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|
The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty.
|
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|
http://dbpedia.org/resource/Werner_Schmeidler +
|
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|
http://dbpedia.org/resource/Wroc%C5%82aw_University_of_Technology +
|
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|
1
|
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http://dbpedia.org/resource/Germany +
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http://commons.wikimedia.org/wiki/Special:FilePath/Schmeidler_SN.2_L%27Aerophile_February_1933.jpg?width=300 +
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|
48755543
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|
10957
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|
1109638556
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http://dbpedia.org/resource/Tempelhof +
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, http://dbpedia.org/resource/Tailplane +
|
| http://dbpedia.org/property/airfoil
|
Göttingen 387
|
| http://dbpedia.org/property/ceilingM
|
2930
|
| http://dbpedia.org/property/ceilingNote
|
wing extensions retracted
:::: wing extensions extended
|
| http://dbpedia.org/property/climbRateMs
|
1.7
|
| http://dbpedia.org/property/climbRateNote
|
wing extensions retracted
:::: wing extensions extended
|
| http://dbpedia.org/property/crew
|
1
|
| http://dbpedia.org/property/designer
|
Werner Schmeidler, Neumann
|
| http://dbpedia.org/property/emptyWeightKg
|
355
|
| http://dbpedia.org/property/emptyWeightNote
|
equipped
|
| http://dbpedia.org/property/endurance
|
7200.0
|
| http://dbpedia.org/property/eng1Name
|
http://dbpedia.org/resource/BMW_X +
|
| http://dbpedia.org/property/eng1Number
|
1
|
| http://dbpedia.org/property/eng1Type
|
five cylinder radial
|
| http://dbpedia.org/property/firstFlight
|
"1932-01-12"^^xsd:date
|
| http://dbpedia.org/property/fuelCapacity
|
fuel ; oil
|
| http://dbpedia.org/property/grossWeightKg
|
470
|
| http://dbpedia.org/property/heightM
|
2
|
| http://dbpedia.org/property/lengthM
|
6.2
|
| http://dbpedia.org/property/manufacturer
|
http://dbpedia.org/resource/Wroc%C5%82aw_University_of_Technology +
|
| http://dbpedia.org/property/maxSpeedKmh
|
160
|
| http://dbpedia.org/property/maxSpeedNote
|
wing extensions retracted
:::: wing extensions extended
*Take-off speed:
*Landing speed: wing extensions retracted
:::: wing extensions extended
|
| http://dbpedia.org/property/morePerformance
|
*Take-off distance into wind, minimum wing extension:
*Take-off distance into wind, maximum wing extension:
*Landing run, minimum wing extension:
*Landing run, maximum wing extension:
|
| http://dbpedia.org/property/nationalOrigin
|
http://dbpedia.org/resource/Germany +
|
| http://dbpedia.org/property/numberBuilt
|
1
|
| http://dbpedia.org/property/primeUnits%3F
|
met
|
| http://dbpedia.org/property/propBladeNumber
|
2
|
| http://dbpedia.org/property/propDiaM
|
1.9
|
| http://dbpedia.org/property/propName
|
metal fixed-pitch propeller
|
| http://dbpedia.org/property/rangeKm
|
300
|
| http://dbpedia.org/property/ref
|
General: L'Aérophile February 1933 Performance: Flugsport March 1932, Flugzeug-Typenbuch 1944
|
| http://dbpedia.org/property/spanM
|
11.4
|
| http://dbpedia.org/property/type
|
Experimental variable wing area aircraft
|
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http://dbpedia.org/resource/Template:Cvt +
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|
| http://dbpedia.org/property/wingAreaNote
|
maximum,
|
| http://dbpedia.org/property/wingAreaSqm
|
12.75
|
| http://dbpedia.org/property/wingLoadingKg/m
|
42.5
|
| http://dbpedia.org/property/wingLoadingNote
|
wing extensions retracted
:::: wing extensions extended
|
| http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:Aircraft_first_flown_in_1932 +
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http://dbpedia.org/resource/Power +
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http://en.wikipedia.org/wiki/Schmeidler_SN.2?oldid=1109638556&ns=0 +
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http://commons.wikimedia.org/wiki/Special:FilePath/Schmeidler_SN.2_L%27Aerophile_February_1933.jpg +
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|
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http://en.wikipedia.org/wiki/Schmeidler_SN.2 +
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|
| rdfs:comment |
The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty.
|
| rdfs:label |
Schmeidler SN.2
|
