About: Akaflieg Braunschweig SB-12

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The Akaflieg Braunschweig SB-12 is a single seat, Standard Class sailplane designed around 1980 by German technical university students to test out a new wing profile from the German Aerospace Centre. It was not intended for production, but the sole SB-12 remains active in 2010.

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 settlement yago:Type105840188
rdfs:label	Akaflieg Braunschweig SB-12 (en)
rdfs:comment	The Akaflieg Braunschweig SB-12 is a single seat, Standard Class sailplane designed around 1980 by German technical university students to test out a new wing profile from the German Aerospace Centre. It was not intended for production, but the sole SB-12 remains active in 2010. (en)
dcterms:subject	1980s German sailplanes Akaflieg Braunschweig aircraft Aircraft first flown in 1980
Wikipage page ID	34796361 (xsd:integer)
Wikipage revision ID	1050893503 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Monowheel Elevator (aircraft) Germany Thickness-to-chord ratio Drum brake Fuselage German Aerospace Centre Ailerons Alps 1980s German sailplanes Akaflieg Braunschweig aircraft Fin Angle of incidence (aerodynamics) Glider (sailplane) Flap (aircraft) Aircraft first flown in 1980 Landing gear Cockpit Tailplane Spoiler (aeronautics) Fiberglass Air brake (aircraft) Canopy (aircraft) Rudder Dihedral (aircraft) T-tail dbr:Akaflieg_Braunschweig Carbon fibre Water ballast Standard Class
sameAs	Akaflieg Braunschweig SB-12 Akaflieg Braunschweig SB-12 Akaflieg Braunschweig SB-12 Akaflieg Braunschweig SB-12
sink rate ms	0.600000 (xsd:double)
sink rate note	minimum at 78 km/h and at an all-up weight of 310 kg (en)
span m	15 (xsd:integer)
wing area sqm	10.020000 (xsd:double)
wing loading kg/m	44.900000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Infobox_aircraft_type dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Aircraft_specs dbt:Akaflieg_Braunschweig_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1980-04-09 (xsd:date)
national origin	Germany
crew	1 (xsd:integer)
manufacturer	dbr:Akaflieg_Braunschweig
ref	Jane's All the World's Aircraft 1981/2 All performance figures estimated (en)
type	Experimental Standard Class sailplane (en)
has abstract	The Akaflieg Braunschweig SB-12 is a single seat, Standard Class sailplane designed around 1980 by German technical university students to test out a new wing profile from the German Aerospace Centre. It was not intended for production, but the sole SB-12 remains active in 2010. (en)
airfoil	DFVLR HQ 014, thickness-to-chord ratio 18.43% (en)
aspect ratio	22.500000 (xsd:double)
empty weight kg	220 (xsd:integer)
glide ratio	42 (xsd:integer)
height m	1.400000 (xsd:double)
length m	6.400000 (xsd:double)
max speed kmh	250 (xsd:integer)
max speed note	smooth air (en)
max takeoff weight kg	450 (xsd:integer)
number built	1 (xsd:integer)
gold:hypernym	Seat
prov:wasDerivedFrom	wikipedia-en:Akaflieg_Braunschweig_SB-12?oldid=1050893503&ns=0
page length (characters) of wiki page	6338 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
manufacturer	dbr:Akaflieg_Braunschweig
origin	Germany
type	Standard Class
foaf:isPrimaryTopicOf	wikipedia-en:Akaflieg_Braunschweig_SB-12
is Link from a Wikipage to another Wikipage of	List of aircraft (Ai–Am) List of gliders (A) 1980 in aviation
is foaf:primaryTopic of	wikipedia-en:Akaflieg_Braunschweig_SB-12

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