Supersonic Transport Fluid Evaluation Program

650328

02/01/1965

Event
Aerospace Fluid Power Systems and Equipment Conference
Authors Abstract
Content
With the imminent development of the United States Mach 3 Supersonic Transport (SST), aircraft hydraulic fluid state-of-the-art must take another step forward to meet system performance requirements combined with high temperature environments.
This paper presents results of pumping tests conducted by Douglas Aircraft Company, Inc., on 18 different chemical types of proposed SST hydraulic fluids comprising 50 different fluid combinations. Pump and fluid performance data are presented for all 50 fluids evaluated. A general discussion of fluid properties versus performance is also provided.
Four specific fluid types are considered the best SST hydraulic fluid contenders. They are: chlorosilicone, mineral oil (super refined), perfluoroalkyl, and polyaryl.
Meta TagsDetails
DOI
https://doi.org/10.4271/650328
Pages
18
Citation
Galloway, C., "Supersonic Transport Fluid Evaluation Program," SAE Technical Paper 650328, 1965, https://doi.org/10.4271/650328.
Additional Details
Publisher
Published
Feb 1, 1965
Product Code
650328
Content Type
Technical Paper
Language
English