
The 1873 Renard Decaplan 10-wing glider had twin skid gear and an aileron at the centre point on each side of the fuselage.
Gliding was reportedly “suitable: but only in a spiral.

The 1873 Renard Decaplan 10-wing glider had twin skid gear and an aileron at the centre point on each side of the fuselage.
Gliding was reportedly “suitable: but only in a spiral.

Remos of Germany continued in 2012 with three models of its GX line: the GX AVIATOR II, GXnES and GX eLite. A variety of standard features and options include Garmin aera 510 and GPSMAP696, Dynon SkyView EFIS, Dynon D100 and D120 EFIS and much more. 2012 prices range from $120,000 to $145,000, with many options.
GX
Engine: Rotax 912S, 100 hp
Propeller: Sensenich
Gross weight: 1320 lb
Empty weight, std: 670 lb
Useful load, std: 650 lb
Payload, full std. fuel: 518 lb
Fuel capacity: 22 lb
Wingspan: 30 ft. 6 in.
Overall length: 21 ft. 3 in.
Overall height: 7 ft. 5 in.
Wing area: 118 sq. ft
Wing loading: 11.2 lbs./sq. ft
Power loading: 13.2 lbs./hp
Seating capacity: 2
Cabin width: 46.8 in
Vso: 38 kt
Vne: 134 kt
Cruise speed: 113 kt
Max rate of climb: 1050 fpm
Takeoff over 50 ft. obstacle: 730 ft
Landing over 50 ft. obstacle: 760 ft

Stall: 34 kt / 39 mph / 63 kmh
Cruise: 124 kt / 143 mph / 230 kmh
VNE: 151 kt / 174 mph / 280 kmh
Empty Weight: 290 kg / 639 lbs
MTOW Weight: 472 kg / 1041 lbs
Climb Ratio: 1300 ft/min / 6.5 m/s
Glide Ratio: 17:1
Take-off distance (50ft obstacle): 450 ft / 137 m
Landing distance (50ft obstacle): 480 ft / 146 m

The Remos G3 is an FAA approved, German manufactured Light Sport Aircraft. Made mostly of carbon fibre, including the landing gear, the Remos weighs 626 lb empty, leaving a useful load of 695 lb. The cockpit is reinforced with Kevlar. Structural composite wing parts are covered with Ceconite fabric to reduce weight. The strutted wings fold back in 5 minutes.
The Remos G3 is approved to tow gliders up to 625 lb gross and banners up to 1633 sq.ft.
Ailerons and elevator are mass balanced, and there is some rudder surface forward of the hinge. Aileron differential is about 1.5:1. Electric trim and flaps are fitted. Flaps extend to 40 degrees. The fuel tank is high in the aft fuselage. Shoulder width in the cabin is 45.8 in. Doors, which are hinged on top, may be opened in flight to 66 kt. They can be removed before flight.
First flown in 1997, the Remos was introduced in 1998 and proclaimed Aircraft of the year at the biennial AERO sport aviation show in Friedrichshafen, Germany, in 2000.

1998
2007 base price: US$99,500

Remos G-3 LSA
Engine: Rotax 912 ULS, 100 hp
TBO: 1500 hr
Prop: 2 blade wood
Fuel type: 100/100LL & auto
Wingspan: 32 ft. 4 in
Overall length: 21 ft. 5 in
Height: 5 ft. 6 in
Wing area: 131 sq. ft
Wing loading: 10.1 lbs./sq. ft
Power loading: 13.2 lbs./hp
Max ramp weight: 1320 lb
Gross weight: 1320 lb
Landing weight: 1320 lb
Empty weight, std: 625 lb
Useful load, std: 695 lb
Payload, full std. fuel: 578 lb
Useful fuel, std: 21 USgals
Seating capacity: 2
Cabin doors: 2
Cabin width: 47 in
VNE: 121 kt / 140 mph / 225 kmh
Cruise speed: 75% power: 113 kt
Vso: 39 kt
Best rate of climb (SL): 1300 fpm / 6.5 m/s
Max operating altitude: 20,000 ft
Takeoff ground roll: 330 ft
Landing ground roll: 590 ft
Take-off distance (50ft obstacle): 450 ft / 137 m
Landing distance (50ft obstacle): 450 ft / 137 m
Engine: Rotax 912, 80 hp
Empty weight: 260 kg
Wing span: 9.8 m
Wing area: 13.31 sq.m
MAUW: 450 kg
Fuel capacity: 60 lt
Max speed: 145 kph
Cruise speed: 140 kph
Minimum speed: 62 kph
Climb rate: 5.8 m/s
Certification: Allemande
Seats: 2
Fuel consumption: 9.5 lt/hr
Price (1998): 114 000 DM
Two-seat monoplanes
U.S. version of Gemini Ultra is Micro-Viper, distributed by Akro-Viper Inc.
Established 1987. Has produced the Gemini and Gemini Ultra two-seat monoplanes, now only built to order, and markets the G-3 Mirage as a composites-built, very light high-wing monoplane (first flown 1997). U.S. version of Gemini Ultra is Micro-Viper, distributed by Akro-Viper Inc.
1998:
Waldweg 1
D-85283 Eschelbach
Germany
2005: Bavaria, Germany.
Remington-Burnelli was producing in 1924 the BR-2 Freighter, an all-metal biplane freighter designed specifically for cargo carrying. Typical of Junkers-inspired design, it combined the Burnelli lifting fuselage with corrugated light alloy skins.
USA
Was producing in 1924 the BR-2 Freighter, an all-metal biplane freighter designed specifically for cargo carrying. Typical of Junkers-inspired design, it combined the Burnelli lifting fuselage with corrugated light alloy skins.
Netherlands
Company formed with intention of restarting production of the Fokker 50 and 100, having bought tooling and rented the production factory in 1998.

Prof. Dr. Hans Reißner built this canard in the experimental workshop of Junkers that was connected to the “Technische Hochschule Aachen”.
First flying on 23 May, 1912, in second form after having been rebuilt (in the third form, it got four fins under the mainplane).
According to G. Schmitt several versions were built and also flown. The Swiss Robert Gesell presented the machine over a few weeks in Johannisthal at the end of 1912.