A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) with integrated fluidic channels receives energy from a solar concentrator (320) and stores the heat.
Thermal Capacitor Block with Integrated Fluidic Channels
2024-01-25
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
THERMAL CAPACITOR BLOCK WITH INTEGRATED FLUIDIC CHANNELS
European Patent Office | 2022
|Fabrication and electrical characterization of integrated nano-scale fluidic channels
British Library Online Contents | 2011
|Integrated Dynamic Fluidic Lens Actuation
British Library Conference Proceedings | 2004
|Integrated dynamic fluidic lens actuation
IEEE | 2004
|Confinement-Induced Diffusive Sound Transport in Nanoscale Fluidic Channels
DataCite | 2023
|