About: Arpin A-1

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.org:8891 associated with source document(s)
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http://dbpedia.org:8891/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FArpin_A-1

The Arpin A-1 was a two-seat low-wing monoplane which was powered by a single radial engine in pusher configuration, mounted behind the cabin between twin booms that carried the tail. An unconventional fixed tricycle undercarriage was fitted. Only one was built.

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	Arpin A-1 (en) Arpin A-1 (fr) アーピン A-1 (ja)
rdfs:comment	The Arpin A-1 was a two-seat low-wing monoplane which was powered by a single radial engine in pusher configuration, mounted behind the cabin between twin booms that carried the tail. An unconventional fixed tricycle undercarriage was fitted. Only one was built. (en) アーピン A-1（Arpin A-1）は、プッシャー方式の単発低翼単葉機である。キャビン後部の2本のブームの間に星型エンジンを後ろ向きに搭載し、通常とは異なる固定の首車輪式降着装置を備えていた。1機のみ製作。 (ja) L'Arpin A-I est un avion de tourisme biplace britannique de l'entre-deux-guerres. Monoplan à aile basse et train tricycle fixe, l'Arpin A-I se caractérisait par un moteur propulsif en étoile entraînant une hélice tournant entre les poutres supportant l'empennage. Le prototype [G-AFGB] effectua son premier vol le 7 mai 1938. * Portail de l’aéronautique (fr)
dcterms:subject	Arpin aircraft Low-wing aircraft Single-engined pusher aircraft 1930s British civil utility aircraft Aircraft first flown in 1938
Wikipage page ID	11048170 (xsd:integer)
Wikipage revision ID	1050359322 (xsd:integer)
Link from a Wikipage to another Wikipage	United Kingdom Radial engine General Aircraft GAL.47 Arpin aircraft M. B. Arpin & Co. Low-wing aircraft Single-engined pusher aircraft Pusher configuration Hanworth Aerodrome 1930s British civil utility aircraft Aircraft first flown in 1938 Blackburn Cirrus Minor School of Army Co-operation Twin boom Old Sarum Tricycle undercarriage Salmson AD.9 Longford, Hillingdon
sameAs	Arpin A-1 Arpin A-1 Arpin A-1 Arpin A-1 Arpin A-1 Arpin A-1
span ft	31 (xsd:integer)
span in	6 (xsd:integer)
span m	9.610000 (xsd:double)
wing area sqft	165 (xsd:integer)
wing area sqm	15.300000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Refbegin dbt:Refend dbt:Reflist dbt:Use_British_English dbt:Use_dmy_dates dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	imp (en)
first flight	1938-05-07 (xsd:date)
national origin	United Kingdom
capacity	one passenger (en)
crew	one, pilot (en)
designer	Morris Arpin (en)
height ft	7 (xsd:integer)
height in	1 (xsd:integer)
length ft	23 (xsd:integer)
manufacturer	M. B. Arpin & Co.
retired	1946 (xsd:integer)
type	Two-seat cabin monoplane (en)
has abstract	The Arpin A-1 was a two-seat low-wing monoplane which was powered by a single radial engine in pusher configuration, mounted behind the cabin between twin booms that carried the tail. An unconventional fixed tricycle undercarriage was fitted. Only one was built. (en) L'Arpin A-I est un avion de tourisme biplace britannique de l'entre-deux-guerres. Monoplan à aile basse et train tricycle fixe, l'Arpin A-I se caractérisait par un moteur propulsif en étoile entraînant une hélice tournant entre les poutres supportant l'empennage. Le prototype [G-AFGB] effectua son premier vol le 7 mai 1938. Après remotorisation avec un Cirrus Minor I de 90 ch cet appareil fut évalué comme Arpin Mk 2 à Old Sarum (School of Army Co-operation) en décembre 1939 comme avion d’observation d’artillerie (AOP). On lui préféra le Taylorcraft Plus D à aile haute, qui deviendra l'Auster AOP. * Portail de l’aéronautique (fr) アーピン A-1（Arpin A-1）は、プッシャー方式の単発低翼単葉機である。キャビン後部の2本のブームの間に星型エンジンを後ろ向きに搭載し、通常とは異なる固定の首車輪式降着装置を備えていた。1機のみ製作。 (ja)
climb rate ftmin	600 (xsd:integer)
climb rate ms	3 (xsd:integer)
cruise speed kmh	153 (xsd:integer)
cruise speed mph	95 (xsd:integer)
empty weight kg	336 (xsd:integer)
empty weight lb	740 (xsd:integer)
endurance	18000.0 (second)
eng1 hp	68 (xsd:integer)
eng1 kw	51 (xsd:integer)
eng1 name	British Salmson AD.9R 9-cylinder air cooled geared radial engine (en)
eng1 number	1 (xsd:integer)
gross weight kg	573 (xsd:integer)
gross weight lb	1261 (xsd:integer)
height m	2.130000 (xsd:double)
length in	2 (xsd:integer)
length m	7.060000 (xsd:double)
max speed kmh	173 (xsd:integer)
max speed mph	108 (xsd:integer)
produced	1 (xsd:integer)

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