000			04328nam a22004693i 4500
001			EBC3111636
003			MiAaPQ
005			20240729124524.0
006			m o d |
007			cr cnu||||||||
008			240724s1963 xx o ||||0 eng d
020			_a9781600862670 _q(electronic bk.)
020			_z9781563478581
035			_a(MiAaPQ)EBC3111636
035			_a(Au-PeEL)EBL3111636
035			_a(CaPaEBR)ebr10516741
035			_a(OCoLC)922978855
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aTL783.54 -- .A44 1962eb
082	0		_a629.4225
100	1		_aStuhlinger, Ernst.
245	1	0	_aElectric Propulsion Development.
250			_a1st ed.
264		1	_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c1963.
264		4	_c©1963.
300			_a1 online resource (762 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aProgress in Astronautics and Aeronautics
505	0		_aCover -- Title -- Copyright -- Electric Propulsion Committee -- Editorial Committee -- Preface -- Contents -- A. Electrothermal Propulsion -- Objectives and Design of a 1-kw Arc-Jet Engine for Space Flight Testing -- Development Work on Plasma Arc Jet Engines -- Arc Jet Engine Performance - Experiment and Theory IV -- Arc Jet Design -- Materials Problems Related to the Electric Arc Jets -- A Chemical Arc-Jet Rocket Feasibility Study -- Chemical Nonequilibrium Effects in Thermal Arc Jet Propulsion -- Magnetically Diffused Radial Electric-Arc Air Heater Employing Water-Cooled Copper Electrodes -- B. Electrostatic Propulsion -- Field Emission Microscope Study of the Kinetics of Cesium Layers on a Tungsten Surface -- Experimental Evaluation of Porous Materials for Surface lonization of Cesium and Potassium -- Experiments on Atom and Ion Emission From Porous Tungsten -- lonization, Emission, and Collision Processes in the Cesium Ion Engine -- Negative Iodine Formation on Metal Hexaboride Surfaces -- Electron Bombardment Ion Source -- Electron Transfer Discharge Ion Source -- In-Flight Generation of Fuel for Cesium Ion Engines: The Cesium Hydride System -- Corrosivity and Contamination of Cesium in Ion Propulsion -- Analysis of Neutralization Problems Using the Ion Accelerator Computer Program -- Neutralization of Ion Beams -- Onboard Colloidal Particle Generator for Electrostatic Engines -- Glycerol Droplets for Electrostatic Propulsion -- C. Electromagnetic Propulsion -- Plasma Thermodynamics II, Complex Equilibria in Nonideal Systems -- Three-Fluid Nonequilibrium Plasma Accelerators (Part 1) -- Characteristics of the Pinch Discharge in a Pulsed Plasma Accelerator -- Experimental Studies of a Repetitively Fired Two-Stage Coaxial Plasma Engine -- Plasma Propulsion by Means of a Helical Transmission Line -- Inductive High-Field Plasma Accelerators.
505	8		_aMeasurements of Impulse of a Pulsed Plasma Accelerator -- D. Space Testing and Space Missions -- Limitations on the Space Test of a Cesium Ion Engine at Altitudes Below 1500km -- Flight Test Concept for a Pulsed Plasma Pinch Engine -- Payload Optimization for Power-Limited Vehicles -- Concept for a Manned Mars Expedition With Electrically Propelled Vehicles -- Nuclear Electric Spacecraft for Unmanned Planetary and Interplanetary Missions -- A Nuclear-Electric Spacebus for Planetary Landing Missions -- Potentialities of Air-Scooping Electrical Space Propulsion Systems -- Contributors to Volume 9.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aElectric rocket engines -- Congresses.
650		0	_aSpace vehicles -- Electric propulsion systems -- Congresses.
655		4	_aElectronic books.
776	0	8	_iPrint version: _aStuhlinger, Ernst _tElectric Propulsion Development _dReston : American Institute of Aeronautics and Astronautics,c1963 _z9781563478581
797	2		_aProQuest (Firm)
830		0	_aProgress in Astronautics and Aeronautics
856	4	0	_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111636 _zClick to View
999			_c68303 _d68303