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The Schweizer SGS 1-29 is an American single-seat, mid-wing, experimental laminar flow airfoil glider built by Schweizer Aircraft of Elmira, New York. The 1-29 is a development of the Schweizer SGS 1-23 that utilizes a 1-23 fuselage and a newly constructed set of 49.2 foot (15.0 m) span wings. The aircraft was constructed to study the feasibility of producing improved boundary layer laminar flow on a metal-winged sailplane. Only one SGS 1-29 was produced and the project was not pursued further.

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dbo:abstract
  • The Schweizer SGS 1-29 is an American single-seat, mid-wing, experimental laminar flow airfoil glider built by Schweizer Aircraft of Elmira, New York. The 1-29 is a development of the Schweizer SGS 1-23 that utilizes a 1-23 fuselage and a newly constructed set of 49.2 foot (15.0 m) span wings. The aircraft was constructed to study the feasibility of producing improved boundary layer laminar flow on a metal-winged sailplane. Only one SGS 1-29 was produced and the project was not pursued further. (en)
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dbo:manufacturer
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  • 1 (xsd:nonNegativeInteger)
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dbp:airfoil
  • NACA 63-618 (en)
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  • 15.750000 (xsd:double)
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  • One (en)
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  • 224 (xsd:integer)
dbp:emptyWeightLb
  • 465 (xsd:integer)
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  • 1958 (xsd:integer)
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  • 34 (xsd:integer)
dbp:grossWeightKg
  • 340 (xsd:integer)
dbp:grossWeightLb
  • 750 (xsd:integer)
dbp:lists
  • *List of experimental aircraft *List of gliders (en)
dbp:manufacturer
dbp:nationalOrigin
  • United States (en)
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  • 1 (xsd:integer)
dbp:primeUnits?_
  • imp (en)
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  • 123 (xsd:integer)
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  • 0.630000 (xsd:double)
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  • 49 (xsd:integer)
dbp:spanIn
  • 3 (xsd:integer)
dbp:spanM
  • 15 (xsd:integer)
dbp:type
  • Experimental Standard-class sailplane (en)
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  • 154 (xsd:integer)
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  • 15.300000 (xsd:double)
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rdfs:comment
  • The Schweizer SGS 1-29 is an American single-seat, mid-wing, experimental laminar flow airfoil glider built by Schweizer Aircraft of Elmira, New York. The 1-29 is a development of the Schweizer SGS 1-23 that utilizes a 1-23 fuselage and a newly constructed set of 49.2 foot (15.0 m) span wings. The aircraft was constructed to study the feasibility of producing improved boundary layer laminar flow on a metal-winged sailplane. Only one SGS 1-29 was produced and the project was not pursued further. (en)
rdfs:label
  • Schweizer SGS 1-29 (en)
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