Seedwings Europe Kestrel

A 2000 hang glider.

Kestrel 133
Wing area: 12.5 m²
Wing span: 9.9 m
Hang glider weight: 27 kg
Minimum pilot weight: 50 kg
Maximum pilot weight: 70 kg
Minimum speed: 32 km/h
Number of battens: 21
Nose angle: 127°

Kestrel 148
Wing area: 13.85 m²
Wing span: 10.2 m
Hang glider weight: 28 kg
Minimum pilot weight: 65 kg
Maximum pilot weight: 80 kg
Minimum speed: 32 km/h
Number of battens: 21
Nose angle: 127°

Kestrel 158
Wing area: 14.6 m²
Wing span: 10.4 m
Hang glider weight: 30 kg
Minimum pilot weight: 75 kg
Maximum pilot weight: 105 kg
Minimum speed: 29 km/h
Number of battens: 27
Nose angle: 127°

Seedwings Europe Crossover

A 2010 hang glider the Crossover 15 aerotowed well with light pitch making it easy to keep station behind the tug. It also had very good directional stability on tow. In flight it was a bit stiff in roll and the light pitch made it a bit less harmonized in the two axises than other gliders. It landed quite fast.

Crossover 14
Wing area: 9.9 m²
Aspect ratio: 7
Hang glider weight: 28 kg
Minimum pilot weight: 80 kg
Maximum pilot weight: 120 kg
Packed length: 4.90 m
Packed length short: 3.45 m

Crossover 15
Wing area: 10.1 m²
Aspect ratio: 6.8
Hang glider weight: 29 kg
Minimum pilot weight: 55 kg
Maximum pilot weight: 80 kg
Packed length: 5.10 m
Packed length short: 3.60 m

Seedwings Europe Space

The 2007 Seedwings Europe Space for Intermediate pilots is a curved tip 75% double surface glider with mylar leading edge and aerofoil uprights. Equipped with VG. It has 12 slats of extrados and 2 slats of intrados. 3 inner velcros keep the profile at high speeds.

Very easy handling. DHV rated almost like a training glider but with 80% double surface and VG.

Manufactured by Austrian company Seedwings Flugsport GmbH commonly known as Seedwings Europe, from 2007. Compared to the earlier versions of the Space the newer ones have been improved slightly. The VG system has an extra pulley to make pulling easier. And the sidewires have been shortened by approx. 1.5 centimeters to make the roll response easier / faster.

Wing very light and quickly mounted (6 slats on each side and 2 rods easy to put and C all) … in terms of flight, take-off and posed are very easy (it poses at less than 25 km / h ). Towing at 25% VG it tows easily and keeps a straight line. It dampens bumps and is comfortable. In still air the sink rate is 1.2 meters at 0% VG. Just pulling 25% VG decreases this to 0.9 meters. At 0% VG the glider has relatively high bar pressure telling you that the glider wants to stabilize itself all the time. At just 25% VG this becomes significantly lighter and the glide improves. You can hear the stall of the glider. When the glider stalls you can hear the wing “buzzing”. For the landing, no problem, the margin for the final push is very large.

The wing can have an unpleasant behavior at the bend turn with a tendency to dive and slip at too low speed. The manufacturer unveiled their explanation that this characteristic comes from the curved wingtip design: All glider with curved wing tips must steered different – instead of classical weight shifting “steering like a handlebar of a bicycle” must be performed.

The wing is indeed a bit slow at roll but nothing crazy. The wing is otherwise very easy to launch and land, very good building quality and great attention to detail.

Space 14
14.0 sq.m
Pilot Weight: 55-85 kg

Space 16
Wing area: 16 m²
Wing span: 10 m
Aspect ratio: 6.25
Hang glider weight: 24 kg
Minimum pilot weight: 70 kg
Maximum pilot weight: 100 kg
Maximum speed: 85 km/h
Number of battens: 14

Seedwings Europe Funky

The 2005 Funky is a single surface hang glider 165sq ft, 30% double surface approx 35 hours airtime. Mint condition, top quality sailwork. Suit beginner or experienced pilot returning to the sport wanting great handling but better performance than a basic sky floater.

According to the manufacturer apart from a few tweaks the Funky is basically a Seedwings Space without the double sail and without VG.

Modern, curved tip single surface glider with mylar leading edge and aerofoil uprights. Similar to the Icaro Relax which some call an “advanced” single surface.

Funky 15
Wing area: 15.3 m²
Hang glider weight: 21 kg
Minimum pilot weight: 55 kg
Maximum pilot weight: 85 kg
Packed length: 4.90 m
Packed length short: 3.50 m

Funky 17
Wing area: 17.3 m²
Hang glider weight: 23 kg
Minimum pilot weight: 80 kg
Maximum pilot weight: 105 kg
Packed length: 5.15 m
Packed length short: 3.75 m

Seedwings Sensor / Seedwings Europe Sensor

Sensor 1

The Sensor 1 was a 1975 hang glider which featured a double surface sail and swept truncated tips. It was very stable in comparison to most high performance gliders, faster than most standards, and with good penetration. It has positive dive recovery with full sail deflation because of rigid truncated washout. This glider has been the test bed for diffusor tip theory in flex membrane wings.

Sensor I

The Sensor I airframe is made from 6061-T6 1.75in x .049 anodised aluminium tubing and all rigging cable is 3/32in 7 x 7 vinyl coated stainless steel aircraft quality. All hardware is aircraft quality, and the sail is made from 4.25oz and 3.0oz stabilised dacron, then available in white only.

There was the option of seated or prone harness.

The Sensor 2 was from 1976 featured Flare Tips advanced tip design. This eliminates tip stall during steep banked turns and parachuting. The wingtips are extended with a Flare Tip Batten which allows the tip to flex in the angle of attack. The airfoil is a semi-double surface inflated type.

Sensor II

The Sensor II’s Flare Tips gives it a tip inertia that is lower than most. This is very light and flexible concept allows for rapid turn response, light tip gust effects, lower induced drag and improved washout distribution. The airfoil gives high L/D and low moment. The keel is reflexed and cambered for positive pitch moment.

The airframe is made from 6061-T6 and 2024-T3 aluminium tubing that is doweled and bushed. All rigging cable is 3/32in 7 x 7 vinyl coated stainless steel aircraft quality. All hardware is aircraft quality.

The sail is made from 3.8oz Howe & Bainbridge stabilised dacron with reinforcement in stress areas and double zig-zag stitched. The sail is fully battened. Seated or prone harness support sysems were options.

Sensor 2

The Sensor 210B is from 1976.

Sensor 210B

The Sensor 210C is from 1977.

Sensor 210C

The Sensor 210E is from 1979.

Sensor 210E

Construction plans were available for the Sensor 210E, all in inches and AN standards, and available in two sizes. The Sensor at that time was “the ultimate flying machine”. Bob Trampenau has been the inventor of curved flexible wingtips. Despite the fixed crossbars (floating crossbars) and big span it was easy to roll. Now, it handles like an ocean vessel.

Both the Sensor 310A and Sensor 310B were 1977 models.

Sensor 310A

The Sensor 411A was also a 1977 hang glider, followed by the Sensor 411B in 1978.

Sensor 411A
Sensor 411B

The 1985 Sensor 510 was for advanced pilots.

Sensor 510

The Sensor 610 came in 1992.

Sensor 610

Seedwing Europe was authorized to produce the model “Sensor 610-144” until 1993. At the end of the contract, they continued to produce the “Sensor” under the name of “Seedwings Europe” without the agreement of Bob Trampenau.

The Sensor 610 CF3 was a 2000 version for advanced pilots.

Sensor 610 CF3

The 2005 Sensor 610 CF4 was for advanced pilots.

Sensor 610 CF4

The 2007 Sensor 610 CF5 was for advanced pilots.

Sensor 610 CF5

The 2008 Sensor 610 F5 was for advanced pilots.

Sensor 610 F5

Seedwings produced the Sensor 610 and, in 1993, the Sensor 611.

Sensor 611

The 1986 Sensor 710 was for advanced pilots.

Sensor 710

Sensor I
Keel length: 7.5 ft
Wing span: 29.5 ft
Wing area: 145 sq,ft
Aspect ratio: 6
Nose angle: 110˚
Sail billow: .025˚
Weight: 45 lb
Pilot weight: 130-160 lb
Takeoff speed: 15 mph
Stall speed: 16 mph
Max speed: 45 mph
Best glide ratio (L/D): 8-1
Best L/D speed: 25 mph
Min sink: 275 fpm

Sensor II
Keel length: 9.2 ft
Wing span: 32.8 ft
Wing area: 165 sq,ft
Aspect ratio: 6.5
Nose angle: 110˚
Sail billow: 0.5˚
Weight: 36 lb
Pilot weight: 140-180 lb
Takeoff speed: 12 mph
Stall speed: 14 mph
Max speed: 45 mph
Best glide ratio (L/D): 9-1
Best L/D speed: 25 mph
Min sink: 225 fpm

Sensor 210E 183
Wing area: 17m²
Wingspan: 10,5m

Sensor 510
Wing area: 14.96 m²
Wing span: 10.6 m
Aspect ratio: 7.5
Hang glider weight: 30 kg
Number of battens: 20

Sensor 610
Wing area: 13.5 m²
Wing span: 10.4 m
Aspect ratio: 8
Minimum pilot weight: 60 kg
Maximum pilot weight: 85 kg
Nose angle: 127°

Sensor 610 CF3 135
Wing area: 12.63 m²
Wing span: 10 m
Aspect ratio: 8
Hang glider weight: 30 kg
Minimum speed: 32 km/h
Maximum speed: 104 km/h
Max glide ratio (L/H): 15
Minimum sink rate: 0.76 m/s
Packed length: 5.2 m

Sensor 610 CF3 142
Wing area: 13.19 m²
Wing span: 10.4 m
Aspect ratio: 8.1
Hang glider weight: 32 kg
Minimum speed: 32 km/h
Maximum speed: 104 km/h
Max glide ratio (L/H): 15
Minimum sink rate: 0.76 m/s
Packed length: 5.3 m

Sensor 610 CF3 150
Wing area: 13.93 m²
Wing span: 10.7 m
Aspect ratio: 8.2
Hang glider weight: 33 kg
Minimum speed: 32 km/h
Maximum speed: 104 km/h
Max glide ratio (L/H): 15
Minimum sink rate: 0.76 m/s
Packed length: 5.5 m

Sensor 611
Wing area: 14.4 m²
Wing span: 10.85 m
Aspect ratio: 8.2
Minimum pilot weight: 75 kg
Maximum pilot weight: 105 kg
Nose angle: 127°

Sensor 710 145
Wing area: 10.12 m²
Wing span: 13.47 m
Aspect ratio: 7.6
Hang glider weight: 29 kg
Minimum pilot weight: 70 kg
Maximum pilot weight: 85 kg
Packed length: 5 m
Number of battens: 14
Nose angle: 132°

Sensor 710 152
Wing area: 10.43 m²
Wing span: 14.12 m
Aspect ratio: 7.7
Hang glider weight: 30 kg
Minimum pilot weight: 77 kg
Maximum pilot weight: 102 kg
Packed length: 5.2 m
Number of battens: 14
Nose angle: 132°

Sensor I
Sensor II

Aviation Preservation Society of Scotland Sopwith 1½ Strutter

Adam Smith, former director of the National Museum of Flight, started to recruit volunteers in 2000. The group has included retired medics, teachers, civil engineers, film-makers and sign-writers – no one who knew how to build a plane.

The exact working replica has been built by a team of dedicated experts and enthusiasts. The building of the plane took place over the 23 years. The Strutter was built from scratch in a big shed in East Lothian. A group of pensioners aged between 65 and 100 built the historic biplane with nine of them not living to see it finished as their names have been recorded on a plaque in the cockpit.

The plane was built by pensioners in a barn in East Lothian is set to be flown by a young female pilot, Ellie Carter, 20, for the first time.

But they have now completed a Strutter, with a working engine. The Strutter was seen leaving East Lothian on the back of a lorry to undergo testing in West Lothian.

Funding was needed to keep the Strutter in Scotland. It stands in an outsize converted fruit shed in Congalton, near Edinburgh, soon to be sold.

If the shed cannot be purchased, the plane was likely to move to England.

Mike Harper, chair of the Aviation Preservation Society of Scotland, said: “The Strutter is probably worth twice what the shed is worth, but we don’t want to see it leave Scotland, where it was designed and built.

Schweizer 330 / 333

330T

The Schweizer turbine 330 is powered by an Allison 225 C10A engine. The new 350 shp Allison engine has been derated to 200 shp in the 330, which the company claims will provide a full 200 shp under standard day conditions up to 18,000 feet or to 16,000 feet on a 95oF day.

The piston powered 300 and the turbine powered 330 have virtually identical dynamic components main and tail rotor blades, transmissions and drive shafts with the exception of the powerplants.

In training configuration the 330 features three abreast seating, with the middle seat raised and slightly aft to give the instructor an overview. Another variant, for the civil utility market, has four seats in two by two configuration.

In September 2000 Schweizer Aircraft received type certification for the 333. This upgraded version of the 330SP features a new rotor system composed of cambered airfoil blades combined with an increase in maximum and continuous takeoff power. This gives 290 lbs more useful load and a cruise 20 kts higher than the 330SP. The 330SP may be upgraded to the 333.

Gallery

Schweizer 330 Sky Knight
Engine: Allison 250-C10A, 148 shp
Length: 30.84 ft / 9.4 m
Height: 8.53 ft / 2.6 m
Rotor diameter: 26.903 ft / 8.2 m
Max take off weight: 2050.7 lb / 930.0 kg
Weight empty: 1049.6 lb / 476.0 kg
Max. speed: 100 kt / 185 km/h
Cruising speed: 91 kt / 169 km/h
Initial climb rate: 1574.8 ft/min / 8.0 m/s
Service ceiling: 20997 ft / 6400 m
Range: 241 nm / 446 km
Fuel capacity: 60 gal / 227 lt
Crew: 1
Payload: 2-3 pax

330 / TH-330
Engine: 1 x Allison 250-C20W
Instant pwr: 175 kW
Rotor dia: 8.17 m / 27’6″
MTOW: 1000 kg
Useful load: 475 kg
Max speed: 230 mph
Max cruise: 108 kts
Max range: 495 km
Ceiling: 11,200′
HIGE: 13,900 ft
HOGE: 11,200 ft
Crew: 1
Pax: 3
Seats: 3-4

333
Engine: 1 x RR-Allison 250-C20W

Schweizer Aircraft Corp

The Schweizer Aircraft Corporation was an American manufacturer of sailplanes, agricultural aircraft and helicopters located in Horseheads, New York. The company grew out of the Mercury Glider Club which produced the first two Schweizer gliders in the Schweizers’ barn. The company was originally called the Schweizer Metal Aircraft Company. Attorney Bob McDowell indicated to the Schweizers that they should move their manufacturing operation out of their father’s barn and relocate to the Elmira, New York area. The Schweizers received the suggestion positively as they needed more space to produce gliders, but they had no money with which to make the move.

It was incorporated in 1939 by three Schweizer brothers (Paul, William, and Ernest), who built their first glider in 1930.

McDowell convinced Elmira Industries Inc, the local business development corporation, to provide space for the Schweizers on the second floor of the Elmira Knitting Mill Building in return for stock in the company. This resulted in the Schweizer Metal Aircraft Company becoming the Schweizer Aircraft Corporation in 1939, with a sale of shares to Elmira Industries, local businessmen and soaring pilots.

Schweizer primarily produced light, piston-engined helicopters for use in utility and flight-training roles. The Schweizer 300CBi, originally designed and manufactured by Hughes aircraft as the Hughes 269 for the United States Army, is one of the most widely used training helicopters in the world. In 1986, Schweizer acquired all rights to the helicopter from McDonnell Douglas, who had purchased Hughes Helicopters in 1984. After Schweizer acquired the FAA Type Certificate, the helicopter was known for a short time as the Schweizer-Hughes 300C and then simply, the Schweizer 300C.

Schweizer is perhaps known best for its popular line of gliders (sailplanes), the earliest of which (the model SGP 1-1) was produced in 1930. Although very few of the early gliders were built, later models gained popularity, such as the SGS 2-8 and 2-12, which were adopted by the U.S. Army Air Corps for training as the TG-2 and TG-3, respectively.

The Schweizer SGS 1-23 was a world class competition and record setting glider between its first flight in 1948 and the end of its production in 1967.

In the 1950s and 60s the Schweizer Aircraft Corporation designed and manufactured the very popular SGS 1-26 and SGS 2-33 gliders. They are easy to fly, with simple construction, and are quite rugged and forgiving. A powered light aircraft, the Schweizer SA 1-30 was tested, but did not go into production.

The 2-33 was adopted by the United States Air Force Academy as the TG-4, for use in introductory airmanship training. The Academy used over a dozen such gliders until 2002 when they were replaced by more modern sailplanes. The Royal Canadian Air Cadets continue to operate a fleet of over seventy 2-33As.

Other popular Schweizer gliders include the single-seat SGS 1-26 and the two or three-seat 2-32, both of which can be found in many soaring clubs and in private ownership across the United States.

Primarily designers and makers of sailplanes, one of which (SGS 2-32) fitted with piston engine was tested by Lockheed Aircraft Corporation as Q-Star for ‘quiet reconnaissance’ in Vietnam. On Q-Star was based the Lockheed YO-3A, using Schweizer wings and tail, new fuselage and muffled engine.

Company also built for Grumman the Ag-Cat agricultural biplane, later for Gulfstream, before acquiring the rights in 1981 (Ag-Cat subsequently produced by Ag-Cat Corporation).

Schweizer produced the Grumman G-164 Ag Cat, a single-engine biplane agricultural aircraft originally developed by Grumman in the 1950s. Under the contract with Grumman the airplane was built almost continuously between 1957 and 1981. During this period of time Schweizer built 2,455 of the airplanes.

In 1981 Schweizer bought the rights to the design and continued production under the name Schweizer Ag Cat. In 1995 Schweizer sold the rights to the Ag Cat to Ag-Cat Corp. of Malden, Texas. In February 2001 the design was sold to Allied Ag-Cat Productions Inc. of Walnut Ridge, Arkansas. Allied Ag-Cat is not producing new aircraft although a related company operates a large fleet of Ag-Cats.

The basic airframe incorporates many safety innovations, including a pressurized cockpit to keep pesticides out, air conditioning and a fuselage structure that is designed to progressively collapse in the event of a collision.

The basic designof Schweizer S269C remained unchanged over the years. Between Hughes and Schweizer, nearly 3,000 copies of the Model 269/300 have been built and flown over the last 50 years. Schweizer continued to develop the Model 300 by adding a turbine and redesigning the body to create the Schweizer 330, and then further developments led to the development of the Schweizer 333.

An improved version in the series, the Sikorsky S-434, was released in 2008.

In 1972 Schweizer hired David Thurston and production of his Thurston Teal was part of the agreement to work at Schweizer. The company produced three Schweizer TSC-1A1 Teals and nine TSC-1A2 Teal IIs before production was moved to Teal Aircraft in 1976.

The development of the Schweizer SGM 2-37 two-place motor glider for the United States Air Force Academy in 1982 led to a new area of expertise for the company. In the mid-1960s Lockheed had used the Schweizer SGS 2-32 sailplane as the basis for its YO-3 quiet reconnaissance aircraft. Schweizer decided to develop the SGM 2-37 into a similar concept aircraft as the YO-3. The result was the SA 2-37A and B, known as the RG-8A in military use.

The RG-8A was later developed by the company into the twin piston-engined and twin-boom SA 2-38 Condor with the US military designation of RU-38A Twin Condor. This design was further refined into the turboprop-powered RU-38B Twin Condor. The RU-38 was still in production in 2008.

It is believed the US Drug Enforcement Administration purchased aircraft designated Shadowhawk from Schweizer. The aircraft had a poor operational history. They may be designated SA 38B.
Other projects

In partnership with Northrop Grumman (formerly Ryan Aeronautical), Schweizer is developing the MQ-8 Fire Scout helicopter UAV.

Schweizer is currently participating in development of Sikorsky’s X-2 Demonstrator, a prototype aircraft using co-axial rotor blades with a pusher propeller for extra forward thrust.

Makes fuselage assemblies for Piper Aircraft Corporation and structures for Bell Helicopters. Became license-holder for Hughes 300 helicopter in 1983, producing piston-engined three-seat Model 300C from 1984 to present day and developing new 3/4-seat Model 330 turboshaft-powered helicopter (first flown June 1988); also supports Hughes Model 269s.

In 1986 flew the SA 2-37A low-noise special-missions aircraft suited to surveillance and other roles, followed in May 1995 by a radical twin-boom SA 2-37A conversion known as SA 2-38A. Two joined the U.S. Coast Guard as RU-38A Twin Condors for covert patrol and surveillance (one by conversion, one built as new).

In December 1999, Schweizer Aircraft celebrated its 60th Anniversary, and had built more than 2,160 sailplanes. Schweizer was a major U.S. aerospace contractor and no longer manufactured gliders.

Helicopter products offered by the company as of February 2009 included the 300C, 300CBi, and 333.

Previously the oldest privately owned aircraft company in the United States, Schweizer was acquired by Sikorsky Aircraft Corporation of Stratford, Connecticut, in 2004, and became a diversified aerospace company.

In 2011 and 2012 Sikorsky Aircraft Corporation laid off all the workers and closed the plant.

Schempp-Hirth / Göppingen

Sportflugzeugbau Göppingen (Sport Aircraft Göppingen)
Sportflugzeugbau Schempp-Hirth
Schempp-Hirth Flugzeugbau Gmbh

Martin Schempp and Wolf Hirth first met in 1928 and beginning in 1935, the team developed the Minimoa, the first high performance glider to sell more than 100 models. The production of Schempp-Hirth gliders began in the municipal building yard in Göppingen, near Stuttgart, where Martin Schempp founded the Sportflugzeugbau Göppingen (Sport Aircraft Göppingen) company in 1935.

In 1938 the company moved to Kirchheim/Teck and employed more than 300 people during the war time.

The first serial gliders were the aerobatic single seat trainer GÖ-1 ‘Wolf’ from Wolf Hirth and the renown GÖ-3 ‘Minimoa’ as well as the two seat GÖ-4 from Wolfgang Hütter. Occasionally there are single examples which are preserved and maintained as oldtimers which can still be found at airshows.

During the war, the production was forcefully expanded to build parts for, amongst other things, the ME-109, the “Giant” and for the Bachem “Natter”. Alongside the GÖ-4 there were also complete aircraft which were built, like the GÖ-8 and the 13,6m-“Habicht”.

The period after the war till 1955 was bridged with the production of plywood suitcases, leg prosthesis, furniture, weaving looms etc, yet also with fighter jet dummies (F-86) and sound studios for television stations.

The connection to the aviation industry was implemented early on with the production of the Matteson M-1 glider, the production of the powered aircraft GS-6a “Milan” and with works on engine pod and tail section of the “Trumpf” airship D-LEDA.

Licenced production such as “Emeraude” and “Smaragd”, subcontracting for “Kl-107” “, “Do-27”, “Do-28” and subsequently the production of the Standard Austria glider in several versions, ensured the employment of the about 50 employees till 1965.

In 1960s company renamed and built the Milan 656 light tourer, also French Piel Emeraude under licence. During early 1960s production of powered aircraft ceased, licence rights for Emeraude being transferred to Binder Aviatik KG.

Regaining a foothold in the world market was achieved with an own design, the SHK, by Rolf Kunz which was flown into third place in its first attempt at the 1965 World Championships in South Cerny/England.

After that the technology revolution from wood to fiberglass was completed in quick steps – at Schempp-Hirth under the directorship of Klaus Holighaus, who, with the maiden flight of his Cirrus in January 1967, was able to celebrate a successful debut.

Two years later, again in January, he already flew his first “Super Orchid”, the Nimbus-1. With this glider George Moffat won the 1970 World Championships in Marfa/Texas, USA.

With more than 700 produced examples, (of which 200 were produced by Grob), the Standard Cirrus was Schempp-Hirth’s second most successful aircraft in produced units. Further successes followed in 1972 and 1974 when Göran Ax in Yugoslavia and George Moffat in Australia became World Champions in the Open Class flying the Nimbus-2 (the production version of the Nimbus-1).

1974 also marked the maiden flight of the Janus, being the worlds first two seat glider in fiberglass construction. Constantly refined (e.g. 20 m CFK wings) it was only retired from production in 1996 after over 20 years. The last variants were the janus-Ce and janus-CT.

Also in 1974, there was the maiden flight of the single seat motorglider Nimbus-2M. Not only were the first experiences with retractable engines achieved, but also numerous world records were set, from the limited series production.

For the FAI introduced “15 m Racing Class”, Schempp-Hirth delivered the Mini-Nimbus, which came on to the market in many versions and was superseded in 1980 by the Ventus.

A new material had found its way, however, into the Kirchheimer production halls: the carbon fiber. What was included into the Nimbus-2C in a rather inconspicuous manner, proved itself to be the start of, at that time not appreciative of how large, an effective future in the production of high performance gliders. The thin wing profiles of the succeeding developments would not have been possible without the higher strength and stiffness of the carbon fiber.

The lengthening of the lifespan for fiberglass constructed gliders from 3000 to 6000 hours was for example, proven with a Nimbus-2 inner wing.

Serial introduction of carbon fiber was first included on the Nimbus-2C, Mini-Nimbus-C, Janus-C and Janus-CM. the optimal qualities of this new material were only utilized fully later on in the Ventus and Nimbus-3, in the production of the long and thin wings of these models.

Just a few months after its maiden flight, the Nimbus-3 won the 1981 World Championships in Paderborn.

Then the Ventus and Nimbus-3 won the 1983 World Championships in Hobbs/USA and subsequently the Nimbus-3 was also at the front in Rieti in 1985. Together with this, a string of national championships titles for both models and a number of world records for the Nimbus-3 were achieved.

Whilst the production of the single seat Nimbus-3 had to be discontinued after a fire in one of the production halls, this enabled the production of the Racing Class glider Ventus to be increased, allowing the increase in demand for its motorized variant Ventus-bT to be satisfied.

Constant refinement was also the key for the success of the Racing Class glider Ventus which debuted in spring 1986 as the model Ventus-c (on request with wing tip extensions for 17,6 m wingspan). Production of this model was ceased in 1994 after over 600 examples were produced (including self launchers and turbos).

January 1998 saw the delivery of the 4000th built Schempp-Hirth aircraft since the start of the company (including aircraft built under licence).

Today thousands of their gliders are flying around the world. Schempp-Hirth sailplanes include the Ventus A, an advanced 15-meter-class plane with carbon-fiber technology, thin wings, and a low-profile fuselage. The Ventus B is a 15-meter-class craft with a larger cockpit for tall pilots. The Nimbus 2C (open class) has a 20.3- meter wingspan with either carbon or carbon/fiberglass construction. The Janus B has an 18.2-meter wingspan for high-performance tandem two-place flying. The Janus C has a 20-meter span with carbon wings, seating for two, and competition-type performance. The Janus CM, with a 20-meter span, is a two-place motorglider with carbon wings and fully retractable engine. Schempp-Hirth’s newest sailplanes include the Discus, Duo Discus, Ventus and Nimbus, available in a variety of variations, including pure gliders and powered sailplanes.

January 1998 saw the delivery of the 4000th built Schempp-Hirth aircraft since the start of the company (including aircraft built under licence).

2014: Schempp-Hirth Flugzeugbau GmbH
Type Certificate: EASA.A.532

Scheibe

Scheibe-Flugzeugbau GmbH

Egon Scheibe was a young German aircraft engineer, who designed and built some of the most successful gliders before WW2. After the war, he founded Scheibe Flugzeugbau and built a large number of successful gliders, most notably the Bergfalke tandem 2-seater.

Formed at Dachau, near Munich, in 1951 by Egon Scheibe, who at first built gliders designed by Scheibe in Austria. This company had some success with the Mü 13E Bergfalke 1 and then produced a number of conventional gliders. His Sperling two-seat light high-wing monoplane first flew August 1955, and was developed with new wing and tail as SF-23A and built in numbers until 1963. SF-24A Motorspatz built from 1959. SF-25 Motorfalke licencebuilt from 1970 by Slingsby Sailplanes Ltd in UK as Type 61 Falke. SF-28A Tandem-Falke tandem two-seat motorglider no longer offered. Available were the SF-25C Falke 2000 and Rotax-Falke two-seat motorgliders, and the SF-40 two-seat lightplane (first flown 1994), the latter originally offered in A and B versions with tailwheel undercarriages, but the latest version was the SF-40-C with a nosewheel undercarriage. SF-34B Delphin was produced in France as the S.N. Centrair Alliance 34 two-seat glider, while the SF-36 R two-seat motorglider was also expected to go into production in France.

The firm had produced more than 2300 machines by 1983 plus numerous kits for homebuilders.

1983-98: Scheibe Flugzeugbau GmbH, August Pfaltz-Strasse 23, Postfach 1829, D 8060 Dachau bei Mfinchen, West Germany.

Scheibe Flugzeugbau GMBH eventually closed its doors in 2006, partly because of the lack of a successor for Egon Scheibe, but probably also due to the increasingly difficult trading conditions after the boom of Ultralight/Microlight aircraft that have taken over a large portion of the market for fun, relatively cheap, and easy to fly recreational aircraft. The Motorfalke design was subsequently taken over by the newly formed Scheibe Aircraft GMBH based in Heubach (Germany), which has certified the Turbo-Rotax powered version with the glider towing market in mind.