Schweizer SGS 1-29
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Original source: Own work Author Dudley0415 [edit] Licensing I, the copyright holder of this work, hereby publish it under the following license: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
Author: Dudley0415 [edit] Licensing I, the copyright holder of this work, hereby publish it under the following license: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work

The Schweizer SGS 1-29 is a United States 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.

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Made by Schweizer Aircraft.

Empty Weight Lb
465
Wing Area Sqm
15
Designer
Schweizer brothers
Lists
*List of experimental aircraft*List of gliders
Aspect Ratio
16
Origin
United States
Wing Profile
NACA 63-618
Glide Ratio
3120.0
Gross Weight Lb
750
Sink Rate Ms
1
Number Built
1
Crew
One
Empty Weight Kg
224
Gross Weight Kg
340
Span M
15
Sink Rate Ftmin
123
Manufacturer
First Flight
1958
Span In
3
Span Ft
49
National Origin
United States
Wing Area Sqft
154
Met Or Eng
eng
Category

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