Drive for artificial space flight body using thermal arc

The drive (10) forms a modular component of a thermal arcing system (12) and has a drive material supply (14) and a controller (16) containing a switchable parallel mass flow controller (24) having valves (26,28). A gas generator is disposed between the supply and mass flow controller. The controlle...

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Bibliographische Detailangaben
Hauptverfasser:	RIEHLE, MARTIN., 70563 STUTTGART, DE, ZUBE, DIETER.., BOTHELL, WASH., US, MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS HEATING 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 drive (10) forms a modular component of a thermal arcing system (12) and has a drive material supply (14) and a controller (16) containing a switchable parallel mass flow controller (24) having valves (26,28). A gas generator is disposed between the supply and mass flow controller. The controller is operated by a computer (40), to which an independent processor (42) is coupled.