Calazzo Salvatore designed the Deadalo 2000 trike unit for paragliders and hang gliders. Engine options are Hirth, Zanzottera, and Vittorazi.

Empty weight: 40 kg
Fuel capacity: 20 lt
Engine: Hirth F-33, 28 hp
Seats: 1
Price (1998): 7 000 000 L

A small single seater for hang glider wings, circa 1998.

Empty weight: 79 kg
Wing span: 10.12 m
Wing area: 13.50 sq.m
Fuel capacity: 10 lt
Engine: Zenoah G25 B1, 22 hp
MAUW: 180 kg
Seats: 1
Max speed: 95 kph
Cruise speed: 60 kph
Minimum speed: 32 kph
Climb rate: 3 m/s
Fuel consumption: 4 lt/hr
Price (1998): 37 265 Fttc

Manufactured in France, the strut-braced trike has gas shocks and can be fitted with factory options including floats, tow system, and spray system. The kit price includes engine and prop.

The Phase II 503 Chronos 16 uses the same basic trike unit and engine as the Zoom, but uses a double-surface wing.

The Phase II 618 ES Chronos 16 Float has the 76 hp Rotax and has enough power to handle floats. Without floats it is good for towing a hang glider.

Phase 2 / Zoom
Engine: Rotax 503, 52 hp.
HP range: 46-70.
Speed max: 75 mph.
Cruise: 48 mph.
Range: 175 sm.
ROC: 500 fpm.
Take-off dist: 150 ft.
Landing dist: 170 ft.
Service ceiling: 15,000 ft.
Fuel cap: 10 USG.
Weight empty: 315 lbs.
Gross: 750 lbs.
Height: 12 ft.
Length: 8 ft.
Wing span: 35 ft.
Wing area: 151 sq.ft.
Seats: 2.
Landing gear: nose wheel.

Cosmos Phase II 503
Empty weight: 130 kg
Wing span: 10.6 m
Wing area: 19 sq.m
Fuel capacity: 55 lt
Engine: Rotax 503 DCDI, 52 hp
MAUW: 350 kg
Seats: 2
Max speed: 105 kph
Cruise speed: 60 kph
Minimum speed: 40 kph
Climb rate: 5 m/s
Fuel consumption: 8 lt/hr
Price (1998): 80 900 Fttc

Phase II 503 Chronos 16
Empty weight: 132 kg
Wing span: 10.6 m
Wing area: 16 sq.m
Fuel capacity: 55 lt
Certification: Vz, B, NL
Engine: Rotax 503 DCDI, 52 hp
MAUW: 350 kg
Seats: 2
Max speed: 125 kph
Cruise speed: 90 kph
Minimum speed: 45 kph
Climb rate: 5 m/s
Fuel consumption: 7 lt/hr
Price (1998): 87 300 Fttc

Phase III 582 ES Top 12.9
Empty weight: 138 kg
Wing span: 9.87 m
Wing area: 13 sq.m
Fuel capacity: 55 lt
Certification: Vz, B
Engine: Rotax 582 DCDI, 64 hp
MAUW: 350 kg
Seats: 2
Max speed: 145 kph
Cruise speed: 100 kph
Minimum speed: 50 kph
Climb rate: 7 m/s
Fuel consumption: 9 lt/hr
Price (1998): 109 900 Fttc

Phase II 618 ES Chronos 16 Float
Empty weight: 158 kg
Wing span: 10.6 m
Wing area: 16 sq.m
Fuel capacity: 55 lt
Engine: Rotax 618 DCDI, 73 hp
MAUW: 400 kg
Seats: 2
Max speed: 130 kph
Cruise speed: 100 kph
Minimum speed: 55 kph
Climb rate: 4 m/s
Fuel consumption: 12 lt/hr
Price (1998): 176 000 Fttc

Engine: Rotax 503, 52 hp.
HP range: 40-70.
Speed max: 48 mph.
Cruise: 28 mph.
Range: 55 sm.
Stall: 22 mph.
ROC: 700 fpm.
Take-off dist: 50 ft.
Landing dist: 50 ft.
Service ceiling: 15,000 ft.
Fuel cap: 5 USG.
Weight empty: 310 lbs.
Gross: 850 lbs.
Height: 12 ft.
Length: 8.5 ft.
Wing span: 36 ft.
Wing area: 232 sq.ft.
Seats: 2.
Landing gear: nose wheel.

Circa 1998, the single seat Echo 12 is of low overall height, and uses a one piece moulding for fuselage, tank and seat.

Engine: Rotax 447, 40 hp.
HP range: 40-65.
Speed max: 87 mph.
Cruise: 45 mph.
Range: 150 sm.
Stall: 24 mph.
ROC: 1000 fpm.
Take-off dist: 100 ft.
Landing dist: 150 ft.
Service ceiling: 15,000 ft.
Fuel cap: 9 USG.
Weight empty: 246 lbs.
Gross: 600 lbs.
Height: 9 ft.
Length: 8 ft.
Wing span: 32 ft.
Wing area: 139 sq.ft.
Seats: 1.
Landing gear: nose wheel.

Engine: Rotax 503 DCDI, 52 hp
Wing span: 9.87 m
Wing area: 12.9 sq.m
Empty weight: 126 kg
MAUW: 280 kg
Fuel capacity: 35 lt
Seats: 1
Max speed: 155 kph
Cruise speed: 110 kph
Minimum speed: 40 kph
Climb rate: 6 m/s
Fuel consumption: 7 lt/hr
Price (1998): 89 350 Fttc

Engine: Rotax 503, 52 hp.
HP range: 46-70.
Speed max: 75 mph.
Cruise: 48 mph.
Range: 175 sm.
Stall: 27 mph.
ROC: 500 fpm.
Take-off dist: 150 ft.
Landing dist: 175 ft.
Service ceiling: 15,000 ft.
Fuel cap: 10 USG.
Weight empty: 310 lbs.
Gross: 750 lbs.
Height: 12 ft.
Length: 8 ft.
Wing span: 35 ft.
Wing area: 151 sq.ft.
Seats: 2.
Landing gear: nose wheel.