Hybrid Radiator for Spacecraft Thermal Control Systems

Hybrid Radiator for Spacecraft Thermal Control Systems

A radiator with a two-layer hybrid structure is proposed for thermal control systems in spacecraft. Mathematical modeling confirms the efficiency of the emitting surface. On that basis, without loss of reliability, the heat pipes may be eliminated, and consequently the radiator mass is significantly...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Russian engineering research 2022, Vol.42 (1), p.57-59
Hauptverfasser: Belyavskii, A. E., Kudryavtseva, N. S., Sorokin, A. E.
Format: Artikel
Sprache:eng
Schlagworte:
Engineering
Engineering Design
Heat pipes
Hybrid structures
Radiators
Spacecraft
Thermal control systems
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:A radiator with a two-layer hybrid structure is proposed for thermal control systems in spacecraft. Mathematical modeling confirms the efficiency of the emitting surface. On that basis, without loss of reliability, the heat pipes may be eliminated, and consequently the radiator mass is significantly decreased.
ISSN:1068-798X
1934-8088
DOI:10.3103/S1068798X22010038