2 edition of Performance of a quasi-steady, multi megawatt, coaxial plasma thruster found in the catalog.
Performance of a quasi-steady, multi megawatt, coaxial plasma thruster
1994 by Lewis Research Center, National Aeronautics and Space Administration, National Technical Information Service, distributor in [Cleveland, Ohio], [Springfield, Va .
Written in English
|Statement||Jay T. Scheuer ... [et al.].|
|Series||NASA contractor report -- 195311., NASA contractor report -- NASA CR-195311.|
|Contributions||Scheuer, Jay T., Lewis Research Center.|
|The Physical Object|
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Performance of a Quasi-Steady, Multi-Megawatt, Coaxial Plasma Thruster by Jay T. Scheuer, Kurt F. Schoenberg, Ivars Henins, Richard A. Gerwin, Ronald W. Moses Jr, Jose A. Garcia, and Robert F. Gribble Los Alamos National Laboratory, Los Alamos, NM Robert P.
Hoyt Aerospace and Energetics Research Program, University of Washington, Seattle. Get this from a library. Performance of a quasi-steady, multi megawatt, coaxial plasma thruster. coaxial plasma thruster book [Jay T Scheuer; Lewis Research Center.;].
Journal Article: Preliminary investigation of power flow and performance phenomena in a multi megawatt coaxial plasma thruster. Journal Article: A magnetically-nozzled, quasi-steady, multimegawatt, coaxial plasma thruster Title: A magnetically-nozzled, quasi-steady.
Performance of a quasi-steady, multi megawatt, coaxial plasma thruster eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA. Performance of a kW class applied field MPD thruster [electronic resource] / Maris A.
Mantenieks. Evaluation of low power hall thruster propulsion [microform] / David Manzella [et al.] Multi-axis thrust measurements of the EO-1 pulsed plasma thruster [microform] / Lynn Coaxial plasma thruster book.
Available in the National Library of Australia collection. Author: Lochte-Holtgreven, W; Format: Book; xvi, p. 23 cm. developing and testing quasi-steady MW-class MPD thrusters as a prelude to steady-state high power thruster tests.
This paper provides an overview of the GRC high power pulsed thruster test facility, and presents preliminary performance data for a quasi-steady baseline MPD thruster geometry. Nomenclature b = thrust coefficient.
A quasi-steady MPD thruster doesn’t fit for practical use in space, because of its weight and complicated system. And, conventional MPD thrusters were equipped with water-cooled coils which apply the magnetic field.
So, the thruster systems is complicated, because of increasing external systems, such as circulating pump and heater. designs for both quasi-steady (King and RudolphRudolph and egg ) and steady-state (Coomes et al.
Gilland et al. ) MPD thruster. Eﬀects of Power Supply Resonances in Onset Studies of Quasi-Steady MPD Thrusters and has been used in extensive studies of thruster performance,2,3 electrode erosion,10 and plasma properties. The dimensions of the thruster are shown in Fig.
For the experiments in this paper, the thruster was fed. In this research, in order to confirm the quasi-steady state in the operation of MPD thruster, the propulsion performance per discharging time was acquired using the power supply developed in the previous research.
As a result, time independence was observed after the discharge time of 1 ms and operation with high quasi-steady was confirmed. walls of the rocket core. High-temperature ceramic plasma-facing surfaces handle the thermal radiation: the principal heat transfer mechanism from the discharge.
The rocket uses a helicon plasma source [5,6] for efﬁcient plasma production in the ﬁrst stage. This plasma is energized further by an ion cyclotron heating (ICH) RF. Onset Voltage Hash and Anode Spots in Quasi-Steady Magnetoplasmadynamic Thrusters Luke Uribarri A Dissertation Presented to the Faculty which is observed in coaxial plasma accelerators such as the plasma focus [43,44].
at relevant wavelengths integrated over the length of a quasi-steady thruster pulse. Research focus: Professor Gallimore is an experimental plasma physicist who specializes in advanced spacecraft propulsion.
He has extensive experimental experience with a number of electric propulsion devices including multi-megawatt pulsed coaxial plasma accelerators, low power steady arcjets, and Hall thrusters. The Quasi-steady State Performance of a Solar-Biomass Hybrid Cooling System Boonrit Prasartkaew 1, * and S.
Kumar 2 1 Department of Mechanical Engineering, Faculty of Engineering, Rajamangala University of Technology Thunyaburi, Klong 6. This work presents a mean line analysis for the prediction of the performance and aerodynamic loss of axial flow impulse turbine wave energy extraction, which can be easily incorporated into the turbine design program.
The model is based on the momentum principle and the well-known Euler turbine equation. Predictions of torque, pressure drop, and turbine efficiency showed Cited by: 7.
Krypton ion thruster performance. MICHAEL PATTERSON and; GEORGE WILLIAMS, JR. Measurement of plasma parameters in the stationary plasma thruster (SPT) plume and its effect on spacecraft components First Page; PDF; PDF Plus; No Access The Air Force Phillips Laboratory multimegawatt quasi-steady MPD thruster facility.
SALVADOR. Performance under Reciprocating Flow In this section the turbine performance under reciprocating flow is estimated by quasi-steady analysis with Kand obtained in steady flow experiment. Whenaxial velocity vachangessinusoidallywith amplitude Vaandperiod Tw, is written as 05 sin, (12) where Va/UI, 2rct/Tw.
Thenmeanturbine efficiency is. The company specializes in the development of unique ultra-high performance plasma guns for use in fusion energy, plasma physics research, and industrial applications. The name HyperV comes from the word “HyperVelocity” and references the extremely high velocities achieved by plasma when formed and fired from the company's plasma guns.
Full text of "NASA Technical Reports Server (NTRS) Bibliography of Lewis Research Center technical publications announced in " See other formats. This banner text can have markup. web; books; video; audio; software; images; Toggle navigation. basic text on mpd thrusters. Spallation Neutron Source reaches megawatt power.
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Studylib. Abstract An array of diagnostic techniques was used to study anode steady self-field MPD thrusters. Quasi Steady-State Model for Power System Stability: Limitations, Analysis and a Remedy Xiaozhe Wang, Hsiao-Dong Chiang Cornell University Ithaca, NYUSA [email protected], [email protected] Abstract—The quasi steady-state (QSS) model tries to reach a good compromise between accuracy and efﬁciency in long-term stability by: 1.
Advanced Plasma Technology is a collection of 25 chapters on various aspects of plasma processes authored by well known plasma scientists.
We are convinced that this book will be of help to both students and researchers, in academia as well as in the industry. SE 39 th Place Bellevue, WA Phone: () Propagating Magnetic Wave Plasma Accelerator (PMWAC) for Deep Space Exploration Phase-I Final Report TABLE OF CONTENTS.
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Vol. 29, No. 12, pp.Printed in Great Britain /86 $+ Pergamon Journals Ltd. Heat transfer review of literature by: A novel transient rotor current control scheme is proposed in this paper for a doubly-fed induction generator (DFIG) equipped with a superconducting magnetic energy storage (SMES) device to enhance its transient voltage and frequency support capacity during grid faults.
We live in a complex, interactive, and increasingly borderless world in which our lives are impacted more than ever before by events occurring outside the sphere of our personal influence. A recycling application could consist in converting the waste power into electric power for a downstream electric propulsion thruster, or to boost the performance of the main electric propulsion thruster.
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