{"@type": "dcat:Dataset", "accessLevel": "public", "bureauCode": ["026:00"], "contactPoint": {"@type": "vcard:Contact", "fn": "Michael Patterson", "hasEmail": "mailto:michael.s.patterson@faa.gov"}, "description": "&lt;p&gt;These issues are addressable by: increasing the thrust, power, and thrust-to-power ratio capability of EP systems; reducing the non-recurring engineering systems costs; and developing system architectures with performance characteristics that capture the broadest possible range of missions so that development &amp;amp; flight costs are amortized over multiple users.&amp;nbsp; We believe these objectives can be achieved by developing the Next Generation Electric Propulsion Thruster (NGEPT); a GRC-patented modular EP device based on a new arrangement of relatively mature and proven technologies with the potential to yield revolutionary capabilities&lt;/p&gt;", "distribution": [{"@type": "dcat:Distribution", "downloadURL": "http://techport.nasa.gov/xml-api/14697", "format": "XML", "mediaType": "application/xml"}], "identifier": "TECHPORT_14697", "issued": "2014-04-01", "keyword": ["completed", "glenn-research-center", "project"], "landingPage": "http://techport.nasa.gov/view/14697", "modified": "2025-04-01", "programCode": ["026:000"], "publisher": {"@type": "org:Organization", "name": "Space Technology Mission Directorate"}, "references": ["http://techport.nasa.gov/doc/home/TechPort_Advanced_Search.pdf", "http://techport.nasa.gov/fetchFile?objectId=3447", "http://techport.nasa.gov/fetchFile?objectId=3448", "http://techport.nasa.gov/fetchFile?objectId=3456", "http://techport.nasa.gov/fetchFile?objectId=6560", "http://techport.nasa.gov/fetchFile?objectId=6561", "http://techport.nasa.gov/fetchFile?objectId=6584", "http://techport.nasa.gov/home"], "temporal": "2014-04-01T00:00:00Z/2014-09-01T00:00:00Z", "title": "High Thrust-Density Electrostaic Engines Project"}