About: Akaflieg Braunschweig SB-11

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The Akaflieg Braunschweig SB-11 is an experimental, single seat, variable geometry sailplane designed by aeronautical students in Germany. It won the 15 m span class at the World Gliding Championships of 1978 but its advances over the best, more conventional, opposition were not sufficient to lead to widespread imitation.

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-11 (en)
rdfs:comment	The Akaflieg Braunschweig SB-11 is an experimental, single seat, variable geometry sailplane designed by aeronautical students in Germany. It won the 15 m span class at the World Gliding Championships of 1978 but its advances over the best, more conventional, opposition were not sufficient to lead to widespread imitation. (en)
dcterms:subject	1970s German sailplanes Akaflieg Braunschweig aircraft Aircraft first flown in 1978
Wikipage page ID	34571436 (xsd:integer)
Wikipage revision ID	1083039002 (xsd:integer)
Link from a Wikipage to another Wikipage	Carbon-fiber-reinforced polymer Schempp-Hirth Janus Schleicher ASW 20 Monowheel Sailplane Châteauroux Camber (aerodynamics) Shoulder wing Stall (flight) Empennage Helmut Reichmann Wingspan Fuselage Ailerons Akaflieg München Mü27 Akaflieg Akaflieg Darmstadt D-40 1970s German sailplanes Akaflieg Braunschweig aircraft Fin Fowler flaps Trailing edge Flap (aircraft) Aircraft first flown in 1978 Chord (aircraft) Landing gear Induced drag Air brake (aircraft) Akaflieg Stuttgart FS-29 Aspect ratio (wing) Operation Sigma Sigma Rudder Schempp-Hirth Experimental aircraft Dihedral (aircraft) Wing loading T-tail Stabilator
Link from a Wikipage to an external page	http://www.akaflieg-braunschweig.de/prototypen/sb11/
sameAs	Akaflieg Braunschweig SB-11 Akaflieg Braunschweig SB-11 Akaflieg Braunschweig SB-11 Akaflieg Braunschweig SB-11
sink rate ms	0.670000 (xsd:double)
sink rate note	minimum; flaps retracted, this is at 104 kmh with flaps extended at 85 kmh (en)
span m	15 (xsd:integer)
stall speed kmh	75 (xsd:integer)
stall speed note	flaps retracted; 58 kmh flaps extended (en)
wing area note	with flaps retracted; 13.2 m² flaps extended (en)
wing area sqm	10.560000 (xsd:double)
wing loading kg/m	44.500000 (xsd:double)
wing loading note	at 470 kg with flaps retracted; 35.06 kg/m³ flaps extended (en)
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	1978 (xsd:integer)
national origin	Germany (en)
crew	1 (xsd:integer)
group	Notes (en)
manufacturer	Akaflieg
ref	Sailplanes 1965-2000 (en)
type	Experimental single seat sailplane (en)
has abstract	The Akaflieg Braunschweig SB-11 is an experimental, single seat, variable geometry sailplane designed by aeronautical students in Germany. It won the 15 m span class at the World Gliding Championships of 1978 but its advances over the best, more conventional, opposition were not sufficient to lead to widespread imitation. (en)
airfoil	Wortmann HQ - 144 - 39 W3 (en)
aspect ratio	21.300000 (xsd:double)
empty weight kg	270 (xsd:integer)
glide ratio	best 1:41 at 104 kmh flaps retracted; 1:36 at 85 kmh flaps extended (en)
gross weight kg	340 (xsd:integer)
gross weight note	(en)
length m	7.405000 (xsd:double)
max speed kmh	265 (xsd:integer)
max speed note	flaps retracted; 140 kmh flaps extended (en)
number built	1 (xsd:integer)
gold:hypernym	Seat

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