S-M-J Maverick I
| Maverick I | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States |
| Manufacturer | S-M-J |
| Designer | Shanklin, Moore, Johnson |
| Unit cost |
$5,000 in 1969 |
The S-M-J Maverick I is an American aircraft designed for homebuilt construction.
Design and development
The Maverick I is a single-place, open cockpit, single-engine, strut-braced low wing, conventional landing gear- equipped aircraft. The fuselage is of wood construction and the wing is all-aluminum.[1]
Specifications (Maverick I)
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: 139 kn; 257 km/h (160 mph)
- Cruise speed: 122 kn; 225 km/h (140 mph)
See also
- Aircraft of comparable role, configuration and era
References
- ↑ Air Progress: 8. Winter 1969. Missing or empty
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