About: Gardan GY-120

Facets (new session)
Description
Metadata
Settings
- Rule:
- Inverse Functional Properties:
- "Same As":

About: Gardan GY-120 Goto Sponge NotDistinct Permalink

An Entity of Type : yago:Type105840188, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon

http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FGardan_GY-120&invfp=IFP_OFF&sas=SAME_AS_OFF

The Gardan GY-120 was a single engine, parasol wing ultralight seating two in tandem, designed and built in France in the 1980s. It did not go into production.

Attributes	Values
rdf:type	Thing software 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	Gardan GY-120 (en)
rdfs:comment	The Gardan GY-120 was a single engine, parasol wing ultralight seating two in tandem, designed and built in France in the 1980s. It did not go into production. (en)
dcterms:subject	Aircraft manufactured in France Single-engined tractor aircraft 1980s French sport aircraft Aircraft first flown in 1984 Parasol-wing aircraft
Wikipage page ID	34281979 (xsd:integer)
Wikipage revision ID	943770862 (xsd:integer)
Link from a Wikipage to another Wikipage	Conventional undercarriage Ultralight Elevator (aircraft) Tandem Aircraft manufactured in France Fuselage Leading edge Ailerons Single-engined tractor aircraft Fin France 1980s French sport aircraft Parasol wing Hirth 2702 Aircraft first flown in 1984 Parasol-wing aircraft Chord (aircraft) Tailplane Rudder Longerons dbr:Yves_Gardan Inline engine (aviation) Two-stroke Two stroke Kingpost Landing wires Flying wires MTOW
sameAs	Gardan GY-120 Gardan GY-120 Gardan GY-120
sink rate ms	1.800000 (xsd:double)
sink rate note	minimum at 65 km/h (en)
span m	10 (xsd:integer)
stall speed kmh	38 (xsd:integer)
wing area sqm	17.500000 (xsd:double)
wing loading kg/m	19.400000 (xsd:double)
wing loading note	maximum (en)
dbp:wikiPageUsesTemplate	dbt:Gardan_aircraft dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	1984-04-27 (xsd:date)
national origin	France
capacity	two (en)
designer	dbr:Yves_Gardan
fuel capacity	30.0 (litre)
manufacturer	Société des Avions Yves Gardan (en)
ref	Ultralight and Microlight Aircraft of the World (en)
type	Two seat ultralight (en)
has abstract	The Gardan GY-120 was a single engine, parasol wing ultralight seating two in tandem, designed and built in France in the 1980s. It did not go into production. (en)
aspect ratio	5.700000 (xsd:double)
ceiling m	2500 (xsd:integer)
ceiling note	service (en)
climb rate ms	2.500000 (xsd:double)
climb rate note	maximum at sea level (en)
cruise speed kmh	75 (xsd:integer)
cruise speed note	economic (en)
empty weight kg	145 (xsd:integer)
eng1 hp	40 (xsd:integer)
eng1 name	Hirth 2702
eng1 note	at 7,000 rpm, toothed belt 2.7:1 output speed reduction (en)
eng1 number	1 (xsd:integer)
eng1 type	air cooled, twin cylinder inline two stroke (en)
g limits	+6.6/-3.3 ultimate (en)
glide ratio	power off 10:1 at 65 km/h (en)
height m	2.500000 (xsd:double)
length m	5.800000 (xsd:double)
max speed kmh	120 (xsd:integer)
max takeoff weight kg	340 (xsd:integer)
more performance	2100.0 (second)
number built	1 (xsd:integer)
power/mass	11.400000 (xsd:double)

Faceted Search & Find service v1.17_git139 as of Feb 29 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 56 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software