Feasibility study of a low-temperature expandable megawatt pulse power radiator
Future space missions require development of lightweight, large-surface-area radiators. These conceptual systems are envisioned as generating waste heat in the form of pulses with peak-to-average power ratios of 10 super(4)-10 super(5). The present Note focuses on the definition of a "collectib...
Gespeichert in:
Veröffentlicht in: | Journal of spacecraft and rockets 1986-09, Vol.23 (5), p.539-541 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | Future space missions require development of lightweight, large-surface-area radiators. These conceptual systems are envisioned as generating waste heat in the form of pulses with peak-to-average power ratios of 10 super(4)-10 super(5). The present Note focuses on the definition of a "collectible" expendable concept. During the pulse, heat is removed directly from a high-power density component through flash or spray evaporation. The vapor generated is collected in an expandable, variable-volume, variable-surface-area radiator. The vapor is condensed within the radiator during an interpulse period and recirculated to the coolant reservoir to be recycled. |
---|---|
ISSN: | 0022-4650 1533-6794 |
DOI: | 10.2514/3.25842 |