The calculation of the heat control accumulator volume of two-phase heat transfer loop of a spacecraft thermal control system
Spacecraft thermal control systems based on two-phase mechanically pumped loops have advantages in terms of mass and power consumption for auxiliary needs compared to single-phase thermal control systems. However, the disadvantage of two-phase mechanically pumped loops is that when changing the heat...
Guardado en:
| Autores principales: | , , |
|---|---|
| Formato: | article |
| Lenguaje: | EN RU UK |
| Publicado: |
National Aerospace University «Kharkiv Aviation Institute»
2021
|
| Materias: | |
| Acceso en línea: | https://doaj.org/article/fb28130972eb4717be30b770fa752bf2 |
| Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|