STRUCTURAL PROPELLANT FOR ION ROCKETS (SPIR)

Systems, methods, and apparatus for a structural propellant for ion rockets (SPIR) are disclosed. A method for in-space propulsion of a spacecraft involves removing, by a removal device, a portion of a structure of the spacecraft. The method further involves feeding, by the removal device, the porti...

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Bibliographische Detailangaben
Hauptverfasser:	CHILDRESS, Jamie J, KESSLER, Thomas L
Format:	Patent
Sprache:	eng ; fre ; 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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