Electro-chemical hybrid power space thruster

The invention discloses an electro-chemical hybrid power space thruster which comprises a shell, an insulating heat-insulating sleeve, a spring, a low-voltage cathode, an electronic control solid propellant, a low-voltage anode, an insulating plate, a high-voltage anode, an electric propulsion prope...

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Bibliographische Detailangaben
Hauptverfasser:	SHEN RUIQI, BAO LIRONG, WANG ZHIWEN, ZHANG WEI, XIANG SHUJIE, WANG HUI, XIE HAIMING
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING CHEMISTRY COMBUSTION ENGINES EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS GAS-ATTACK COMPOSITIONS GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART) HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES FOR LIQUIDS MANUFACTURE THEREOF MATCHES MEANS FOR GENERATING SMOKE OR MIST MECHANICAL ENGINEERING METALLURGY OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER USE OF SINGLE SUBSTANCES AS EXPLOSIVES WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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