A heat transfer control structure includes: an outer shell having an outer surface and an inner surface, the outer shell being heated by airflow along the outer surface; an inner shell disposed opposed to the inner surface of the outer shell, the inner shell being configured to accommodate a payload therein; and a plate coupled to the inner shell such that the plate is opposed to the inner shell across a gap. The outer shell is coupled to the plate.
Heat transfer control structure, flying object and spacecraft with high heat resistance
26.11.2024
Patent
Elektronische Ressource
Englisch
HEAT TRANSFER CONTROL STRUCTURE, FLYING OBJECT AND SPACECRAFT WITH HIGH HEAT RESISTANCE
Europäisches Patentamt | 2021
|Power Transfer for Formation Flying Spacecraft
AIAA | 2006
|AIAA | 2003
|Linear Control of Spacecraft Formation Flying
British Library Conference Proceedings | 2000
|Robust Control of Spacecraft Formation Flying
Online Contents | 2007
|