About: Hirth Hi 20 MoSe

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The Hirth Hi 20 MoSe was a German motor glider designed in the late 1930s. Based on the Göppingen Gö 4 side-by-side seat training glider, it had a foldaway propeller, column-mounted above the fuselage and shaft-driven by a small internal piston engine.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Hirth Hi-20 (de) Hirth Hi 20 MoSe (en)
rdfs:comment	Die Hirth Hi-20 MoSe war ein Motorsegler mit Klapptriebwerk in den 1930er Jahren. (de) The Hirth Hi 20 MoSe was a German motor glider designed in the late 1930s. Based on the Göppingen Gö 4 side-by-side seat training glider, it had a foldaway propeller, column-mounted above the fuselage and shaft-driven by a small internal piston engine. (en)
dct:subject	Single-engined pusher aircraft 1940s German sailplanes Mid-wing aircraft Motor gliders Aircraft first flown in 1941
Wikipage page ID	35436082 (xsd:integer)
Wikipage revision ID	1114161323 (xsd:integer)
Link from a Wikipage to another Wikipage	Carden-Baynes Auxiliary Propeller (aircraft) Internal combustion engine Germany Tandem Fuselage Single-engined pusher aircraft 1940s German sailplanes Glider (sailplane) Dorsal (anatomy) Motor glider Pusher configuration Göppingen Gö 4 Mid-wing aircraft Motor gliders Aircraft first flown in 1941 Fairing (aircraft) World War II Volksflugzeug Training aircraft Two stroke engine Kirchheim/Teck dbr:Nabern
sameAs	Hirth Hi 20 MoSe Hirth Hi 20 MoSe Hirth Hi 20 MoSe Hirth Hi 20 MoSe
sink rate ftmin	177 (xsd:integer)
sink rate note	minimum, propeller retracted (en)
span m	14.780000 (xsd:double)
wing area sqm	18.700000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Infobox_aircraft_type dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	1941-10-25 (xsd:date)
national origin	Germany
crew	1 (xsd:integer)
manufacturer	Wolf Hirth Gmbh, Nabern (en)
type	Self-launching glider (en)
has abstract	Die Hirth Hi-20 MoSe war ein Motorsegler mit Klapptriebwerk in den 1930er Jahren. (de) The Hirth Hi 20 MoSe was a German motor glider designed in the late 1930s. Based on the Göppingen Gö 4 side-by-side seat training glider, it had a foldaway propeller, column-mounted above the fuselage and shaft-driven by a small internal piston engine. (en)
aspect ratio	11.700000 (xsd:double)
climb rate ftmin	220 (xsd:integer)
cruise speed mph	53 (xsd:integer)
empty weight kg	280 (xsd:integer)
eng1 hp	25 (xsd:integer)
eng1 name	Krautter (en)
eng1 note	at 5,500 rpm (en)
eng1 number	1 (xsd:integer)
eng1 type	four cylinder air-cooled two-stroke (en)
gross weight kg	380 (xsd:integer)
length m	6.880000 (xsd:double)
max speed mph	68 (xsd:integer)
more performance	*Landing speed: 55 km/h; 30 kn (en)
number built	1 (xsd:integer)
prop blade number	2 (xsd:integer)
prop dia m	1.400000 (xsd:double)
prop dia note	geared down 2.3:1 (en)
see also	*Volksflugzeug (en)
gold:hypernym	Glider
prov:wasDerivedFrom	wikipedia-en:Hirth_Hi_20_MoSe?oldid=1114161323&ns=0
page length (characters) of wiki page	6488 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
manufacturer	dbr:Nabern
origin	Germany
type	Glider (sailplane)
foaf:isPrimaryTopicOf	wikipedia-en:Hirth_Hi_20_MoSe
is Link from a Wikipage to another Wikipage of	Mose (disambiguation) List of gliders (H) List of gliders (R) Hirth Hi-20 MoSe
is Wikipage redirect of	Hirth Hi-20 MoSe

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