The Landing Gear of the Lockheed SST

650224

02/01/1965

Authors Abstract
Content
The landing gear of the Lockheed Model L-2000 supersonic transport is described as a vital element of the overall configuration of the airplane, considering the sometimes conflicting demands for safety, simplicity, long service life, small frontal area, and low pavement loading. The choice of six wheels for each main gear is explained, as is the selection of titanium alloy and high heat-treat steel as the principal structural materials. The nose gear steering system and the wheel well cooling systems are described, together with criteria for tires, wheels, and brakes.
Meta TagsDetails
DOI
https://doi.org/10.4271/650224
Pages
10
Citation
Carter, K., "The Landing Gear of the Lockheed SST," SAE Technical Paper 650224, 1965, https://doi.org/10.4271/650224.
Additional Details
Publisher
Published
Feb 1, 1965
Product Code
650224
Content Type
Technical Paper
Language
English