About: Doman LZ-5

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.org associated with source document(s)
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The Doman LZ-5 was a utility helicopter developed in the United States in the early 1950s by Doman Helicopters Inc. of Danbury, Connecticut. Despite the procurement of international manufacturing agreements, no series production of the aircraft ever occurred, and only three prototypes were built. Two of these were purchased by the United States Army as the YH-31, but eventually becoming VH-31.

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 umbel-rc:Model_airplane
rdfs:label	Doman LZ-5 (es) Doman LZ-5 (en)
rdfs:comment	El Doman LZ-5 fue un helicóptero utilitario desarrollado en los Estados Unidos a principios de los años 50 del siglo XX, por Doman Helicopters Inc. de Danbury, Connecticut. A pesar de la obtención de acuerdos internacionales de fabricación, no se elaboraron series de aeronaves de producción y solo se construyeron tres prototipos. Dos de ellos fueron comprados por el Ejército estadounidense como YH-31, que finalmente se convirtieron en VH-31. (es) The Doman LZ-5 was a utility helicopter developed in the United States in the early 1950s by Doman Helicopters Inc. of Danbury, Connecticut. Despite the procurement of international manufacturing agreements, no series production of the aircraft ever occurred, and only three prototypes were built. Two of these were purchased by the United States Army as the YH-31, but eventually becoming VH-31. (en)
foaf:depiction
dct:subject	Single-engined piston helicopters 1950s United States helicopters Doman aircraft 1950s United States civil utility aircraft Aircraft first flown in 1953
Wikipage page ID	14597257 (xsd:integer)
Wikipage revision ID	1081463473 (xsd:integer)
Link from a Wikipage to another Wikipage	Stanley Hiller Single-engined piston helicopters 1950s United States helicopters Doman aircraft Doman LZ-4 Glidden Doman Hiller Aviation Museum dbr:Doman_Helicopters Hiller Aircraft 1950s United States civil utility aircraft Aircraft first flown in 1953 Ground effect (aerodynamics) Doman LZ-1 New England Air Museum Fleet Aircraft Ambrosini (aircraft manufacturer) Lycoming SO-580 Horizontally-opposed engine
sameAs	Doman LZ-5 Doman LZ-5 Doman LZ-5 Doman LZ-5 Doman LZ-5 Doman LZ-5
dbp:wikiPageUsesTemplate	dbt:Citation_needed dbt:Cite_book dbt:Convert dbt:Refimprove dbt:Reflist dbt:Short_description dbt:Doman_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type dbt:USAF_helicopters
thumbnail	wiki-commons:Special:FilePath/Doman_YH-31.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	1953-04-27 (xsd:date)
capacity	6 passengers or 4 stretchers or ** cargo (en)
crew	2 (xsd:integer)
designer	Glidden Doman
height ft	10 (xsd:integer)
height in	5 (xsd:integer)
length ft	37 (xsd:integer)
manufacturer	dbr:Doman_Helicopters
ref	Jane's All the World's Aircraft 1956–57 (en)
status	Prototypes only (en)
type	Utility helicopter (en)
has abstract	El Doman LZ-5 fue un helicóptero utilitario desarrollado en los Estados Unidos a principios de los años 50 del siglo XX, por Doman Helicopters Inc. de Danbury, Connecticut. A pesar de la obtención de acuerdos internacionales de fabricación, no se elaboraron series de aeronaves de producción y solo se construyeron tres prototipos. Dos de ellos fueron comprados por el Ejército estadounidense como YH-31, que finalmente se convirtieron en VH-31. (es) The Doman LZ-5 was a utility helicopter developed in the United States in the early 1950s by Doman Helicopters Inc. of Danbury, Connecticut. Despite the procurement of international manufacturing agreements, no series production of the aircraft ever occurred, and only three prototypes were built. Two of these were purchased by the United States Army as the YH-31, but eventually becoming VH-31. (en)
ceiling ft	11500 (xsd:integer)
climb rate ftmin	850 (xsd:integer)
cruise speed mph	99 (xsd:integer)
empty weight lb	2900 (xsd:integer)
empty weight note	, normal empty weight (en)
endurance	13320.0 (second)
eng1 hp	400 (xsd:integer)
eng1 name	Lycoming SO-580-A1 (en)
eng1 number	1 (xsd:integer)
eng1 type	air-cooled eight-cylinder horizontally-opposed engine (en)
length in	10 (xsd:integer)
length note	(en)
max speed mph	104 (xsd:integer)
max takeoff weight lb	5200 (xsd:integer)
more performance	Mission radius: Hover ceiling: (en)
number built	3 (xsd:integer)
rot area sqft	1810 (xsd:integer)
rot dia ft	48 (xsd:integer)
rot number	1 (xsd:integer)
gold:hypernym	Helicopter
prov:wasDerivedFrom	wikipedia-en:Doman_LZ-5?oldid=1081463473&ns=0
page length (characters) of wiki page	7416 (xsd:nonNegativeInteger)
number built	3 (xsd:nonNegativeInteger)
designer	Glidden Doman

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