About: Gatard Statoplan Poussin

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

About: Gatard Statoplan Poussin Goto Sponge NotDistinct Permalink

An Entity of Type : umbel-rc:Model_airplane, 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%2FGatard_Statoplan_Poussin&invfp=IFP_OFF&sas=SAME_AS_OFF&graph=http%3A%2F%2Fdbpedia.org&graph=http%3A%2F%2Fdbpedia.org

The Gatard Statoplan AG 02 Poussin (French: "Chick") was a light, single-seat sports airplane developed in France in the late 1950s and marketed for homebuilding. In layout, it was a low-wing cantilever monoplane of short-coupled design with fixed tailwheel undercarriage. Construction was a plywood-covered wooden structure throughout, and the cockpit was enclosed by a large perspex bubble canopy. The variable-incidence horizontal stabiliser was fitted with small endplates to provide extra directional stability but there were no separate elevators.

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	Gatard Statoplan Poussin (en)
rdfs:comment	The Gatard Statoplan AG 02 Poussin (French: "Chick") was a light, single-seat sports airplane developed in France in the late 1950s and marketed for homebuilding. In layout, it was a low-wing cantilever monoplane of short-coupled design with fixed tailwheel undercarriage. Construction was a plywood-covered wooden structure throughout, and the cockpit was enclosed by a large perspex bubble canopy. The variable-incidence horizontal stabiliser was fitted with small endplates to provide extra directional stability but there were no separate elevators. (en)
dcterms:subject	1950s French sport aircraft Gatard aircraft Low-wing aircraft Aircraft first flown in 1957 Homebuilt aircraft Single-engined tractor aircraft
Wikipage page ID	16682206 (xsd:integer)
Wikipage revision ID	1018211943 (xsd:integer)
Link from a Wikipage to another Wikipage	NACA airfoil Monoplane Homebuilt aircraft Volkswagen air-cooled engine Lift (force) French language Conventional landing gear 1950s French sport aircraft Climb (aeronautics) Gatard aircraft Low-wing aircraft Aircraft first flown in 1957 Homebuilt aircraft Single-engined tractor aircraft France Angle of attack Flight dynamics Flap (aircraft) Bubble canopy Cantilever Flat-four dbr:Albert_Gatard
sameAs	Gatard Statoplan Poussin Gatard Statoplan Poussin Gatard Statoplan Poussin Gatard Statoplan Poussin
span m	6.400000 (xsd:double)
stall speed kmh	65 (xsd:integer)
wing area sqm	6.150000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cvt dbt:Reflist dbt:Gatard_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	1957 (xsd:integer)
crew	one (en)
designer	dbr:Albert_Gatard
manufacturer	Homebuilt aircraft
ref	Jane's All The World's Aircraft 1976–77 (en)
type	Sports plane (en)
has abstract	The Gatard Statoplan AG 02 Poussin (French: "Chick") was a light, single-seat sports airplane developed in France in the late 1950s and marketed for homebuilding. In layout, it was a low-wing cantilever monoplane of short-coupled design with fixed tailwheel undercarriage. Construction was a plywood-covered wooden structure throughout, and the cockpit was enclosed by a large perspex bubble canopy. The variable-incidence horizontal stabiliser was fitted with small endplates to provide extra directional stability but there were no separate elevators. An unusual feature of the design was the aircraft's method of climbing. In most aircraft designs, climb is achieved (without change in engine power) by pitching the aircraft so that the angle of attack of the wings increases, thereby increasing lift. The Poussin, however, was designed to climb by lowering specially-designed flaps and trimming the tailplane to balance out any change in pitch, therefore allowing the aircraft to achieve its maximum rate of climb while keeping the fuselage within 4° of level. The extra drag created by the lowered flaps was balanced by drag saved by keeping the fuselage level. (en)
airfoil	NACA airfoil
climb rate ftmin	435 (xsd:integer)
cruise speed kmh	144 (xsd:integer)
empty weight kg	170 (xsd:integer)
eng1 kw	18 (xsd:integer)
eng1 name	modified Volkswagen (en)
eng1 number	1 (xsd:integer)
eng1 type	air-cooled flat-four (en)
height m	1.500000 (xsd:double)
length m	4.530000 (xsd:double)
max takeoff weight kg	280 (xsd:integer)
more performance	Take-off distance to : Landing distance from : (en)
never exceed speed kmh	216 (xsd:integer)
prop blade number	2 (xsd:integer)
prop name	Gatard fixed-pitch wooden propeller (en)
range km	375 (xsd:integer)
gold:hypernym	Airplane
prov:wasDerivedFrom	wikipedia-en:Gatard_Statoplan_Poussin?oldid=1018211943&ns=0
page length (characters) of wiki page	4452 (xsd:nonNegativeInteger)
designer	dbr:Albert_Gatard
manufacturer	Homebuilt aircraft
foaf:isPrimaryTopicOf	wikipedia-en:Gatard_Statoplan_Poussin
is Link from a Wikipage to another Wikipage of	Gatard Statoplan Pigeon Gatard Statoplan AG-02 Poussin
is Wikipage redirect of	Gatard Statoplan AG-02 Poussin
is foaf:primaryTopic of	wikipedia-en:Gatard_Statoplan_Poussin

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, 59 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software