Accession Number:

AD0422763

Title:

TEMPERATURE CONTROL SYSTEMS FOR SPACE VEHICLES,

Descriptive Note:

Corporate Author:

NORTH AMERICAN AVIATION INC DOWNEY CA

Personal Author(s):

Report Date:

1963-09-01

Pagination or Media Count:

285.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE