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Power requirements determined for high-power-density electric motors for electric aircraft propulsion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Johnson, Dexter Brown, Gerald V. |
| Copyright Year | 2005 |
| Description | Future advanced aircraft fueled by hydrogen are being developed to use electric drive systems instead of gas turbine engines for propulsion. Current conventional electric motor power densities cannot match those of today s gas turbine aircraft engines. However, if significant technological advances could be made in high-power-density motor development, the benefits of an electric propulsion system, such as the reduction of harmful emissions, could be realized. |
| File Size | 179140 |
| Page Count | 3 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050217395 |
| Archival Resource Key | ark:/13960/t9382b344 |
| Language | English |
| Publisher Date | 2005-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Electric Propulsion Fly By Wire Control Power Supplies Hydrogen Electric Motors Gas Turbine Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
