A space flight body, in particular a satellite, is proposed, with a drive unit which is operated with hydrogen and oxygen and serves for a maneuvering of the space flight body, and with a fuel material generating device with at least one electrolyzer, which is configured for periodically generating hydrogen and oxygen and comprises at least one electrolysis cell having at least one alkaline electrolyte, wherein the fuel material generating device comprises at least one first storage tank for a storage of the generated hydrogen and at least one second storage tank for a storage of the generated oxygen, allowing the gas for at least one jet nozzle to be retrievable from the two storage tanks by the drive unit via a duct.
RAUMFLUGKÖRPER MIT EINER ANTRIEBSSTOFFERZEUGUNGSVORRICHTUNG
SPACE CRAFT HAVING A FUEL PRODUCTION APPARATUS
ENGIN SPATIAL AVEC UN APPAREIL DE PRODUCTION D'UN CARBURANT
2021-04-21
Patent
Electronic Resource
German
VERWENDUNG ZUMINDEST EINER SEKUNDÄRSTRUKTUR IN EINEM RAUMFLUGKÖRPER, RAUMFLUGKÖRPER UND VERFAHREN
European Patent Office | 2019
|Gyroskopie-Trägerstruktur, inertiale Raumflugkörper-Messeinheit und Raumflugkörper
European Patent Office | 2019
|TIBKAT | 1970
|Flugmechanische Probleme aerodynamischer Raumflugkörper
TIBKAT | 1967
|