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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