Overview
Acro Sport Nesmith Cougar — single-seat homebuilt sport aircraftThe Cougar emerged in the early 1970s as a compact low-wing design built around welded steel tubing and fabric covering. Its configuration emphasizes structural simplicity and light weight. Builders were drawn to the design because it required conventional materials and did not depend on complex manufacturing processes.Engine installations vary, but most Cougars use piston engines producing between 100 and 125 horsepower. Cruise speeds typically approach 120 knots (222 km/h), depending on configuration. Maximum takeoff weight generally remains below 1,200 pounds (544 kg), consistent with its lightweight construction and single-seat layout.The Nesmith Cougar remains active in the experimental category, with many examples still flying. Its straightforward design and responsive handling make it suitable for sport and limited aerobatic flying. The aircraft stands as a representative example of grassroots American homebuilt aviation.
Live Fleet Activity (COUG)
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Specifications
- Engine
- 1 × Lycoming O-235
- Engine type
- Piston
- Power
- 115 hp · 86 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 18 ft 11 in · 5.77 m
- Tail height
- 5 ft 6 in · 1.68 m
- Fuselage diameter
- 2 ft 0 in · 0.60 m
- Wing span
- 20 ft 6 in · 6.25 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 1,250 lb · 550 kg
- Max landing weight
- —
- Max payload
- 450 lb · 200 kg
- Fuel capacity
- 30 gal · 100 L · 100 kg (AvGas)
- Max cruise speed
- 170 kt · 196 mph · 315 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 46 kt · 53 mph · 85 km/h
- Range
- 650 nm · 750 mi · 1,200 km
- Fuel burn
- —
- Ceiling
- 13,000 ft · 4,000 m
- Rate of climb
- 1,300 ft/min · 7 m/s
- Takeoff distance
- 1,120 ft · 340 m
- Landing distance
- 980 ft · 300 m
Gallery