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Model number adi sportster adi sportster

General Information of ADI SPORTSTER
Designer : Martin Hollmann

First Flight : 1974

Manufacturer : Aircraft Designs

Number Built : 65 (2005)

Role : Autogyro

General characteristics of ADI SPORTSTER
Airfoil : NACA 8H12

Capacity : 1 passenger

Crew : 1

Empty Weight : 650 lb (295 kg)

Fuel Capacity : 17 U.S. gallons (64 L; 14 imp gal)

Gross Weight : 1,100 lb (499 kg)

Height : 8 ft 0 in (2.44 m)

Length : 12 ft 0 in (3.66 m)

Main Rotor Area : 616 sq ft (57.2 m2)

Main Rotor Diameter : 28 ft 0 in (8.53 m)

Powerplant : 1 × Lycoming O-320 4-cyl. air-cooled horizontally opposed piston engine, 150 hp (110 kW)

Performance of ADI SPORTSTER
Cruise Speed : 75mph (65kn; 121km/h)

Maximum Speed : 90mph (145km/h; 78kn)

Power/Mass : 0.14 hp/lb (0.22 kW/kg)

Range : 150mi (130nmi; 241km)

Rate Of Climb : 1,000ft/min (5.1m/s)

Service Ceiling : 12,000ft (3,658m)

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