1 s p December 2000 SUB Gottingen B 3387 Third International Conference on Spacecraft Propulsion October 2000 Cannes, Fr...
Description
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December 2000
SUB Gottingen
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215 089 200 2002 B 3387
Third International Conference on
Spacecraft Propulsion 10-13 October 2000 Cannes, France
Organised by: Le Centre National d'Etudes Spatiales (CNES) and The European Space Agency (ESA)
European Spate Agen
5
NASA Technology Investments in Electric Propulsion: New Directions in the New Millennium J. Sankovic et al.
7
Electric Propulsion Subsystem Development and Application in Russia G. Popov et al.
21
An Overview of Electric and Advanced Propulsion Activities in Japan K. Komurasaki et al.
27
Chemical Spacecraft Propulsion in ESA: Current Activities /. Kalsch
41
European Activities in Electric Propulsion G. Saccoccia
49
An Overview of the CNES Propulsion Program A. Cadiou
65
Electric and Chemical Propulsion at Alcatel Space P. Garnero et al.
73
Electric Propulsion Activities for Eurostar 3000 J-M. Stephan
81
Session 1: Chemical Propulsion Systems The Design, Development and In-orbit Performance of a Propulsion System for The SNAP-1 Nanosatellite D. Gibbon et al.
91
The Propulsion Subsystem of the CNES Microsatellite Product Line R. Salome
99
Suppression of Propellant Shift in the Cluster II Propulsion Subsystem M. Griffiths
107
IV
Spacecraft Propulsion Systems - An Overview of Fiat Avio Activities L. De Rose et al.
117
MON and MMH Pressure Surges for a Simplified Propellant Feed System C. Leca et al.
125
Propellant Gauging Method Applied on Astrium SAS Telecommunication Satellite L. Brouard et al.
131
Hydrazine Propulsion Systems with a Micropump F. Dugue et al.
139
A Generic Approach for Propulsion System Simulation. Application to Astrium Projects P. Cheoux-Damas et al. ESA Online Propulsion System and Component Database J. Herholz et al.
147
155
Session 2: Electric Propulsion Systems Plasma Propulsion Subsystem Lifetest - Alcatel X. Ragot and N. Mattei
167
Numerical Simulation of Xenon Mass Transfer S. d 'Halewyn et al.
173
Space Propulsion Activities at Centrospazio M. Andrenucci
179
Researching of Electric Propulsion Quick Start Problem for a Spacecraft Orientation System A. Loyan et al. x
181
Session 3: Advanced Propulsion Concepts A Fusion Propulsion System for Rapid Deep Space Missions T. Kammash
191
Single and Opposed-cavity Solar Thermal Thrusters Made of Single Crystal Tungsten H. Sahara et al.
195
Low-Power Solid-State Microwave Thruster Systems M. Micci
203
Numerical Computation of CW-laser Thruster Flows P. Molina-Morales et al.
211
V
The Concept of a Rocket Engine Using CO2/Metal Propellant for Mars Sample Return Missions /. Gokalp and E. Shafirovich
219
New Generation of Silicon Based Microthrusters for Space Application C. Rossi et al.
229
Space Propulsion by Laser for the Future A. Lebehot et al.
235
Session 4.1: Chemical Thrusters Earth Storable Bipropellant Thrusters for Geostationary Spacecraft G. Madhavan Nair et al.
245
Development of a Low-Cost 22N Thruster U. Gotzig
255
Catalytic Decomposition of Different Monopropellants R. Eloirdi et al.
263
Characterization in Endurance of the SNECMA IN Hydrazine Thruster C. Pavoine et al.
271
Properties of Supersonic Cold Gas Jets for Space Probe Moving A. Lebehot et al.
277
Session 4.2: Hall Thrusters An Overview of Plasma oscillations in Hall Thrusters E. Choueiri
287
Investigations of Low Frequency Oscillation Phenomena in a Hall Thruster T. Miyasaka et al.
305
Transients During Stationary Plasma Thruster Start-Up B. Arkhipov et al.
311
Transient Excitation and Behavior of a Closed Electron Drift Plasma Thrusters M. Prioul et al.
.317
1-D Performance Analysis of a Hall Thruster E. Ahedo et al.
323
Recent Results on Plasma Thrusters In France M. Lyszyk et al.
331
VI
PPS 1350 Plasma Thruster Subsystem Life Test P. Dumazert and S Lagardere-Verdier
341
Operating Conditions and Plasma Study of an ATON-class Hall thruster S. Roche et al.
351
Ion Energy Measurement of a D-55 Hall Thruster V. Garkusha et al.
359
Effects of the Secondary Electronic Emission on the Sheath Phenomenon in a Hall Thruster L. Jolivet and J.F. Roussel
367
Influence of the Plasma-wall Interactions on the Operation of Hall Thrusters K. Makowski et al.
377
Simulation of Plasma Dynamics in SPT A. Bishaev et al.
385
Low-power Hall Thruster with Specific Impulse up to 2000 Seconds and Above M. Belikov et al.
393
Small SPT Unit Development and Tests B. Arkhipov et al.
399
Session 4.3: Ion Thrusters The Potential Future Capabilities of Gridded Ion Thrusters D. Fearn
404
Grid Lifetime Model of a 3-grid Ion Engine M. Nakano and T. Tachibana
413
RF Ion Thruster Design Software Based on Numerical Modelling M. Closs
419
TheRIT15 Ion Engines - A Survey of the Present State of Radio Frequency Ion Thruster Technology and its Future Potentiality H. Leiter et al.
423
RITA Ion Propulsion for ARTEMIS - Lifetime Test Results R. Killinger et al.
433
Status of the RIT-XT High Performance RF-ion Thruster Development R. Killinger et al.
443
Vll
Jets and Sprays Emitted from Colloid Thrusters: Experiments and Modeling P. Lozano and M. Martinez-Sanchez
451
The Results of Numerical and Experimental Investigation of Low-Power Ion Thruster with Slit-Type Acceleration System 0. Gorshkov et al.
459
Design Status of Engineering Model of Microwave Discharge Electrostatic Thruster S. Satori et al
467
Micronewton Indium FEEP thrusters W. Steiger et al.
475
Session 4.4: MPD, Arcjet, PPT Numerical Analysis on Performance Improvement of Arcjet Thruster Using Applied Field T. Fujiwara et al.
485
Numerical Simulation of Coaxial Applied Field Magnetoplasmadynamic Thruster Configurations P. Nikrityuk and M. Auweter-Kurtz
493
Numerical Tools for the Simulation of the APPT behaviour: Arc Generation and Plasma Flow S. Elaskar et al.
501
High Efficiency Ablative Pulsed Plasma Thruster Characteristics N. Antropov et al.
509
Session 5: Propulsion Components Pyrovalves "Evolution" E. Le Floch et al.
519
Industrialisation of ATV Latch Valves (Low Pressure High Flow & Low Pressure Low Flow) E. Benoit and F. Lagier
527
The PEPT-230 Micro-satellite Propellant Tank Development D. Hasan et al.
535
New High Pressure Tank for Xenon Storage C. Le Floe 'h et al.
543
Vlll
Correlations Between Neutral Buoyancy Tests and CFD C. Figus and L. Ounougha
547
Update of Cold Gas Propulsion at MOOG R. Bzibziak
553
Power Supply and Control Equipment for Russian Stationary Plasma Thrusters for Propulsion Systems of Geostationary Communication Satellites V. Kim et al.
561
Development and Testing of Electronic Pressure Regulator (EPR) Assembly E. Freidl and W. Miiller
565
Development and Testing of the GOCE Proportional Xenon Feed System C. Edwards and D. Mundy
571
Proportional Flow Control Valve (PFCV) for Electric Propulsion Systems E. Bushway and R. Perini
579
The Hollow Cathode - A Versatile Component of Electric Thrusters D. Fearn and S. Patterson
587
Oxide Hollow Cathode Assembly for PPS1350 J.P. Bugeat et al.
595
High Power Processing Unit for Stationary Plasma Thruster H. Declercq et al.
601
Session 6: Spacecraft/thruster Interactions Spacecraft/thrusters Interaction: New Models for Chemical Propulsion C. Theroude et al.
609
Numerical and Experimental Investigation of Plumes Interacting with Satellite Walls J. Allegre et al.
619
Heat Transfer Measurements on a Plate Adjacent to a Bipropellant Thruster G. Dettleff
627
Dynamic Action of Hall Thruster's Jet on Spacecraft's Solar Arrays B. Arkhipov et al.
635
Spacecraft Contamination by Sputtered Products of the SPT Ceramic Isolator S. Khartov et al.
639
"Escape" Software Modeling Package for Forecasting the Electrostatic Charging of a Satellite with Electric Propulsion in the Ionosphere of Earth A. Plokhikh et al.
645
IX
Electric Propulsion Systems as Contributors of Microwave Interference Radiation K. Kirdyashev
653
The SMART-1 Electric Propulsion Diagnostic Package G. Matticari et al.
661
The Estimation of the Torque and Forces Arising due to Interaction of the Exhaust Plume with S/C Body A.G. Korsun
669
Plasma Plume/Spacecraft Interaction. State of the Art in Investigation Methodology E. Tverdokhlebova and A.G. Korsun
675
Modelling and Experimental Verification of Hall and Ion Thrusters at ESTEC M. Tajmar et al.
683
Plume Effects in Plasma Propulsion, an Overview of CNES Activities F. Damon
693
Session 7: Applications to New Missions Electric Propulsion for ESA Scientific and Earth Observation Missions J. Gonzalez et al.
703
Toward a Unified System Design for Future Missions with Electric Propulsion S. Geffroy et al.
711
Advanced Hall Electric Propulsion for Future In-Space Transportation.. S. Oleson and J. Sankovic
717
Preliminary Design of a Multi-purpose Space Platform for Missions to the Sun, Internal Planets of Solar System A. Glukhov
727
Control Strategies for Orbit Maintenance of Leo Small Satellites with FEEP S. Marcuccio et al.
733
FEEP Propulsion System for Microsatellites P. Bianco
741
RITA for Drag Compensation on GOCE H. Bassner et al.
749
Application of Pulsed Plasma Thrusters for Small Satellites N. Antropov et al.
757
Development of Propulsion Units for Small Spacecraft B. A. Arkhipov et al.
763
X
The GRACE Cold Gas Attitude and Orbit Control System M. Schelkle
769
Session 8: In-flight Experience TDF2 Satellite Propulsion System Passivation N. Fillet et al.
779
Session 9: Ground Testing Ion Energy, Ion Velocity and Thrust Vector Measurements for the SPT-140 Hall Thruster /. Pollard and E. Beiting
789
Laser Induced Fluorescence Measurements in Xenon Plasma Thrusters N. Dorval et al.
797
A High Power Electric Propulsion Test Facility M. Andrenucci et al.
799
Development of a Thrust Balance in the Micronewton Range J.P. Marque et al.
807
Poster session Numerical Modeling of the Behaviour of High Pressure Vessel Under an Hypervelocity Impact C. Maveyraud et al.
811
The Advanced Propulsion Concept of Minimal Cost Flights in Both Close and Deep Space x V. Vinogradov and V. Murashko
817
i
Impact of Near Wall Processes on Performance of Hall Thruster A. Zhakupov et al.
825
Hall Thruster with a Sectioned Conducting Channel A. Zhakupov et al.
827
Predicting Life of Kapton Coating Impinged by SPT Plasma Jet V. Arbatsky
829
Experimental Investigation of the Alternative Propellants for Stationary Plasma Thruster S. Khartov et al.
833
XI
Reactivity in Phase Vapor of Methylhydrazine in Synthetic Air H. Delalu et al.
837
Theoretical Design of Arcjet Nozzle for Effective Gas Acceleration A. Rybakov and S. Nesterenko
841
Distribution of Liquid Droplet Phase in Low-thrust Rocket Engine Plumes A. Nadiradze
845
Microwave Diagnostics of Plasma-wall Interaction in SPT Accelerating Chamber K. Kirdyashev and V. Brukhty
849
Analysis of Factors Influencing the SPT Starting Discharge Process S. Oghienko and A. Rybakov
855
Particle Simulation of the Main Chamber of a Kaufman-type Ion Thruster M. Jugroot and J. Harvey
861
Investigation of Local Plasma Parameter Distributions Along the SPT Accelerating Channel Under Different External Electric Circuit Parameters V. Kim et al.
865
Use of Electric Propulsion for Compensation of Atmospheric Drag Acceleration During Experiments on Space Materials Science A. Feonychev et al.
869
Measurements of Ion Velocity at the Exit of a Plasma Thruster by "Large" Probe A. Bugrova et al. ;
873
Spectral Characteristics of SPT-ATON Plasma Radiation A. Bishaev et al.
877
Investigation of Plasma Local Parameters in Near-Wall Field of Channel of Stationary Plasma Thruster of ATON Type (SPT-ATON) x A. Bugrova et al. \
881
Simplified Two-dimensional Model of Hall Thrusters L. Garrigues et al.
885
Modeling of the Plume of a Stationary Plasma Thruster J. Bareilles et al.
889
Effect of the Plasma Inhomogeneity on Ion Thruster Grid Performance M. Tartz et al.
893
Measurements of Xenon Ion Velocities of the SPT-140 Using Laser Induced Fluorescence E. Beiting and J. Pollard
897
xu UPS and PPS Effects on Satellites V. Perrin et al. -
901
Semi-empirical Method for Evaluation of a Xenon Operating Hall Thruster Erosion Rate Through Analysis of its Emission Spectra G. Karabadzhak et al.
909
Miniaturized Flow Control Valves J. Benoit
913
Demonstration A Software Tool for the Performance Evaluation of Spacecraft Propulsion Systems P. Erichsen
