Specifications
The thruster itself is in the 20-50 kW class, with a specific impulse of 6,000-9,000 seconds, and a propellant throughput capability exceeding 100 kg/kW. The goal of the project, as of June 2003, was to achieve a Technology readiness level of 4-5 within 2 years.
On page 8 of the September 2004 HiPEP report NASA/TM—2004-213194 says the pre-prototype HiPEP produced 670 mN of thrust at a power level of 39.3 kW using 7.0 mg/s of fuel giving a specific impulse of 9620 s. Downrated to 24.4 kW, the HiPEP used 5.6 mg/s of fuel giving a specific impulse of 8270 s and 460 mN of thrust.
Read more about this topic: High Power Electric Propulsion
Other articles related to "specifications":
Inter MUD - Intermud-3 - Software
... It is also possible to use the I3 specifications in order to create a custom implementation ... It is also possible to use the I3 specifications and the inter router network specifications in order to create a custom implementation ...
... It is also possible to use the I3 specifications in order to create a custom implementation ... It is also possible to use the I3 specifications and the inter router network specifications in order to create a custom implementation ...