L/D speed: 17 mph
Min sink: 158 fpm

Volmer VJ22 Sportsman

The Volmer VJ-22 Sportsman (or Chubasco) is a two-place, side by side, closed cabin, highwing monoplane, amphibious flying boat. Designed by Mr. Volmer Jensen, the Sportsman first flew on 22 December 1958 as an original design based on an earlier aircraft, the VJ-21, a high-wing pusher that contributed much data for the Sportsman.

Volmer VJ22 Sportsman Article

Construction of the original Sportsman started in September 1957 and was completed in December 1958. The rigid, corrosion proof hull is made of 1/16 inch and 3/32 inch aircraft mahogany plywood with 1/4 inch plywood at the step for maximum strength and covered with fiberglass for added protection. The fin is built integral with the hull. The Sportsman can use fabric-covered Aeronca Chief or Champion wings. The wing panels are identical to those of the Aeronca Chief and consist of front and rear solid spruce spars, aluminium ribs, steel tube compression members and internal wire bracing. Each panel is externally braced by steel tube V struts to the fuselage. Floats are attached, and are braced to the outboard end of each wing. The main undercarriage retracts by swinging forward 90o. Shock absorption is by means of rubber bungee cord. The tailwheel incorporates a water rudder, and retracts upwards when not required. The pusher engine is mounted on a steel tube structure above the wing. To facilitate storage, the wings may be removed by undoing the few retaining bolts.

Numerous testing from calm water to five foot swells in the open sea have proven the design to be both extremely airworthy and seaworthy. Wings are wood spar and ribs, fabric covered. It takes off from water at sea level in about 20 seconds. The VJ-22 is powered by a Continental C-85, starter and gen. It has a cruising speed of 85 mph and stalls at 45 mph.

Suited to Continental s from the C85 to the O-200, most VJ-22 have their pylon-mounted engine mounted as a pusher, but one built by Viv Bellamy, G-BAME c/n VHB-1, started in 1971 and first flown from St. Just in early 1974, had a tractor engine. Possibly a Lawrence or Salmson radial.

Viv Bellamy’s G-BAME

Designed to use wings from light aircraft including Auster, Aeronca, and Taylorcraft, In the UK, G-BAHP completed at Rollasons at Croydon by September 1972 featured Aeronca 7AC G-ATXC wings. It was first flown at Biggin Hill in 1973 with a Continental C90 engine.

Engine: Continental, 85 hp
HP range: 85-100
Speed max: 110 mph
Cruise: 80 mph
Range: 225 sm
Stall: 45 mph
ROC: 550 fpm
Take-off dist: (land) 350 ft., (water) 1000 ft
Landing dist: (land) 500 ft., (water) 1000 ft
Service ceiling: 12,000 ft
Fuel cap: 20 USG
Weight empty: 1000 lb
Gross: 1500 lb
Height: 8 ft
Length: 24 ft
Wing span: 36.5 ft
Wing area: 180 sq.ft
Seats: 2
Landing gear: tail wheel, retractable
Takeoff time 20 sec

Engine: 100 hp
ROC: 600 fpm
Span: 36 ft 6 in
Length: 24 ft
Empty wt: 1000 lb
Max wt: 1500 lb

Vol Mediterrani VM-1 Esqual / Esqual Aerocomp AB VM-1

The VM-1 Esqual is a two seat light plane manufactured in composite with high density PVC foam and Epoxy resins. Laminated in a mould and vacuum cured in an oven at constant controlled temperature and humidity.

The fuselage is monocoque. The safety reinforced cockpit has twin axle composite beams all around its frame. The low cantilever wing has positive changing flaps (as high lift devices). The wing structure has a composite sandwich skin with a main double “T” composite spar and an accessory spar near the trailing edge.

Vol Mediterrani VM-1 Esqual

The cockpit seats are side by side. The rudder pedals are adjustable in flight. Electric operated flap and mechanical trim are standard, electric trim is an option. Independent ventilation openings are standard, a cabin heater is an option. The luggage compartment (with 50lts capacity) is located behind the seats and can be accessed during flight.

Vol Mediterrani VM-1 Esqual

The landing gear of the Esqual has a classic tricycle gear which is made of 7175 T6 aluminium grade. The main gear legs are suspended in the main carry through beam together with the reinforced wing spar zone. The main wheels are equipped with independent hydraulic brakes for steering. The nose gear leg is supported in the engine mount and equipped with a free swivel nose wheel.

2009 Price: 75000 EURO

Engine: Rotax 912 ULS (100 HP)
Wing span: 9.10 m
Wing area: 9,0 m²
Length 6.08 m
Height 1.94 m
Empty Weight: 265 kg / 584 lbs
Maximum weight: 544 Kg
Fuel capacity: 2 x 50 lts
VNE: 173 kt / 199 mph / 320 kmh
Stall: 33 kt / 39 mph / 62 kmh
Cruise: 135 kt / 155 mph / 250 kmh
Climb Rate: 1800 ft/min / 9 m/s
Glide Ratio: 1:19
Take-off distance (50ft obstacle): 450 ft / 138 m
Landing distance (50ft obstacle): 660 ft / 200 m
Roll rate (45/45º) 2 sec
Cockpit width 110 cm

Volkswagen E-motor / Type 1 / Type 4

The Volkswagen air-cooled engine is an air-cooled boxer engine with four horizontally opposed cast iron cylinders, cast aluminum alloy cylinder heads and pistons, magnesium crankcase, and forged steel crankshaft and connecting rods.

Variations of the engine were produced by Volkswagen plants worldwide from 1936 until 2006 for use in Volkswagen’s own vehicles, notably the Type 1 (Beetle), Type 2 (bus, transporter), Type 3, and Type 4. Additionally, the engines were widely used in industrial, light aircraft and kit car applications.

Like the Volkswagen Beetle, the first Volkswagen Transporters (bus) used the Volkswagen air-cooled engine, a 1.1 litre, DIN-rated 18 kW (24 PS, 24 bhp), air-cooled four-cylinder “boxer” engine mounted in the rear. The 22 kilowatt (29 PS; 29 bhp) version became standard in 1955, while an unusual early version of the engine which developed 25 kilowatts (34 PS; 34 bhp) debuted exclusively on the Volkswagen Type 2 (T1) in 1959. Since the 1959 engine was totally discontinued at the outset, no parts were ever made available.

The second-generation Transporter, the Volkswagen Type 2 (T2) employed a slightly larger version of the engine with 1.6 litres and 35 kilowatts (48 PS; 47 bhp).

A “T2b” Type 2 was introduced by way of gradual change over three years. The 1971 Type 2 featured a new, 1.6-litre engine, now with dual intake ports on each cylinder head, and was DIN-rated at 37 kilowatts (50 PS; 50 bhp).

The Volkswagen Type 3 (saloon/sedan, notch-back, fastback) was initially equipped with a 1.5-litre engine, displacing 1,493 cubic centimetres (91.1 cu in), based on the air-cooled flat-4 found in the Type 1. While the long block remained the same as the Type 1, the engine cooling was redesigned reducing the height of the engine profile, allowing greater cargo volume, and earning the nicknames of “Pancake” or “Suitcase” engine. This engine’s displacement would later increase to 1.6 litres.

Originally a single- or dual-carburetor 1.5-litre engine (1500N, 33 kilowatts (45 PS; 44 bhp) or 1500S, 40 kilowatts (54 PS; 54 bhp)), the Type 3 engine received a larger displacement (1.6 litre) and modified in 1968 to include Bosch D-Jetronic electronic fuel injection as an option, making it the first mass production consumer cars with such a feature (some sports/luxury cars with limited production runs previously had fuel injection).

In 1968, Volkswagen introduced a new vehicle, the Volkswagen Type 4. The model 411, and later the model 412, offered many new features to the Volkswagen lineup.

While the Type 4 was discontinued in 1974 when sales dropped, its engine became the power plant for Volkswagen Type 2s produced from 1972 to 1979: it continued in modified form in the later Vanagon which was air-cooled from 1980 until mid-1983.

The engine that superseded the Type 4 engine in late 1983 retained Volkswagen Type 1 architecture, yet featured water-cooled cylinder heads and cylinder jackets. The wasserboxer, Volkswagen terminology for a water-cooled, opposed-cylinder (flat or ‘boxer engine’) was subsequently discontinued in 1992 with the introduction of the Eurovan.

The Type 4 engine was also used on the Volkswagen version of the Porsche 914. Volkswagen versions originally came with an 80 horsepower (60 kW) fuel-injected 1.7-litre flat-4 engine based on the Volkswagen air-cooled engine. In Europe, the four-cylinder cars were sold as Volkswagen-Porsches, at Volkswagen dealerships.

Porsche discontinued the 914/6 variant in 1972 after production of 3,351 units; its place in the lineup was filled by a variant powered by a new 95 metric horsepower (70 kW; 94 bhp) 2.0-litre fuel-injected version of Volkswagen’s Type 4 engine in 1973. For 1974, the 1.7-litre engine was replaced by a 76 metric horsepower (56 kW; 75 bhp) 1.8-litre, and the new Bosch L-Jetronic fuel injection system was added to American units to help with emissions control. 914 production ended in 1976. The 2.0-litre engine continued to be used in the Porsche 912E, which provided an entry-level model until the Porsche 924 was introduced.

For the Volkswagen Type 2, 1972’s most prominent change was a bigger engine compartment to fit the larger 1.7- to 2.0-litre engines from the Volkswagen Type 4, and a redesigned rear end which eliminated the removable rear apron. The air inlets were also enlarged to accommodate the increased cooling air needs of the larger engines.

This all-new, larger engine is commonly called the Type 4 engine as opposed to the previous Type 1 engine first introduced in the Type 1 Beetle. This engine was called “Type 4” because it was originally designed for the Type 4 (411 and 412) automobiles. There is no “Type 2 engine” or “Type 3 engine”, because those vehicles did not feature new engine designs when introduced. They used the “Type 1” engine from the Beetle with minor modifications such as rear mount provisions and different cooling shroud arrangements, although the Type 3 did introduce fuel injection on the “Type 1” engine.[citation needed]

In the Type 2, the Volkswagen Type 4 engine was an option from 1972. This engine was standard in models destined for the US and Canada. Only with the Type 4 engine did an automatic transmission become available for the first time in 1973. Both engines displaced 1.7 litres, rated at 66 metric horsepower (49 kW; 65 bhp) with the manual transmission, and 62 metric horsepower (46 kW; 61 bhp) with the automatic. The Type 4 engine was enlarged to 1.8 litres and 68 metric horsepower (50 kW; 67 bhp) in 1974, and again to 2.0 litres and 70 metric horsepower (51 kW; 69 bhp) in 1976. As with all Transporter engines, the focus in development was not on motive power, but on low-end torque. The Type 4 engines were considerably more robust and durable than the Type 1 engines, particularly in Transporter service.

During the 1970s, in Brazil, Volkswagen made available the 1700 cc engine for its regular production car SP-2. The 1700 cc engine was identical to the 1600 cc version, but with enlarged cylinder bores.

Volkswagen AG has officially offered these air-cooled boxer engines for use in industrial applications since 1950, lately under its Volkswagen Industrial Motor brand. Available in 18 kilowatts (24 PS; 24 bhp), 22 kilowatts (30 PS; 30 bhp), 25 kilowatts (34 PS; 34 bhp), 31 kilowatts (42 PS; 42 bhp), 33 kilowatts (45 PS; 44 bhp) and 46 kilowatts (63 PS; 62 bhp) outputs, from displacements of 1.2 litres (73 cu in) to 1.8 litres (110 cu in), these Industrial air-cooled engines were officially discontinued in 1991.

The air-cooled opposed four-cylinder Beetle engines have been used as an experimental aircraft engine. This type of Beetle engine deployment started in the 1960s. A number of companies produced aero engines that are Volkswagen Beetle engine derivatives: Limbach, Hapi, Revmaster, the AeroConversions AeroVee Engine, and others. The VW air-cooled engine does not require a heavy gear reduction unit to utilize a propeller at cruise RPM. With its relative low cost and parts availability, many kit planes or plans built experimental aircraft are designed around the VW engines.

Formula V Air Racing uses aircraft designed to get maximum performance out of a VW powered aircraft resulting in race speeds above 160 mph.

Some aircraft that use the VW engine are:

Airdrome Bleriot Model XI
Airdrome Dream Fantasy Twin
Airdrome Fokker DR-1
Airdrome Fokker D-VI
Airdrome Fokker D-VII
Airdrome Fokker D-VIII
Airdrome Nieuport 11
Airdrome Nieuport 24
Airdrome Taube
AirLony Skylane
Airmotive EOS 001
Akaflieg München Mü23 Saurier
Aurore MB 04 Souris Bulle
Bensen B-8
BK Fliers BK-1
Bounsall Super Prospector
Boyd G.B.1
Bradley Aerobat
Circa Reproductions Nieuport 11
Circa Reproductions Nieuport 17
Corby Starlet
Denney Kitfox
Druine Turbulent
Evans VP-1 Volksplane
Evans VP-2 Volksplane
Falconar F9A
Falconar F11 Sporty
Fisher Avenger V
Fisher Youngster
Flaglor Sky Scooter
Flitzer Z-21
Great Plains Easy Eagle
Harmon Der Donnerschlag
Harmon Mister America
Hummel H5
Hummel Ultracruiser Plus
JDT Hi-MAX
JPM 01 Médoc
Junqua Ibis
Just Superstol
Mignet Pou-du-Ciel
Mini-Hawk Tiger-Hawk
JDT V-MAX
Kolb M3X
Leger Pataplume 1
Light Miniature Aircraft LM-5
Milholland Legal Eagle – half VW and full Type 1 VW engines
Mini Coupe
Monnett Sonerai
Nicollier Menestrel
Parker Jeanie’s Teenie
Pazmany PL-4A
Pober Pixie
Preceptor STOL King
Preceptor Ultra Pup
Preceptor Stinger
RagWing RW1 Ultra-Piet – half VW and full Type 1 VW engines
RagWing RW7 Duster – half VW and full Type 1 VW engines
Rand Robinson KR-1
Rand Robinson KR-2S
Rutan Quickie
Sisler SF-2A Cygnet
Sonex Aircraft Onex
Sonex Aircraft Sonex
Southern Aeronautical Renegade
Southern Aeronautical Scamp
Stewart Headwind
Stolp SA-500 Starlet
Taiwan Dancer TD-3
Taylor Monoplane
Thatcher CX4
Vidor Champion V
Viking Dragonfly
Zenair CH 100

Half VW
For aircraft use a number of experimenters seeking a small two-cylinder four-stroke engine began cutting Type 1 VW engine blocks in half, creating a two-cylinder, horizontally opposed engine. The resulting engine produces 30 to 38 hp (22 to 28 kW). Plans and kits have been made available for these conversions.

One such conversion is the Carr Twin, designed by Dave Carr, introduced in January, 1975, in the Experimental Aircraft Association’s Sport Aviation magazine. The design won the John Livingston Award for its outstanding contribution to low cost flying and also was awarded the Stan Dzik Memorial Award for outstanding design.

Another example is the Total Engine Concepts MM CB-40.

Some aircraft that use the Half VW engine are:

Belite Ultra Cub
Duane’s Hangar Ultrababy
Hummel Bird
Hummel Ultracruiser
Milholland Legal Eagle – half VW and full Type 1 VW engines
Pop’s Props Pinocchio
RagWing RW1 Ultra-Piet – half VW and full Type 1 VW engines
RagWing RW4 Midwing Sport
RagWing RW7 Duster – half VW and full Type 1 VW engines
Spacek SD-1 Minisport
Ultravia Pelican

Specifications:
Type 1

Volkswagen 1100 engine
Production 1945–1953
Displacement 1,131 cc (69.0 cu in)
Cylinder bore 75 mm (2.95 in)
Piston stroke 64 mm (2.52 in)
Compression ratio 5.8:1
Power output 18 kW (24 PS; 24 bhp) @ 3,300 rpm,
22 kW (30 PS; 30 bhp)
Specific power 15.9 kW (22 PS; 21 bhp) / L (18kW variant)
Torque output 68 N·m (50 lbf·ft) @ 2,000 rpm

Volkswagen 1200 engine
Production 1950–1991
Displacement 1,192 cc (72.7 cu in)
Cylinder bore 77 mm (3.03 in)
Piston stroke 64 mm (2.52 in)
Compression ratio 6.1:1 – 7.0:1
Power output 22 kW (30 PS; 30 bhp)
25 kW (34 PS; 34 bhp)
27 kW (37 PS; 36 bhp)
30 kW (41 PS; 40 bhp)
Specific power 18.5–21.0 kW (25–29 PS; 25–28 bhp) / L

Volkswagen 1300 engine
Production 1966–1995

Volkswagen 1500 engine
Production 1961–1971
Displacement 1,493 cc (91.1 cu in)
Cylinder bore 83 mm (3.27 in)
Piston stroke 69 mm (2.72 in)
Power output 1500N: 33 kW (45 PS; 44 bhp),
1500S: 40 kW (54 PS; 54 bhp)
Specific power 22.1–26.8 kW (30–36 PS; 30–36 bhp) / L

Volkswagen 1600 engine
Displacement 1592cc
Cylinder bore 85.5mm
Fuel system initially: 30/31-Pict Carburetor for single port 34-Pict Carburetor for dual port,
later: Bosch L-Jetronic electronic fuel injection
Power output single port: 35 kW (48 PS; 47 bhp)
dual port: 37 kW (50 PS; 50 bhp)

Volkswagen Type 4 engine
Production 1968–1983

Volkswagen 1700 engine
Displacement 1,679 cc (102.5 cu in)
Compression ratio 7.8:1
Power output 76 PS (56 kW) @ 5,000 rpm
Torque output 127 N·m (94 lbf·ft) @ 3,500 rpm

Volkswagen 1800 engine
Power output 50 kW (68 PS; 67 bhp)

Volkswagen 2000 engine
Power output 52 kW (71 PS; 70 bhp)

Voliamo S. Franscesco

S. Franscesco 3

The S. Franscesco side by side two seater has a spaceframe fuselage and fabric covered wooden wings.

The prototype first flew in 1976.

S. Franscesco 3
Engine: Limbach, 80 hp
Wing span: 9.7 m
Wing area: 12 sq.m
MAUW: 450 kg
Empty weight: 280 kg
Fuel capacity: 50 lt
Max speed: 170 kph
Cruise speed: 140 kph
Minimum speed: 60 kph
Climb rate: 3 m/s
Seats: 2
Fuel consumption: 10 lt/hr

Volante Aircraft Co Volante

The ultimate goal of the Volante flying car program was to prove to the aviation community and to the public, by actual demonstration, that the flying car, properly designed, can bring revolutionary new capabilities to a transportation system.

The conversion process, aircraft to car and trailer and back, be very simply carried out in a very short time. They set 10 to 12 minutes as a goal. All flying cars require some conversion, and 12 minutes is a good trade for a lightweight, unencumbered car.

Aircraft
Engine: 180 hp
Wingspan: 27 ft
Length: 20 ft
Height: 7 ft
Empty weight: 1300 lb
Gross weight: 2000 lb
Baggage: 7.6 cu.ft
Cruise speed: 157 mph
Stall: 65 mph
Max range: 650 mi
TO dist: 700 ft

Car
Width: 5 ft 6 in
Height: 4 ft
Length: 13 ft 5 in
Empty weight: 640 lb
Gross weight: 1200 lb

Voisin Canard

March 1911

The Voisin Canard was an aircraft developed by Voisin brothers during 1910 and first flown early in 1911. It was originally flown as a landplane: with the addition of floats it became one of the first seaplanes used by the French Navy.

3 February 1911

As first flown at Issy-les-Moulineaux by Maurice Colliex, the aircraft had an uncovered fuselage of wire-braced wood construction with the 50 hp (37 kW) Rossel-Peugeot rotary engine at the rear and the front-mounted control surfaces consisting of an all-moving elevator divided into two halves, one either side of the fuselage, a rectangular balanced rudder mounted above the elevator, and a pair of short-span fixed horizontal surfaces with a high angle of attack mounted behind and below the elevators. Voisin’s characteristic side-curtains were fitted to the outermost pair of interplane struts and roll control was achieved using trailing-edge ailerons on both upper and lower wings.

Voisin Canard floatplane being tested on the Seine, 3 August 1911

The aircraft was judged a success and Voisin manufactured a number of examples. There are variations between the individual production aircraft: the two examples flown in the French military aircraft trials in 1911 had a wingspan of 15 m (49 ft 3 in).; one was powered by a 56 kW (75 hp) Renault and the second by a 97 kW (130 hp) Gnome. The number of sets of side curtains varied, some aircraft having two or even three sets.

The seaplane variant, fitted with floats designed by Henri Fabre, was initially built to the order of Prince Bibesco, who intended to use it make a flight across the Black Sea. It was first successfully flown from water on 25 April 1911.

One example was bought by the French navy in March 1912 to equip the seaplane tender La Foudre, the first seaplane carrier in history. A second example was delivered to the Navy in December 1913.

47 of the 1911 Voisin Canard (amphibian) were built.

1911 Voisin 17m canard biplane

Powerplant: 1 × Gnome, 52 kW (70 hp)
Wingspan: 12 m (40 ft)
Wing area: 43.9 m2 (473 sq ft)
Length: 7.9 m (26 ft)
Gross weight: 549 kg (1,210 lb)
Maximum speed: 90 km/h (56 mph, 49 kn)
Seats: 2

1911 Voisin Canard (amphibian)
Span: 36’1″
Speed: 47 mph

1911 Voisin 17m canard biplane
Span: 55’9″
Length: 37’9″
Weight: 2140 lb empty

Voisin-Farman II

Farman’s First Biplane at Issy-les-Moulineaux returning to the Hangar after a Flight

During 1908, the Voisin brothers built for Farman another aircraft, to be called the Farman II, incorporating refinements in the design based on Farman’s specifications. After the break in his association with Voisin in early 1909, Henry Farman started aircraft construction for himself.

Voisin Zodiac

Voisin flying his Zodiac aeroplane

Originally, George White of Bristol Aeroplanes wanted to build licensed copies of the Zodiac biplane designed by Gabriel Voisin, after one was bought by White to show at the 1910 London Aero Meet.
After taking the Zodiac to Brooklands airfield for tests, no one could get the plane of the ground—perhaps due to an under-powered engine to plane weight ratio, and the shallow camber of the wing section—a fact commented on by the pioneering aviation magazine, Flight.

To compensate for the wing problem, White and company added a different set… but still… a weak motor is a weak motor.

On May 28, 1910, pilot Maurice Edmond was able to achieve a short flight, but on June 10, 1910, an accident that damaged its undercarriage had the frustrated crew give up on the Zodiac… even with five other such copies being built by the British and Colonial Aeroplane Company at its headquarters at Filton.