DEVELOPMENT OF HIGH-TEMPERATURE HYDRAULIC FLUIDS

530259

01/01/1953

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
HYDRAULIC fluids for high-speed, high-altitude aircraft need to encompass the temperature range -65 F to 450 F and over. In addition, the other physical properties must be satisfactory.
Since none of the fluids now being used in hydraulic systems are completely satisfactory, the Air Force has instituted a research program designed to develop a fluid that is capable of meeting these severe requirements.
Of the fluids investigated, the silicates and the polysiloxanes are considered to have real possibilities, although both need further development work done on them to take care of certain deficiencies.
Meta TagsDetails
DOI
https://doi.org/10.4271/530259
Pages
10
Citation
Mosteller, J., and King, J., "DEVELOPMENT OF HIGH-TEMPERATURE HYDRAULIC FLUIDS," SAE Technical Paper 530259, 1953, https://doi.org/10.4271/530259.
Additional Details
Publisher
Published
Jan 1, 1953
Product Code
530259
Content Type
Technical Paper
Language
English