Pasped Skylark: Difference between revisions
Content deleted Content added
MilborneOne (talk | contribs) new aircraft article |
wikilinking |
||
| Line 6: | Line 6: | ||
| caption= |
| caption= |
||
}}{{Infobox Aircraft Type |
}}{{Infobox Aircraft Type |
||
| type= |
| type=Two-seat cabin [[monoplane]] |
||
| national origin=United States |
| national origin=[[United States]] |
||
| manufacturer=[[Pasped Aircraft Company]] |
| manufacturer=[[Pasped Aircraft Company]] |
||
| designer= |
| designer= |
||
| Line 20: | Line 20: | ||
}} |
}} |
||
|} |
|} |
||
The '''Pasped W-1 Skylark''' is a 1930s [[United States|American]] two-seat single-engined cabin monoplane designed and built by the [[Pasped Aircraft Company]] of Glendale, California.<ref name="orbis" /> |
The '''Pasped W-1 Skylark''' is a 1930s [[United States|American]] two-seat single-engined cabin [[monoplane]] designed and built by the [[Pasped Aircraft Company]] of Glendale, California.<ref name="orbis" /> |
||
==Design and development== |
==Design and development== |
||
Revision as of 23:18, 18 February 2010
| Pasped Skylark | |
|---|---|
| Role | Two-seat cabin monoplane |
| National origin | United States |
| Manufacturer | Pasped Aircraft Company |
| First flight | 1935 |
| Number built | 1 |
The Pasped W-1 Skylark is a 1930s American two-seat single-engined cabin monoplane designed and built by the Pasped Aircraft Company of Glendale, California.[1]
Design and development
The Skylark is a braced low-wing monoplane with a fixed tailwheel landing gear.[1] It is powered by a 125 hp (93 kW) Warner Scarab radial engine.[1] The enclosed cockpit has side-by-side seating for two.[1] It has a welded steel fuselage and wooden wings.[1] With other two-seat aircraft of the era having a better performance on smaller engines the Skylark did not enter production.[1]
Specifications
Data from [2]
General characteristics
- Crew: 2
- Length: 25 ft 0 in (7.62 m)
- Wingspan: 35 ft 11 in (10.95 m)
- Max takeoff weight: 1,885 lb (855 kg)
- Powerplant: 1 × Warner Scarab radial engine, 125 hp (93 kW)
Performance
- Maximum speed: 139 mph (224 km/h, 121 kn)
- Cruise speed: 125 mph (201 km/h, 109 kn)
- Minimum control speed: 35 mph (56 km/h, 30 kn)
- Range: 475 mi (764 km, 413 nmi)
References
Notes
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help)