UK
Markets the AX2000 two-seat very light monoplane and several flex-wing microlights as the single-seat Chaser- S, two-seat Quantum Sport and Supersport, two-seat Quantum LITE Basic 503TC and two-seat Quasar.
Publicly owned Pegasus Aviation bought the rights to the French edition of a highly modified Weedhopper.
1998:
Elm Tree Park
Manton
SN8 1PS Marlborough
United Kingdom
In 1931 Pegasus Aircraft Mfg Co built a two-place, open cockpit, high wing monoplane, registered N11145 c/n 1A1. Powered by a 60hp LeBlond engine, after it crashed the registration was cancelled on 18 October 1932.
Pegasus Aircraft Mfg Co
Anthony A Guarniere & Jack Harris,
Maple Heights OH.
USA
In 1931 built a two-place monoplane.
Development of the Pegazair started in 1985 by Serg Dufour of Mont-Saint-Michel, Quebec. Originally it consisted of a new set of Pega-STOL wings with retractable leading edge slats to be installed on Zenair CH 701 STOLs to replace its wing which has fixed leading edge slots, first flown in June 1991.
Dufour went on to develop a new fuselage and tail to match the wings. The Pegazair is a two seats in side-by-side configuration, strut-braced, high-wing monoplane with conventional landing gear. Fuselage construction is welded steel tubing with aluminum skins. The wings employ full length flaperons and leading edge slats that deploy automatically. The tailplane is slotted for slow speed authority. The prototype was outfitted with a 65 hp (48 kW) Continental A-65 engine.
The aircraft was built as the Tapanee Pegazair-100 and the design was later developed into the four seat Tapanee Levitation 4.
Variants
Pegazair P80
Powered by a 80 hp (60 kW) Rotax 912UL
Pegazair P100
Powered by a 80 hp (60 kW) Continental O-200 or 115 hp (86 kW) Rotax 914
Specifications:
P-80
Engine: Rotax 912
Seats: 2 side by side
Length: 22.5 ft
Wingspan: 29.0 ft
Wing area: 150 sq/ft
Max.flaps: 30 deg
MAUW: 1200 lbs
Empty Weight: 625 lbs
Usefull load: 575 lbs
VSO: 23 mph
Min.speed 50 % pwr: 15 mph
Cruise speed: 95 mph
VNE: 110 mph
Gross takeoff dist: 175 ft
Climb rate at Gross: 900 ft / min.
Usable fuel: 52 litres
Range: 325 milles
Ultimate Load: +6 -3,3 G
Pegazair-100 STOL
Engine: 1 × Continental O-200, 75 kW (100 hp)
Length: 6.83 m (22 ft 5 in)
Wingspan: 9 m (29 ft)
Wing area: 14 m2 (150 sq ft)
Airfoil: NACA 2415
Max.flaps: 30 deg
Empty weight: 374 kg (825 lb)
Gross weight: 658 kg (1,450 lb)
Usable Fuel capacity: 134 litres (29 imp gal; 35 US gal)
Cruise speed: 169 km/h; 91 kn (105 mph)
Stall speed: 45 km/h; 24 kn (28 mph)
Never exceed speed: 201 km/h; 109 kn (125 mph)
Min.speed 50 % pwr: 18 mph
Gross takeoff dist: 300 ft
Climb rate at Gross: 800 ft / min.
Range: 1,014 km; 547 nmi (630 mi)
g limits: +6/-3.3
Wing loading: 47 kg/m2 (9.7 lb/sq ft)
Seats: 2 side by side
P-100
Engine: Rotax 914, 115 hp
Seats: 2 side by side
Length: 22.5 ft
Wingspan: 29.0 ft
Wing area: 150 sq/ft
Max.flaps: 30 deg
MAUW: 1350 lbs
Empty Weight: 760 lbs
Usefull load: 690 lbs
VSO: 28 mph
Min.speed 50 % pwr: 18 mph
Cruise speed: 115 mph
VNE: 125 mph
Gross takeoff dist: 225 ft
Climb rate at Gross: 950 ft / min.
Usable fuel: 134 litres
Range: 793 milles
Ultimate Load: +6 -3,3 G
1995: 437 Route 309 Nord, Mont-St.-Michel, Quebec J0W 1P0, Canada.
Built the Pegazair-100 STOL
Pony Trek 1
Paraglider circa 1998.
Wing area: 26.8 sq.m
Pilot weight: 65-85 kg
No. of cells: 50
Wing span: 11.7 m
Aspect ratio: 5
Min sink: 1 m/s
Pony Trek 2
Paraglider circa 1998.
Wing area: 28.2 sq.m
Pilot weight: 80-100 kg
No. of cells: 52
Wing span: 12.6 m
Aspect ratio: 5.2
Min sink: 1 m/s
Pony Trek 3
Paraglider circa 1998.
Wing area: 29.6 sq.m
Pilot weight: 95-115 kg
No. of cells: 54
Wing span: 12.7
Aspect ratio: 5.3
Min sink: 1 m/s
A glider for experienced and XC pilots, the Fenix 2 (Afnor/Cen Performance) is based on a new profile that “allows high performance and resistance to collapses” according to the manufacturer. During its development the goal was to obtain high performance with “exceptional” stability even at top speed, together with easy and dynamic handling. The glider incorporates internal diagonals ribs and a reduced number of lines in two cascades for less drag. It has a partially closed leading edge, and aspect ratio of 5,7. Among its qualities, Pegas mention easy and intuitive handling that makes coring even the tightest thermals an easy task, a wide and usable speed range, and a stability similar to paragliders of Standard category.
The Fenix 2 was constructed with fabric Skytex S9017 for the sail, reinforcements in Dacron W-382/175g and Mylar Scrim, and Dyneema lines 1.1mm and Superaramid 1.7mm.
It was available in 5 sizes, the smallest aimed at Acro; and there’s also a “race” version in two sizes.
Fenix 1
Paraglider circa 1998.
Wing area: 24.1 sq.m
Pilot weight: 65-85 kg
No. of cells: 98
Wing span: 12.1 m
Aspect ratio: 6
Min sink: 1 m/s
Fenix 2
Paraglider circa 1998.
Wing area: 27 sq.m
Pilot weight: 80-100 kg
No. of cells: 98
Wing span: 12.8 m
Aspect ratio: 6
Min sink: 1 m/s
Fenix 3
Paraglider circa 1998.
Wing area: 29.5 sq.m
Pilot weight: 95-115 kg
No. of cells: 98
Wing span: 13.3 m
Aspect ratio: 6
Min sink: 1 m/s
Fenix XR
Paraglider model new in 1998.
Wing area: 29.6 sq.m
Pilot weight: 75-85 kg
No. of cells: 98
Wing span: 13.8 m
Aspect ratio: 6.4
1998: Delnicha 17, CZ-17000 Prague, CZECH REPUBLIC
Paraglider manufacturer
A tractor monoplane designed and recorded as a Deutsche Sommer aircraft, in respect to Pega & Emich (Griesheim am Main) being sold to the Deutsche Sommer-Flugzeugwerke early in 1911. Unsuccessfully powered by a 60 hp Hoffmann-Rotor engine, sporting an uncovered fuselage and elevator section in front.
1998
Cycle: turboed 4 stroke
No cylinders: 2
Bore: 77 mm
Stroke: 67.79 mm
Compression: 8.8
Displacement: 650 cc
Cooling: Air / oil
Ignition: Elctronic
Reduction: Hydromechanical Epicyclic 3/1
Dimension: 750 x 485 x 650 mm
Weight: 70.75 kg complete
Max pwr: 80 hp at 6500 rpm
Max torque: 120 at 3500 rpm
Price 1998: 67 400 Fttc
