Engineering:Ace Scooter
From HandWiki
Scooter | |
---|---|
Role | Homebuilt aircraft |
National origin | United States |
Manufacturer | Ace Aircraft Manufacturing Company |
The Ace Scooter is an American aircraft that was designed for homebuilt construction.
Design and development
The Ace Scooter is a single place, strut-braced, high wing aircraft with conventional landing gear, which is steel. The tractor engine is mounted above the wing. The open cockpit has a short rounded nose. The fuselage is of wood construction with aircraft fabric covering.[1][2]
Specifications (Scooter)
Data from Air Trails
General characteristics
- Crew: 1
- Length: 15 ft 8 in (4.78 m)
- Wingspan: 28 ft (8.5 m)
- Height: 7 ft (2.1 m)
- Wing area: 115 sq ft (10.7 m2)
- Aspect ratio: 6.75
- Empty weight: 390 lb (177 kg)
- Gross weight: 625 lb (283 kg)
- Fuel capacity: 7 U.S. gallons (26 L; 5.8 imp gal)
- Powerplant: 1 × Volkswagen air-cooled engine Horizontally opposed piston, 65 hp (48 kW)
- Propellers: 2-bladed wooden
Performance
- Maximum speed: 76 kn (88 mph, 142 km/h)
- Cruise speed: 65 kn (75 mph, 121 km/h)
- Stall speed: 30 kn (34 mph, 55 km/h)
- Service ceiling: 12,000 ft (3,700 m)
- Rate of climb: 600 ft/min (3.0 m/s)
Related development
References
- ↑ "none". Air Trails: 74. Summer 1971.
- ↑ "Ace Aircraft Ace Scooter". http://all-aero.com/index.php/contactus/45-planes-d-e-f/3641-flaglor-scooter.
![]() | Original source: https://en.wikipedia.org/wiki/Ace Scooter.
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