About: SNCASO SO.7010 Pégase

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

About: SNCASO SO.7010 Pégase Goto Sponge NotDistinct Permalink

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

http://dbpedia.demo.openlinksw.com/c/5aWuUEZqsu

The SNCASO SO.7010 Pégase was a six-passenger light transport aircraft developed in France immediately after World War II. It was powered by a pair of tandem-coupled V-8 engines but this power plant proved to be too troublesome for development to proceed.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	SNCASO SO-7010 Pégase (it) SNCASO SO.7010 Pégase (fr) SNCASO SO.7010 Pégase (en)
rdfs:comment	The SNCASO SO.7010 Pégase was a six-passenger light transport aircraft developed in France immediately after World War II. It was powered by a pair of tandem-coupled V-8 engines but this power plant proved to be too troublesome for development to proceed. (en) Le SNCASO SO.7010 Pégase est un avion de tourisme et d'affaires construit en France dans l'immédiat après-guerre. Il est demeuré à l'état de prototype. (fr) Lo SNCASO SO-7010 Pégase era un aereo da trasporto, progettato dal consorzio francese Société nationale des constructions aéronautiques du sud-ouest (SNCASO) nella seconda metà degli anni quaranta. Caratterizzato dall'inusuale configurazione bimotore che azionava una singola elica disposta all'estremità anteriore del velivolo, rimase allo stato di prototipo e non ebbe seguito produttivo. (it)
foaf:depiction
dct:subject	Sud-Ouest aircraft 1940s French civil aircraft
Wikipage page ID	44881043 (xsd:integer)
Wikipage revision ID	1008967512 (xsd:integer)
Link from a Wikipage to another Wikipage	Propeller (aircraft) Monoplane SNCASO Low wing Sud-Ouest aircraft Tandem Fuselage Drag (physics) Fin France Paris Crankcase Landing gear 1940s French civil aircraft Cantilever World War II Rudder V-8 engine dbr:Mathis_G.16 dbr:Mathis_G8 dbr:Mathis_G16
sameAs	SNCASO SO.7010 Pégase SNCASO SO.7010 Pégase SNCASO SO.7010 Pégase SNCASO SO.7010 Pégase SNCASO SO.7010 Pégase SNCASO SO.7010 Pégase
span m	14.750000 (xsd:double)
wing area sqm	33 (xsd:integer)
wing loading kg/m	88 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:SNCASO_aircraft dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/SO.7010_Pégase.png?width=300
dbp:primeUnits%3F_	met (en)
first flight	1948-02-27 (xsd:date)
national origin	France
capacity	Six passengers (en)
crew	Two (en)
designer	Lucien Servanty (en)
manufacturer	SNCASO
ref	Les avions Francais de 1944 a 1964, S.N.C.A.S.O. SO-7010 'Pégase', Jane's all the World's Aircraft 1947 (en)
retired	after 15 Flights (en)
type	Six seat passenger transport (en)
has abstract	The SNCASO SO.7010 Pégase was a six-passenger light transport aircraft developed in France immediately after World War II. It was powered by a pair of tandem-coupled V-8 engines but this power plant proved to be too troublesome for development to proceed. (en) Le SNCASO SO.7010 Pégase est un avion de tourisme et d'affaires construit en France dans l'immédiat après-guerre. Il est demeuré à l'état de prototype. (fr) Lo SNCASO SO-7010 Pégase era un aereo da trasporto, progettato dal consorzio francese Société nationale des constructions aéronautiques du sud-ouest (SNCASO) nella seconda metà degli anni quaranta. Caratterizzato dall'inusuale configurazione bimotore che azionava una singola elica disposta all'estremità anteriore del velivolo, rimase allo stato di prototipo e non ebbe seguito produttivo. (it)
ceiling m	5000 (xsd:integer)
cruise speed kmh	275 (xsd:integer)
empty weight kg	2048 (xsd:integer)
eng1 hp	400 (xsd:integer)
eng1 name	dbr:Mathis_G.16
eng1 number	1 (xsd:integer)
eng1 type	coupled V-8 air-cooled piston engines (en)
height m	4.400000 (xsd:double)
length m	11.120000 (xsd:double)
max speed kmh	300 (xsd:integer)
max takeoff weight kg	3050 (xsd:integer)
more power	(en)
number built	1 (xsd:integer)
power/mass	9.655000 (xsd:double)
prop blade number	3 (xsd:integer)
prop dia m	2.560000 (xsd:double)
prop name	variable pitch propeller (en)
range km	1250 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:SNCASO_SO.7010_Pégase?oldid=1008967512&ns=0
page length (characters) of wiki page	5939 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
manufacturer	SNCASO
origin	France
foaf:isPrimaryTopicOf	wikipedia-en:SNCASO_SO.7010_Pégase
is Link from a Wikipage to another Wikipage of	List of aircraft (Sn) List of civil aircraft Vega Model 2 Starliner SNCASO 1948 in aviation SNCASO SO.7010 Pegase SNCASO SO-7010 Sud-Ouest S.O.7010 Pégase
is Wikipage redirect of	SNCASO SO.7010 Pegase SNCASO SO-7010 Sud-Ouest S.O.7010 Pégase

Faceted Search & Find service v1.17_git147 as of Sep 06 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3331 as of Sep 2 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 58 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software