TEMPERATURE CONTROL SYSTEMS FOR SPACE VEHICLES,

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Abstract:

Methods of dynamic response analysis for space vehicle temperature control systems are described, including mathematical equations, tables, graphs, and an example analysis. A procedure for design of systems, including selection of control methods, coolants, and components and design analysis, is also included. Also included is a continuation of some topics from Part I and a description of special temperature control problems associated with precision temperature control, cryogenic cooling and reentry. Conclusions and recommendations are included to show areas which need investigation and further study. Author

Author(s):
Honea, F. I.
Author Organization(s):
NORTH AMERICAN AVIATION INC DOWNEY CA
Pagination:
0285

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
62 1449, ASD-TDR-62-493-PT-2
Contract/Grant Number(s):
AF33 657 8953
Task Number(s):
614609
Project Number(s):
6146
Monitor Series:
TDR-62-493-PT-2
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*TEMPERATURE CONTROL, *CONTROL SYSTEMS, SPACECRAFT, TEMPERATURE, CONFIGURATIONS, MATHEMATICAL ANALYSIS, TABLES(DATA), COOLANTS, LIQUID COOLING, HEAT TRANSFER, HEAT EXCHANGERS, ABSORPTION, THERMAL INSULATION, AUTOMATIC, INFRARED DETECTORS, CRYOGENICS, COOLING
Report Date:
1963 Sep 01