AUTOMATIC TEMPERATURE CONTROL FOR LIQUID-COOLED FLIGHT SUITS.

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Abstract:

An automatic control system for maintaining constancy of skin temperature T sub s has been shown to be feasible by using special sensors to detect changes in T sub s and proportional fluid amplifiers to regulate the temperature of water flowing through the tubing of a water-cooled undergarment. Tests have indicated the response of the system when T sub s increased due to exercise or to an external heat load. Author

Author(s):
Merrill, Glen L. ; Starr, James B.
Author Organization(s):
HONEYWELL INC ST PAUL MINN RESEARCH DEPT
Descriptive Note:
Final rept. Jun 66-Mar 67,
Pagination:
0083

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
12045-FR1, NADC-AC-6702
Contract/Grant Number(s):
N156-48547
Task Number(s):
MF02202026001
Monitor Series:
6702
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*FLIGHT CLOTHING, TEMPERATURE CONTROL, AUTOMATIC, LIQUID COOLING, FLUID AMPLIFIERS, DETECTORS, SKIN(ANATOMY), SURFACE TEMPERATURE, WATER, CONTROL SYSTEMS
Field(s)/Group(s):
Protective Equipment
Report Date:
1967 Aug 03