
The TST-8 ALPIN DM, new tandem two seater with a retractable engine first flew in 1999 and was introduced in 2000. JAR 22 certified.

The TST-8 ALPIN DM, new tandem two seater with a retractable engine first flew in 1999 and was introduced in 2000. JAR 22 certified.

Czech Republic design imported to Canada and sold by Boohemican International. This motorglider is a modified version of the TST-1Alpin. More or less an ALPIN with the engine mounted in the front and a fixed three-wheel undercarraige, first flown in 1995. Ready to fly $16,250. Two to three month delivery date on kits. Plans $325.
Engine used: Czech M-215
Hp/Hp range: 40/40-55
Length: 19.1 ft
Wing span: 40.4 ft
Wing area: 107.6 sq ft
Fuel Capicty: 6 gal
Empty weight: 561 lbs
Gross weight: 990 lbs
Top Speed: 110 mph
Cruise: 70 mph
Stall: 41 mph
Range: 250 s.m
Rate of climb: 900 fpm
Takeoff distance: 600 ft
Landing distance: 400 ft
Service ceiling: 10,000 ft
No. seats: 1
Landing gear: trigear
Bldg materials: CWF
Bldg man hours: 600
No completed and flown: 3
Info package: $10
Kit cost: $9,840

Czech Republic design imported to Canada and sold by Boohemican International. Engine, propeller and instruments are included in kit price. Ready to fly price in 2009 $21,925. Two to three month delivery date on kits. Plans $325.
Two seat motorglider, side-by-side, with Rotax 582 engine in tractor configuration and nose wheel undercarriage. JAR 22 certified, and first flown in 1996.
Engine used: M-215
Hp/Hp range: 43/43-65
Length: 21.1 ft
Wing span: 48 ft
Wing area: 140 sq ft
Fuel Capacity: 10 gal
Empty weight: 561 lbs
Gross weight: 990 lbs
Top Speed: 112 mph
Cruise: 70 mph
Stall: 41 mph
Range: 26 s.m
Rate of climb: 500 fpm
Takeoff distance: 650 ft
Landing distance: 600 ft
Service ceiling: 10,000 ft
No. seats: 2
Landing gear: trigear
Bldg materials: CWF
Bldg man hours: 700
No completed and flown: 4
Info package: $10
Kit cost 2009: $14,875

The TST-5 VARIANT is an alternative to the DUO with shorter wings (1996)
Two seater, side-by-side microlight aircraft, with ROTAX 582 engine in tractor configuration, clipped wings, suported by struts, and nose wheel undercarriage. JAR 22 certified.

Originally a single seater, World Class performance glider, with “T” tail, nose type tow hook and one wheel undercarriage significant upgraded Alpin, the TST-3 Alpin T kit sailplane has tandem seating for two, with an option for a retractable engine (TST-3 Alpin TM), and with a 44 ft wingspan This aircraft flew several 500 km FAI triangles – in gliding mode (1998).
The TST-3 TL, is a lighter version of the TST-3 T; its pilot broke a series of records in cross-country flights in the 220 kg flying weight category (2001).
JAR 22 certified.
Air Est Services of Marley in France would supply either plans or kits for the TST-1 and would even build a completed sailplane.

The firm designed its first wooden ultralight glider, the TST-1 Alpin, and tested the prototype in 1993. Despite gliding parameters that could bring smiles today, the glider demonstrated a couple of interesting performance feats – e.g. several 300 km FAI triangles and even a 500 km FAI triangle.
The Aplin is a standard club type with a 40.7 ft wingspan for the novice and average skill pilot.
Air Est Services of Marley in France would supply either plans or kits for the TST-1 and would even build a completed sailplane.
Initial engine options were the Czech built UVMV of 28 hp or a 24 hp Koneig.
The design was imported to Canda and sold by Boohemican International. Certified as European ultralight. In 1997, Ready to fly price $15,250, and a two to three month delivery date on kits. Plans cost $325.
The JAR 22 certified single seater glider / motorglider version has a detachable auxiliary Rotax 447 engine in pusher configuration.

There is a tractor version called the TST 1 Junior.

In 1988 two homebuilders from Edmonton, Alberta, Canada, attended the EAA Fly-in with their replica fighters. Ross Grady had his P-40 and Bob Tessori had his Regianne 2002.
Tessori was selling plans for $400 in 1988.
Engine: Ivchenko IA 14RA radial, 260 hp
Max speed: 169 mph

Terrafugia, a New England-based company has introduced the Transition. It’s a street-legal airplane that the company calls “the first step on the road to the practical flying car.”
At first glance, the Transition basically looks like a plane with collapsible wings that make it drive-able on city streets.


The carbon-fiber Terrafugia Transition is in development since 2006, and first flew in 2009.

On the road, it can drive 70 mph (110 kmh) and 93 kn (107 mph / 172 kmh) in the air and have a flight range of 425 nmi (489 miles / 787 km).
Nearing production in 2012, the price was holding at US$279,000 and more than 100 customers were waiting for delivery, possibly in 2014.
The Terrafugia Transition has received exemptions from the NHTSA that make it legal to drive on the road. With polycarbonate windows instead of automotive safety glass and tires not normally considered street legal, it has nevertheless passed muster for both the sky and the highway in terms of weight and safety.

The Terrafugia company had been doing lots of fine tuning since then to attain the proper licensing and exemptions needed to ensure these roadable aircraft are ready for delivery by the end of 2012.
Geely, the company that also owns Volvo, agreed to acquire Terrafugia in 2017. The Terrafugia flying car, created by a handful of MIT grads, received FAA approval in 2016 allowing the transforming car to be certified as a light sport aircraft. The exemption means Terrafugia can create a road- and air-legal vehicle that weighs up to 1,800 pounds.
Terrafugia’s Transition model, the company test vehicle, claims a range of 400 nm at a top speed of about 90 knots. The Transition air/car’s wings fold back to allow the craft to fit in a standard single-car home garage.
The Zhejiang Geely Holding Group confirmed that it is hiring engineers, who must be English-speaking, to help introduce and test-produce prototypes to produce flying cars in China. The company was also seeking contractors to renovate workshops in a passenger car production facility in Hangzhou, Zhejiang province, for the same purpose. Geely said it expects to finish the development of Terrafugia’s first model, TF-1, and launch it in the United States by July 2019.
Transition N302TF
Engine: Rotax 912S, 100hp
Wingspan: 27’6″
Length: 19’2″
Useful load: 430 lb
Cruise Speed: 100 mph (160 km/h)
Stall: 51 mph
Range: 410 mi (660 km) plus 30 min. reserve
Mileage on Road: 35 mpg
Seats: 2

Single or side by side two seat single engined high wing monoplane with conventional three axis control. Wing has unswept leading and trailing edges, and constant chord; cruciform tail. Pitch control by elevator on tail; yaw control by fin mounted rudder; roll control by full span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile NC; double surface. Undercarriage has three wheels in tail dragger formation; nylon rope suspension on tailwheel and steel spring sus¬pension on main wheels. Ground steering by differential braking. Brakes on main wheels. Aluminium tube framework, partially enclosed (totally enclosed optional). Engine mounted above wing driving pusher propeller.
One of the revelations of Sun ‘n’ Fun in March 1983 at Lakeland was the prototype Tierra with which Teratorn Aircraft made a spectacular entrance into that section of the ultralight market which is in direct competition with traditional light air¬craft. This machine offers the facility to be used either as a single seat ultralight or to be transformed into a US category experimental aircraft by the addition of a second scat, the problem of centre of gravity shift being resolved by positioning the single seat in the centre of a wide cockpit, so that it only has to be moved sideways to make room for two. The single stick is central and, as the Tierra has two rudder bars, it becomes a dual control machine when fitted with both seats.
The fuel tank is mounted behind the seating low down at the rear of the cockpit which closes with the clever use of zips for the side panels, the windows coming down to the lower longeron of the cabin. This enclosure is available as an option, as are isolation panels for the cabin. These are made of soundproof material and fit behind the cabin and above the wing and are easily removable. The structure of the Tierra is formed from triangular frames. All the joints in the airframe are reinforced with a strong high density elastic foam pressed into the tubes which absorbs vibration and eliminates metal to metal con¬tact.
Engine location is above the cabin, the motor using dyna focal mounts as in modern conventional aviation. It is a Rotax 377 cc unit fitted with a reduction drive and Teratorn’s own Flexidyne type clutch system. Finally comes an accessory which is still rare in ultralight aviation: the horizontal tail surface of the Tierra is fitted with a trimmer permit¬ting maximum stability in flight regardless of the load carried or its position.
Tierra
Engine: Rotax 377, 36hp at 6600rpm
Propeller diameter and pitch 60 x 36 inch, 1,52 x 0.91 m
Toothed belt reduction, ratio 2.6/1
Max static thrust 245 lb, 111 kg
Power per unit area 0.24 hp/sq.ft, 2.7 hp/sq.m
Fuel capacity 5.0 US gal, 4.2 Imp gal, 18.9 litre
Length overall 18.5 ft, 5.64 m
Height overall 6.0ft, 1.83m
Wing span 31.5ft, 9.60m
Constant chord 4.5 ft, 1.37 m
Sweepback 0 deg
Total wing area 142 sq.ft, 13.2 sq.m
Wing aspect ratio 7.0/1
Empty weight 253 lb, 115kg
Max take off weight 550 lb, 249 kg
Payload 297 lb, 135 kg
Max wing loading 3.87 lb/sq.ft, 18.9 kg/sq.m
Max power loading 15.3 lb/hp, 6.9 kg/hp
Load factors; +6.0, 3.0 ultimate
Max level speed 63 mph, 101 kph
Never exceed speed 63 mph, 101kph
Cruising speed 50mph, 80kph
Stalling speed 25 mph, 40 kph
Max climb rate at sea level 800 ft/min, 4.1 m/s
Min sink rate 300ft/min, 1.5m/s
Best glide ratio with power off 10/1
Take off distance 50 ft, 15 m
Tierra 1
Engine: Rotax 277
Empty wt: 253 lb
Max wt: 650 lb
Wing span: 31ft
Wing area: 154 sq.ft.
Wing loading: 4.22 lbs/sq.ft
Power loading: 23.21 lbs/hp
Max speed: 62 mph
Cruise: 55 mph
Stall: 26 mph
Vne: 75 mph
Seats: 1
Tierra 11
Engine: Rotax 532
Empty: 385 wt. lbs
Max wt.: 850 lbs
Wing span: 36ft
Wing area: 190 sq.ft.
Wing loading: 4.38 lbs/sq.ft
Power loading: 13.08 lbs/hp
Max speed mph: 75
Cruise mph: 60
Stall mph: 30
Vne mph: 80
Seats: 2
Tierra UL
Engine: Rotax 277 (268 cc) 28 hp
Static thrust: 180 lbs
Empty wt: 249 lbs
Wing span: 30’6”
Wing area: 155 sq.ft
Height: 5’8”
Length: 18’6”
Fuel cap; 5 USG
Construction: Aluminium, Dacron, Steel
Max wt: 500 lb
Stall: 24 mph
Max speed: 60 mph
Vne: 70 mph
Climb rate: 500-600 fpm
Design limit: +6, -3g
Glide ratio: 10-1
Wing loading: 3.23 lbs/sq.ft
Power loading: 17.86 lbs/hp
A single-seat aerobatic/ competition monoplane (first flown 1991)