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DEVELOPMENT OF HIGH-TEMPERATURE HYDRAULIC FLUIDS
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English
Abstract
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.
Citation
Mosteller, J. and King, J., "DEVELOPMENT OF HIGH-TEMPERATURE HYDRAULIC FLUIDS," SAE Technical Paper 530259, 1953, https://doi.org/10.4271/530259.Also In
References
- Standard Oil Development Co. Fourth Quarterly Report July 1951 Contract AF 33(038) 14593
- “Dibasic Acid Esters, an Ester Type for Fluids and Lubricants,” Pennsylvania State College Report, PRL 3.49 Jan 51 Contract Nord 7958 (Task B).
- “Fluids, Lubricants, and Related Materials,” Pennsylvania State College Report, PRL 5.3 1953 Contract AF 33(038) 18193.
- “Fluids, Lubricants, and Related Materials,” Pennsylvania State College Report, PRL 5.3 June 52 Contract AF 33 (038) 18193
- “Fluids, Lubricants, and Related Materials,” Pennsylvania State College PRL Final Report September 1953 Contract AF 33(038) 18193
- “Development of High-Temperature Hydraulic Fluids,” California Research Corp. Contract AF 33(038)9831 Final Report dated January, 1951 Quarterly Reports :January, 1952, April, 1952, June, 1952, and September, 1952