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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| creator | RIEHLE, MARTIN., 70563 STUTTGART, DE ZUBE, DIETER.., BOTHELL, WASH., US MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE |
| description | 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. |
| format | Patent |
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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.</description><edition>6</edition><language>eng ; ger</language><subject>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</subject><creationdate>1999</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19990114&DB=EPODOC&CC=DE&NR=19729471A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19990114&DB=EPODOC&CC=DE&NR=19729471A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RIEHLE, MARTIN., 70563 STUTTGART, DE</creatorcontrib><creatorcontrib>ZUBE, DIETER.., BOTHELL, WASH., US</creatorcontrib><creatorcontrib>MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE</creatorcontrib><title>Drive for artificial space flight body using thermal arc</title><description>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.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES FOR LIQUIDS</subject><subject>MECHANICAL ENGINEERING</subject><subject>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR</subject><subject>PRODUCING MECHANICAL POWER</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>WEAPONS</subject><subject>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1999</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBwKcosS1VIyy9SSCwqyUzLTM5MzFEoLkhMBgrmZKZnlCgk5adUKpQWZ-alK5RkpBblAuUTi5J5GFjTEnOKU3mhNDeDoptriLOHbmpBfnwq2IC81JJ4F1dDS3MjSxNzQ0dDY2LUAADlQi37</recordid><startdate>19990114</startdate><enddate>19990114</enddate><creator>RIEHLE, MARTIN., 70563 STUTTGART, DE</creator><creator>ZUBE, DIETER.., BOTHELL, WASH., US</creator><creator>MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE</creator><scope>EVB</scope></search><sort><creationdate>19990114</creationdate><title>Drive for artificial space flight body using thermal arc</title><author>RIEHLE, MARTIN., 70563 STUTTGART, DE ; ZUBE, DIETER.., BOTHELL, WASH., US ; MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE19729471A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>1999</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES FOR LIQUIDS</topic><topic>MECHANICAL ENGINEERING</topic><topic>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR</topic><topic>PRODUCING MECHANICAL POWER</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>WEAPONS</topic><topic>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</topic><toplevel>online_resources</toplevel><creatorcontrib>RIEHLE, MARTIN., 70563 STUTTGART, DE</creatorcontrib><creatorcontrib>ZUBE, DIETER.., BOTHELL, WASH., US</creatorcontrib><creatorcontrib>MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RIEHLE, MARTIN., 70563 STUTTGART, DE</au><au>ZUBE, DIETER.., BOTHELL, WASH., US</au><au>MESSERSCHMID, ERNST, DR., 72766 REUTLINGEN, DE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Drive for artificial space flight body using thermal arc</title><date>1999-01-14</date><risdate>1999</risdate><abstract>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.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
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| language | eng ; ger |
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| subjects | 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 |
| title | Drive for artificial space flight body using thermal arc |
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