A PROPULSION SYSTEM

The present invention relates to a propulsion system for a spacecraft comprising at least one electrical propulsion engine comprising at least one neutraliser; and a pressurant gas system comprising a pressurant gas; wherein the pressurant gas is fed directly into the at least one neutraliser. La pr...

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Bibliographische Detailangaben
Hauptverfasser:	GIANNETTI, Vittorio, GRAY, Howard, SADLER, James Edward
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	The present invention relates to a propulsion system for a spacecraft comprising at least one electrical propulsion engine comprising at least one neutraliser; and a pressurant gas system comprising a pressurant gas; wherein the pressurant gas is fed directly into the at least one neutraliser. La présente invention concerne un système de propulsion pour un engin spatial comprenant au moins un moteur de propulsion électrique comprenant au moins un neutraliseur; et un système de gaz de chasse comprenant un gaz de chasse; ledit gaz de chasse étant introduit directement dans l'au moins un neutraliseur.