Sparmann S-1
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| {{Infobox Aircraft Begin
| name=Sparmann S-1 | image= Sparmann S 1-A.jpg | caption=Sparmann S-1. }}{{Infobox Aircraft Type | type=Training monoplane | national origin=Sweden | manufacturer=Sparmann | designer= | first flight= | introduced= | retired= | status= | primary user=Swedish Air Force | number built= | developed from= | variants with their own articles= }} |
The Sparmann S-1 was a 1930s Swedish military training monoplane, designed by Edmund Sparmann, built in small numbers for the Swedish Air Force. The S-1 was a single-seat low-wing braced-monoplane with a fixed trail-skid landing gear. It was powered by a single 130 hp (97 kW) de Havilland Gipsy Major engine.
Operators
;{{SWE}}
Specifications
{{Aircraft specs
|ref={{cite web|last=Henriksson|first=Lars|title=P 1 - Sparmann S 1-A "Sparmannjagaren" (1939-1947)|url=http://www.avrosys.nu/aircraft/Misc/461P1.htm|access-date=10 June 2013}}{{cite book |title=Jane's all the World's Aircraft 1937 |editor1-last=Grey |editor1-first=C.G. |year=1937 |publisher=Sampson Low, Marston & company, ltd |location=London |editor2-last=Bridgman|editor2-first=Leonard |page=266c}}
|prime units?=met
|crew=1
|length m=6.18
|span m=8
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=8.34
|aspect ratio=
|airfoil=
|empty weight kg=417
|gross weight kg=630
|gross weight note=normal; {{cvt|585|kg}} aerobatic
|max takeoff weight kg=625
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|120|L|USgal impgal}} in a fuselage tank
|more general=
|eng1 number=1
|eng1 name=de Havilland Gipsy Major
|eng1 type=4-cyl. inverted air-cooled in-line piston engine
|eng1 kw=97
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|max speed kmh=250
|max speed note=aerobatic
|cruise speed kmh=210
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=880
|range note=at cruise
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=6000
|ceiling note=service ceiling
|g limits=
|roll rate=
|glide ratio=
|climb rate ftmin=1495
|time to altitude={{cvt|1000|m}} in 2.5 minutes
::::::{{cvt|2000|m}} in 5.3 minutes
::::::{{cvt|4000|m}} in 14.7 minutes
::::::{{cvt|5000|m}} in 24.4 minutes
|wing loading kg/m2=75
|wing loading note=normal; {{cvt|70.2|kg/m2}}
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|0.094|hp/lb|kW/kg|order=flip}} normal; {{cvt|0.1043|hp/lb|kW/kg|order=flip}} aerobatic
|thrust/weight=
|more performance=
}}
See also
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|similar aircraft=
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References
{{reflist}}
Further reading
- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }}
- {{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing}}