About: Tisserand Hydroplum

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The Tisserand Hydroplum is a small amphibious aircraft with a single, pusher engine, built in France in the 1980s. Originally a single-seat, high-wing monoplane, it was developed into a two-seat biplane for production in kit form as the SMAN Pétrel.

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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	Tisserand Hydroplum (en)
rdfs:comment	The Tisserand Hydroplum is a small amphibious aircraft with a single, pusher engine, built in France in the 1980s. Originally a single-seat, high-wing monoplane, it was developed into a two-seat biplane for production in kit form as the SMAN Pétrel. (en)
dcterms:subject	High-wing aircraft Single-engined pusher aircraft 1980s French sport aircraft Aircraft first flown in 1983 Amphibious aircraft Biplanes
Wikipage page ID	34330936 (xsd:integer)
Wikipage revision ID	1123838924 (xsd:integer)
Link from a Wikipage to another Wikipage	Amphibious aircraft Rotax 912 Monoplane Conventional undercarriage Brazil Homebuilt aircraft Ultralight Elevator (aircraft) Empennage Strut Centre of gravity Fuselage Leading edge AAC SeaStar Ailerons High-wing aircraft Single-engined pusher aircraft Aircraft fabric covering EDRA Aeronautica Super Pétrel Fin Float (nautical) France 1980s French sport aircraft Hirth Flat-twin Pusher configuration High-wing Rotax 532 Aircraft first flown in 1983 Amphibious aircraft Biplanes Biplane Wing configuration Tailplane Spoiler (aeronautics) Hull (watercraft) Fairing (aircraft) Longeron Rudder Dihedral (aircraft) Spar (aviation) Tricycle gear Interplane strut Flat-four Flight dynamics (aircraft) Planing (sailing) dbr:ARPLAS dbr:EDRA_Aeronautica_Paturi
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sameAs	Tisserand Hydroplum Tisserand Hydroplum Tisserand Hydroplum
sink rate ms	1.700000 (xsd:double)
sink rate note	minimum, power off at 70 km/h (en)
span m	9.250000 (xsd:double)
stall speed kmh	50 (xsd:integer)
wing area sqm	15.400000 (xsd:double)
wing loading kg/m	16.200000 (xsd:double)
wing loading note	maximum (en)
dbp:wikiPageUsesTemplate	dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	late September 1983 (en)
national origin	France
crew	1 (xsd:integer)
designer	Claude Tisserand (en)
fuel capacity	20.0 (litre)
ref	Ultralight and Microlight Aircraft of the World (en)
type	Single-seat amphibious ultralight (en)
has abstract	The Tisserand Hydroplum is a small amphibious aircraft with a single, pusher engine, built in France in the 1980s. Originally a single-seat, high-wing monoplane, it was developed into a two-seat biplane for production in kit form as the SMAN Pétrel. (en)
airfoil	NACA 2415 (en)
aspect ratio	6.600000 (xsd:double)
ceiling m	3000 (xsd:integer)
ceiling note	service (en)

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