Aerospace
Technical Paper

Spacecraft Two-Phase Thermal Control System Simulation

972535

7/1/1997

Event
International Conference On Environmental Systems
Authors
Vladimir V. Malozemov Moscow State Aviation Institute
Natalia S. Kudriavtseva Moscow State Aviation Institute
Abstract
Content
The results of computer simulation of a typical spacecraft pumped two-phase thermal control system are presented. The two-phase thermal control system transients under effect of the typical disturbances are obtained. The system dynamic characteristics are analyzed and influence of design parameters on the quality of system dynamic processes are discussed.
Meta Tags
Topics
Computer simulation
Control systems
Spacecraft
Simulation and modeling
Affiliated or Co-Author
Moscow State Aviation Institute
Details
DOI
https://doi.org/10.4271/972535
Citation
Malozemov, V. and Kudriavtseva, N., "Spacecraft Two-Phase Thermal Control System Simulation," International Conference On Environmental Systems, Lake Tahoe, Nevada, United States, July 14, 1997, https://doi.org/10.4271/972535.
Additional Details
Publisher
SAE International
Published
7/1/1997
Product Code
972535
Content Type
Technical Paper
Language
English