SGS 1-29 Schweizer   


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General Details
Manufacturer: Schweizer
Plane Name:

SGS 1-29

Classified as: Unclassified
Country Of Origin: U S A
Designer: Ernest Schweizer
No. of Seats 1
No. Built 1
   
Performance:
L/DMax: 34 84 kph / 45 kt / 52 mph
   
MinSink: 0.62 m/s / 2.05 fps / 1.21 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
15 49.2 14.29 153.8 224 465 116 255 340 750 23.79 4.87 0 0
Aspect ratio: 15.75
Airfoil: NACA 63-618
Structure: all metal
Engine:

Comment:
Only one 1-29 was built and has subsequently been presented to the National Soaring Museum. It consists of a modified 1-23G fuselage and tail with the addition of a constant chord, laminar-flow airfoil wing and balanced dive brakes. The wing ribs are indentical, made from one master die to help ensure laminar flow. It has flush, counter-sunk rivets, and the heavy, deep spar helps to reduce elastic wing deflections and minimize skin oil-canning.


           

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