Hydraulic Power Units for Supersonic Aircraft

670529

02/01/1967

Event
Aerospace Systems Conference and Engineering Display
Authors Abstract
Content
The requirements of hydraulic power units for the Supersonic Transport are compared with those for present commercial aircraft and with the requirements that have been met in supersonic military applications Trends in component power, speed, flow and other parameters, and their effects on component design are discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/670529
Pages
6
Citation
Lambeck, R., "Hydraulic Power Units for Supersonic Aircraft," SAE Technical Paper 670529, 1967, https://doi.org/10.4271/670529.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670529
Content Type
Technical Paper
Language
English