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![]() Date: 2007-02-22 23:29:11Space technology Ion thruster Plasma Variable Specific Impulse Magnetoplasma Rocket Specific impulse Rocket engine Hall effect thruster Helicon Double Layer Thruster Electrically powered spacecraft propulsion Spacecraft propulsion Aerospace engineering Propulsion | Add to Reading List |
![]() | CAPCOM Issue 36: June 2009 VSSEC ENGINEERING AND SCIENCE CAREERS EXPODocID: 11XzI - View Document |
![]() | Plasma Adiabaticity in a Diverging Magnetic Nozzle IEPC[removed]Presented at the 33rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., USA October 6–10, 2013 J. P. SheeDocID: S0Hc - View Document |
![]() | JOURNAL OF PROPULSION AND POWER Vol. 27, No. 4, July–August 2011 Technical Notes Downloaded by UNIVERSITY OF MICHIGAN on February 28, 2013 | http://arc.aiaa.org | DOI: [removed]DocID: RXD6 - View Document |
![]() | Ambipolar ion acceleration in an expanding magnetic nozzleDocID: REAA - View Document |
![]() | Plasma Propulsion:Environment[removed]DocID: FqrF - View Document |