Accession Number : AD0422763
Title : TEMPERATURE CONTROL SYSTEMS FOR SPACE VEHICLES,
Corporate Author : NORTH AMERICAN AVIATION INC DOWNEY CA
Personal Author(s) : Honea, F. I.
Report Date : SEP 1963
Pagination or Media Count : 285
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)
Descriptors : *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.
Distribution Statement : APPROVED FOR PUBLIC RELEASE