MEASURES OF PILOT RESPONSE TO A CHANGING THERMAL LOAD UNDER PROTECTED AND UNPROTECTED CONDITIONS
Abstract
A series of test exposures of pilot subjects to the simulated thermal environment of a very high performance aircraft cockpit are reported herein. The effectiveness of a current ventilated, full-pressure suit was tested in terms of its capability for successfully protecting the pilot subjects from the experimental temperature profile. Detailed physiological and performance data for the subjects under both test and control conditions are presented, as is a description of the numerous instrumentation problems posed by the dynamic simulation of cockpit thermal conditions. The tests were restricted to a rather small sample of subjects, but there are indications that some peculiar physiological reactions to changing temperature profile may set a different level of tolerance than that shown for steady temperature states.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 08, 1959
- Accession Number
- AD0834037
Entities
People
- E. G. Aiken
- R. C. Armstrong
- W. L. Wu
Organizations
- General Dynamics