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High Thrust-Density Electrostaic Engines Project
<p>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; flight costs are amortized over multiple users.&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</p>
Complete Metadata
| bureauCode |
[ "026:00" ] |
|---|---|
| identifier | TECHPORT_14697 |
| issued | 2014-04-01 |
| landingPage | http://techport.nasa.gov/view/14697 |
| programCode |
[ "026:000" ] |
| 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 |
