About: Nelson H-63

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The Nelson H-63, known in the US military designation system as the YO-65, is an American dual ignition, four-cylinder, horizontally opposed, two-stroke aircraft engine that was developed by the Nelson Engine Company for use in helicopters and light aircraft. The engine designation means horizontally opposed 63 cubic inch displacement.

Attributes	Values
rdf:type	yago:WikicatNelsonAircraftEngines yago:WikicatTwo-strokeAircraftPistonEngines yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Instrumentality103575240 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Whole100003553 yago:WikicatAir-cooledAircraftPistonEngines
rdfs:label	Nelson H-63 (en)
rdfs:comment	The Nelson H-63, known in the US military designation system as the YO-65, is an American dual ignition, four-cylinder, horizontally opposed, two-stroke aircraft engine that was developed by the Nelson Engine Company for use in helicopters and light aircraft. The engine designation means horizontally opposed 63 cubic inch displacement. (en)
dcterms:subject	Air-cooled aircraft piston engines Two-stroke aircraft piston engines Nelson aircraft engines
Wikipage page ID	31173759 (xsd:integer)
Wikipage revision ID	1111456712 (xsd:integer)
Link from a Wikipage to another Wikipage	San Leandro, California List of aircraft engines US Army United States Light aircraft Franklin Engine Company Type certificate Helicopter Air-cooled aircraft piston engines Two-stroke aircraft piston engines Aircraft engine Carburetor Irwin, Pennsylvania EAA AirVenture Museum Syracuse, New York Naples, Florida Nelson Aircraft Nelson aircraft engines Hiller YROE 80/87 avgas Two-stroke Horizontally opposed Hiller XROE-1 Rotorcycle Lobet/Shafor Ganagobie Nelson Engine Company
sameAs	Nelson H-63 Nelson H-63 Nelson H-63 Nelson H-63 Nelson H-63
valvetrain	2 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Citation_needed dbt:Convert dbt:Cvt dbt:Reflist dbt:Short_description dbt:Use_American_English dbt:Use_mdy_dates dbt:Nelson_Aircraft dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs
national origin	United States
manufacturer	Nelson Engine Company
power	at 4000 rpm (en)
ref	FAA Type Certificate Data Sheet, Aircraft engines of the World 1957 (en)
type	Two-stroke aircraft engine (en) Four-cylinder, two-stroke, dual ignition, vertically mounted helicopter engine (en)
weight	Bare engine: ; including the cooling fan, cooling shroud and clutch (en)
has abstract	The Nelson H-63, known in the US military designation system as the YO-65, is an American dual ignition, four-cylinder, horizontally opposed, two-stroke aircraft engine that was developed by the Nelson Engine Company for use in helicopters and light aircraft. The engine designation means horizontally opposed 63 cubic inch displacement. (en)
compression	8 (xsd:integer)
coolingsystem	fan forced air (en)
displacement	63 (xsd:integer)
fuelsystem	Nelson E-500 carburetor (en)
fueltype	80 (xsd:integer)
major applications	Hiller YROE
oilsystem	premixed oil in fuel, SAE 30 outboard motor oil mixed at 16:1 fuel to oil (en)
reduction gear	none (en)
see also	*List of aircraft engines (en)
gold:hypernym	Ignition
prov:wasDerivedFrom	wikipedia-en:Nelson_H-63?oldid=1111456712&ns=0
page length (characters) of wiki page	5283 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Nelson_H-63
is Link from a Wikipage to another Wikipage of	Schempp-Hirth Nimbus-2 List of aircraft engines Lobet Ganagobie Hiller ROE Rotorcycle H63 Nelson Aircraft Nelson H-63A Nelson O-65 Nelson YO-65 Nelson YO-65-2
is Wikipage redirect of	Nelson H-63A Nelson O-65 Nelson YO-65 Nelson YO-65-2
is eng1 name of	Hiller ROE Rotorcycle
is foaf:primaryTopic of	wikipedia-en:Nelson_H-63

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