S-M-J Maverick I
| Maverick I | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States |
| Manufacturer | S-M-J |
| Designer | Shanklin, Moore, Johnson |
The S-M-J Maverick I is an American aircraft designed for homebuilt construction.
Design and development[edit]
The S-M-J Maverick I is a single-seat, open cockpit, single-engine aircraft with a strut-braced low wing and conventional landing gear. The fuselage is of wood construction and the wing is aluminium.[1]
Specifications (Maverick I)[edit]
Data from Air Progress
General characteristics
- Crew: one
- Wingspan: 25 ft (7.6 m)
- Empty weight: 1,075 lb (488 kg)
- Powerplant: 1 × Lycoming O-320 horizontally opposed piston aircraft engine, 150 hp (110 kW)
- Propellers: 2-bladed
Performance
- Maximum speed: 140 kn (160 mph, 260 km/h)
- Cruise speed: 120 kn (140 mph, 230 km/h)
See also[edit]
Aircraft of comparable role, configuration, and era
References[edit]
- ^ Air Progress: 8. Winter 1969.
{{cite journal}}: Missing or empty|title=(help)