About: Aérostructure Lutin 80

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The Aérostructure Lutin 80, earlier known as the PLM 80 (planeur léger motorisé), is a small, single seat motor glider with a low power pusher configuration engine, designed and built in France in the 1980s. Only two were completed.

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	Aérostructure Lutin 80 (en)
rdfs:comment	The Aérostructure Lutin 80, earlier known as the PLM 80 (planeur léger motorisé), is a small, single seat motor glider with a low power pusher configuration engine, designed and built in France in the 1980s. Only two were completed. (en)
dcterms:subject	1980s French ultralight aircraft
Wikipage page ID	37469437 (xsd:integer)
Wikipage revision ID	1113012194 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Elevator (aircraft) Epoxy Empennage Aileron 1980s French ultralight aircraft Fuselage Aircraft fairing France Trailing edge Motor glider Pusher configuration Chord (aircraft) Landing gear Tailplane Air brake (aircraft) Cantilever Canopy (aircraft) Dihedral (aircraft) T-tail Two stroke Glassfibre Disk brake dbr:Conservatoire_de_l'Air_et_de_L'Éspace_d'Aquitaine
Link from a Wikipage to an external page
sameAs	Aérostructure Lutin 80 Aérostructure Lutin 80 Aérostructure Lutin 80
sink rate ms	0.700000 (xsd:double)
span m	11 (xsd:integer)
stall speed kmh	75 (xsd:integer)
wing loading kg/m	49.290000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	1983-05-03 (xsd:date)
national origin	France
crew	One (en)
fuel capacity	30.0 (litre)
manufacturer	Aérostructure SARL (en)
ref	Jane's All the World's Aircraft 1984-85. All performance figures estimated. (en)
type	Single seat motor glider (en)
has abstract	The Aérostructure Lutin 80, earlier known as the PLM 80 (planeur léger motorisé), is a small, single seat motor glider with a low power pusher configuration engine, designed and built in France in the 1980s. Only two were completed. (en)
airfoil	Wortmann WX-66S-196-V1 (en)
aspect ratio	18.910000 (xsd:double)
ceiling m	5000 (xsd:integer)
ceiling note	approximately (en)
climb rate ms	6 (xsd:integer)
climb rate note	powered, maximum at sea level (en)
cruise speed kmh	170 (xsd:integer)
cruise speed note	economical, powered (en)
empty weight kg	155 (xsd:integer)
eng1 kw	28.500000 (xsd:double)
eng1 name	JPX PAL 640 (en)
eng1 number	1 (xsd:integer)
eng1 type	three cylinder two stroke, 636 c.c. swept volume. (en)
glide ratio	32 (xsd:integer)
height m	1.100000 (xsd:double)
length m	5.100000 (xsd:double)
max speed kmh	220 (xsd:integer)
max speed note	powered or gliding in smooth air (en)
max takeoff weight kg	275 (xsd:integer)
never exceed speed kmh	260 (xsd:integer)
never exceed speed note	powered (en)
number built	2 (xsd:integer)
power/mass	103 (xsd:integer)
prop blade number	3 (xsd:integer)
prop dia m	0.940000 (xsd:double)
prop dia note	, pusher. Folding glass-fibre blades. Some photographs show a 2-bladed propeller. (en)
range km	600 (xsd:integer)
range note	with maximum fuel (en)
gold:hypernym	Glider
prov:wasDerivedFrom	wikipedia-en:Aérostructure_Lutin_80?oldid=1113012194&ns=0
page length (characters) of wiki page	6298 (xsd:nonNegativeInteger)
number built	2 (xsd:nonNegativeInteger)
origin	France
type	Motor glider
foaf:isPrimaryTopicOf	wikipedia-en:Aérostructure_Lutin_80
is Link from a Wikipage to another Wikipage of	List of aircraft (0–Ah)

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