3 June 2004
4 June 2004
| PROGRAM 4th INTERNATIONAL SPACECRAFT PROPULSION CONFERENCE |
| These papers are not online on the server, because they are not particularly interesting for our projects at the moment. They are on CD. |
2
June 2004
3 June 2004 4 June 2004 |
|
ESA
Spacecraft Propulsion Activities
G. Saccoccia |
|
An
Overview of the CNES Propulsion Program for Spacecraft
N. Pillet et al. |
|
Experience
and Lessons Learnt from SMART-1, the First European Electric Propulsion
Driven Space Probe
G.D. Racca |
|
The
Rosetta Propulsion System
D. Stramaccioni |
|
INTEGRAL
RCS: Launch Site Operations and In-orbit Behaviour
M. Pessana et al. |
|
End
of Life of SPOT1 - Behavior of the Propulsion System and AOCS Subsystem
during the Last Maneuver of De-orbitation
N. Pillet et al. |
|
Hydrazine
Operations at Near-Freezing Temperatures During the Ulysses Extended Mission
A. McGarry et al. |
|
SMART-1
Electric Propulsion Flight Experience: Main Working Group Findings
D. Estublier et al. |
|
All
Fuelled Up With No Place To Go - The Rosetta MMH Offload Campaign, Kourou
2003
C. Smith |
|
SMART-1:
Spacecraft/Thruster Interaction Data Analysis
J. Gonzalez del Amo et al. |
|
Flight
Validation of the Thermal Propellant Gauging Method used at EADS Astrium
L. Dandaleix et al. |
|
Eutelsat
2 FM4 Spacecraft End of Life Operations and Propulsion Passivation
F. Appaix et al. |
|
Ion
Propulsion-Satellite Interactions during the ARTEMIS Salvage Mission
R. Killinger et al. |
|
High
Altitude Simulation Test for High Expansion Ratio Nozzles
C. Oiknine |
|
Longitudinal
oscillations in Hall thrusters
S. Barral et al. |
|
Examination
of Hall Thruster Xe Ion Flow Features by Means of Fabry-Pérot Interferometry
N. Claire et al. |
|
Non-Intrusive
Characterization of the Hall Thruster Azimuthal Drift Current
C. Thomas et al. |
|
Characteristics
of the XHT-100 Low Power Hall Thruster Prototype
M. Andrenucci et al. |
|
Principles
of Hall Thruster Onboard Malfunction Diagnostics Based on Magnetic Field
Measurements of Plasma Currents
B. Rubin et al. |
|
Hall
Effect Thruster with High Specific Impulse
O. Gorshkov et al. |
|
Experimental
Characterisation of PPS®X000 ML
L. Jolivet et al. |
|
Smooth
Control of Electric Jet Propulsion
R. Chuyan et al. |
|
Gauging
Components for "State-of-the-art" Propellant Management on next Generation
Satellite Platforms
P. Van Put et al. |
|
Qualification
of a Flow Control Valve for 200N ATV Thruster: Development of European
1N FCV for Hydrazine Propulsion
E. Benoit et al |
|
Silicon
Pressure Sensors for Space Propulsion Applications
M. Nese et al |
|
Valves
Based on Amplified Piezoelectric Actuators
R. Le Letty et al. |
|
Development
Activities on an advance Propellant Flow Control Unit
G. Noci et al. |
|
Development
of an Advanced Proportional Xenon Feed Assembly for the GOCE Spacecraft
M. van der List et al. |
|
Developments
in Electric Propulsion Feed Systems
D. Bushway |
|
Operation
of a T6 Thruster at the Elevated Thermal Conditions of Mercury for the
ESA Bepi Colombo Mission
N. Wallace et al. |
|
Electric
Propulsion System on @Bus Platform
M. Lyszyk et al. |
|
An
Overview of the T6 Gridded Ion Propulsion System Pre-development Activities
for Alpha-Bus
J. Huddleson et al. |
|
Hybrid
(Coupled Plasma/Ion) Electric Propulsion Systems
E. Chesta et al. |
|
Propulsion
Selection for the Remote Sensing Mission
M. Marcozzi et al. |
|
SkyLAN:
Station Keeping and Propulsion Aspects for ISL Interconnected GEO Clusters
A. Cotellessa et al. |
|
Preparing
for Flight: The Surrey Space Centre's Microscale Solar Propulsion Experiment
(MSPEx)
F. Kennedy et al. |
|
Concept
of Combined Electroreactive and Electrodynamic Propulsion System for Station
Keeping
V. Strashinsky et al. |
|
A
Flexible Cold Gas Propulsion System Concept for Different Space Applications
T. Usbeck et al. |
|
APPT
for LEO Applications
M. Kazeev et al. |
|
Angular
Properties of Xe+-Sputtered Molybdenum at Low Impingement Energy
M. Crofton et al. |
|
Life
Verification of the T5 Ion Extraction Grids for the GOCE Application
M. Potts et al. |
|
Development
and Chamber Testing of a Miniature Radio-frequency Ion Thruster for Microspacecraft
M. Micci et al. |
|
The
Optimisation of the T6 Ion Thruster for the ESA AlphaBus Pre-Development
Activity
J. Brandon-Cox et al. |
|
Investigation
of Sputter Behaviour of Graphite Materials for Ion Thruster Grids
M. Tartz et al. |
|
Plasma
and Ion Beam Characterization by Non-conventional Methods
H. Neumann et al. |
|
Multiple
Ion Thruster Plume Interactions
J. Wang et al. |
|
Thrust
Steering of a Gridded Ion Engine
P. Jameson et al. |
|
A
Survey of the "New Grid Systems for Ion Engines" Technology Project
R. Killinger et al. |
|
RIT22-
The Ion Thruster of the RITA Propulsion System for Commercial and Scientific
Applications
H. Leiter et al. |
|
Design
and Testing of a Cold Gas System
A. Hashem |
|
Bi-Propellant
Propulsion System Improvement for Exported Telecommunication Satellites
P. Garnero et al. |
|
Venus
Express Chemical Propulsion System - The Mars Express Legacy
C. Hunter |
|
Effects
of Gravity on Voided Catalyst Bed of Hydrazine Monopropellant Thrusters
D. Goto et al. |
|
Design
and Performance of a Micronewton Proportional Thruster
N. Solway et al. |
|
Development
of Ceramic Thruster for Spacecraft Propulsion System
H. Mishima et al. |
|
EADS-ST's
Latest Bipropellant 10N Thruster and 400 N Engine: The Fully European
Solution
M. Fick et al. |
|
Development
of 22o N Bi-Propellant Thruster with Micro-Showerhead Injector
G. Schulte et al. |
|
Development
of a Bi-propellant Micro-Rocket Engine
P. Miotti et al. |
|
C-R
Modeling and Spectroscopic Diagnostics of SPT Plasmas
K. Katsonis et al. |
|
Fully
3D Simulation of Electric Propulsion Plumes in Space and on Ground
L. Biagioni et al |
|
Computational
Model for Local Parameter Analysis in an Acceleration Channel of a Hall
Thruster
O. Gorshkov et al. |
|
Hall
Thruster Particle Model
F. Taccogna et al. |
|
The
Limitations of Hall Thrusters by their Specific Impulse
A. Nesterenko et al. |
|
Numerical
Modeling of Heat Flows in a Hall Thruster
V. Gankin et al |
|
Simulation
of the SPT Ceramic Isolator Sputtering Process under Model Conditions
S. Khartov et al. |
|
Effect
of a Localised Neutral Atom Mass Flow Injection in Hall-Effect Thrusters
L. Garrigues et al. |
|
Effect
of Voltage Variation in Hall Thruster Modeling
S. Roy et al. |
|
Development
of Software for Numerical Simulation of the SPT Discharge Chamber Wall
Erosion by the Accelerated Ions
V. Kim et al. |
|
Propulsion
Systems Design and Simulation Tools in Alcatel Space
F. Appaix et al. |
|
Application
of Satellite Hydrazine Propulsion System In-Orbit Monitoring Model
D. Hasan et al. |
|
Dynamic
Solubility of Pressurised He in Liquid Propellants in Closed Storage Tanks
K. Jokela et al. |
|
In-Space
Chemical Propulsion System Model
C. Byers et al. |
|
Numerical
Simulation and Experimental Validation of Viscous Dominated Micro-Nozzle
Flow in Cold-Gas Thrusters
C. Thornber et al. |
|
Numerical
Study of Backflow for Nozzle Plumes by a Hybrid Approach
M. Ivanov et al. |
|
The
Role of Different Parameters in the Pressurant Budget of Venus Express
and its Dynamic Evolution during the Mission
F. Valencia Bel et al. |
|
Anode
Layer Discharge Plasma and Exhaust Plume Diagnostics
A. Semenkin |
|
Optical
Investigation on Plasma Plume of Tal Cluster System
O. Tverdokhlebov et al. |
|
Control
of the Ceramic Erosion by Optical Emission Spectroscopy
D. Pagnon |
|
Detailed
behavior of microinstabilities in Hall thrusters: experimental insight
108
A. Lazurenko et al. |
|
Measurement
of Absolute Xenon Density and Gas Injection Impact in Hall Thrusters
V. Vial et al. |
|
Lessons
learned from infrared thermal imaging of a Hall thruster
S. Mazouffre et al. |
|
Hall-Effect
Thruster Estimation of Intra-Thruster Performances
A. Bober |
|
Simulations
of a Double Stage Hall Thruster Configuration for Plume Focusing
I. Vieira et al. |
|
Manufacturing
of Advanced Titanium (Lined) Propellant Tanks and High Pressure Vessels
W. Radtke |
|
Design,
Development and Validation of the Eurostar 3000 Large Propellant Tank
J.-M. Autric et al. |
|
Experimental
Assessment of the Susceptibility to Stress-corrosion Cracking of Ti 6A1-4V
Alloy Exposed to MON-1 Propellant Tank Environment
G. Bussu et al. |
|
Decontamination
of MMH- and NTO/MON -propellant Tanks
K. Jokela et al |
|
New
Developments in High Pressure Tanks at EADS Space Transportation
C. Le Floc'h |
|
Mechanical
Design and Analysis of Propellant COPVs
R. Beck |
|
An
Overview of Polymeric Materials Development and Qualification Approach
for Propellant Tank Membrane Applications in Europe
F. Valencia Bel et al. |
|
Functional
Design and Qualification of Surface Tension Propellant Tanks
C. Figus et al. |
|
Simulation
of Erosion and Contamination of Spacecraft Surfaces Induced by Plasma
Thruster Plume
A.B. Nadiradze et al. |
|
Hybrid-PIC
Modeling of Hall Thruster Acceleration Channels
M. Andrenucci et al. |
|
Insight
into EADS Astrium Modelling Packages for Electric Propulsion / Spacecraft
Interactions
S. Provost et al. |
|
Improvement
of the Plasma-wall Interaction Model on a Hall-thruster fluid-PIC Code
E. Ahedo et al. |
|
Angular
Characterisation of Erosion and Contamination by Electric Propulsion
T. Tondu et al. |
|
Numerical
Simulation of Taylor Cone-Jets and Colloid Thruster Plumes
J. Carretero et al. |
|
Numerical
Simulations for the Design of a Magnetoplasmadynamic Thruster with Coaxial
Applied Magnetic Field
D. Haag et al. |
|
Study
of the Plasma Discharge in a Hall Thruster
E. Ahedo et al. |
|
The
Manned Exploration of Mars Using Nuclear Electric Propulsion: A Gradual,
Minimum Cost Strategy
D. Fearn |
|
Integrated
Power and Propulsion System
G. Frenken |
|
Pulsed
Plasma Thrusters for Primary Propulsion and Attitude Control of a Small
All Electrical Satellite
A. Nawaz et al. |
|
An
Orbital Transfer Vehicle with Electric Propulsion to Enhance the Vega
Launcher Operational Envelope
S. Marcuccio et al. |
|
µN
Propulsion Subsystem Developments for Drag-Free Spacecraft
D. Nicolini et al. |
|
Solid
Propellant De-orbiting for Constellation Satellites
R. Schonenborg |
|
Multi-Objective
Low-Thrust Trajectory Optimization for Constant and Variable Specific
Impulse Thrusters
R. Pavarin et al. |
|
End-to-End
Orbital Trajectory Optimization
J. Whiting |
|
Darwin
Mission: The Field Emission Electric Propulsion (Feep) Option
V. Pizzagalli et al. |
|
Micropropulsion
Technologies for the European high-precision Formation Flying Interferometer
DARWIN
M. Kilter |
|
New
Generation of Clusterable In-FEEP Emitters
A. Genovese et al. |
|
Advances
in Micro-Fabricated Droplet Emission Mode 1D Colloid Thruster Arrays
L. Velasquez-Gracia et al. |
|
A
MEMS based Field Emission Electrical Propulsion System with Integrated
Charge Neutralizer for Nano and Pico Spacecraft
R.A.W. Fléron et al. |
|
Correction
Propulsion System with Ablative Pulsed Plasma Thrusters for Unified Space
Platform "Vulcan"
N. Antropov et al. |
|
Low-Power
Microwave Electrothermal Thruster Performance Characterization
M. Micci et al. |
|
Double
Stage HET Development activities at SNECMA
M. Prioul et al. |
|
PPS-1350
Qualification Status and Performances
M. Prioul et al. |
|
Experimental
Investigation of the Two-Stage Plasma Thruster ATTILA
H. Boehrk et al. |
|
Design
and Operation of a Liquid Ion Propulsion System in the Bipolar Mode
P. Lozano et al. |
|
Energy
Transfer to the Propellant in High Power PPT
M. Kazeev et al. |
|
Spectroscopic
Study of the Internal Plasma of a T6 Hollow Cathode
S. Pottinger et al. |
|
Development
of a Vaporizing Liquid Bismuth Anode for Hall Thrusters
L. King |
|
A
Shape Memory Alloy Actuated Satellite Isolation Valve
J. Murray et al. |
|
Stationary
and Dynamical Behavior of Hollow Cathode: Diode Regime and With SPT 100
Hall Thruster
L. Albarede et al. |
|
Conditions
and Perspectives of EPE Cathodes Development for Cureents from 20 mA to
2000 A
A. Loyan et al. |
|
A
Field Effect Spacecraft Neutraliser for Fundamental Physics Missions
D. Nicolini et al. |
|
Hollow
Cathode Thrust Measurements Using a Target
P. Gessini et al. |
|
High
Performance Ceramic Discharge Chambers For Hall Effect Thrusters (HET-DC)
I. Caro |
|
Design
and Development of the Minimum Impulse Thruster Valve
R. Huftalen et al. |
|
Modified
Electro-Thermal Thrust Augmentation for Mini-Satellite Applications
Aharon Oren |
|
The
Design of a T5 Thruster Load Simulator for Spacecraft System AIV
S. Clark et al. |
|
Improvement
of Optical Diagnostic Technique for a Xenon Operating Hall Effect Thruster
G. Karabadzhak |
|
An
Imaging Spectroscopy System Based on Multi-fiber Optic for Investigation
of Ion- and Plasma thruster
S. Meiß et al. |
|
The
New European High Power Electric Propulsion Test Facility
L. Biagioni et al. |
|
Performance
of a Large Vacuum Facility for Spacecraft Propulsion Testing
F. Scortecci et al. |
|
Development
of Plasma Diagnostic Methods on Xenon for Plume Investigations of RIT-Ion
Thrusters
M. Winter et al. |
|
Development
of a Two-axes Thrust Stand for Electric Thrusters
R. Falorni et al. |
|
Deposition
Material Measurements from a Hall Thruster using a Quartz Crystal Microbalance
L. Trevisani et al. |
|
Microfluidic
Diagnostics applied to Cold Gas Thruster Design and Analysis
S. Wereley |
|
Bare
Electrodynamic Tape Tether Experiment onboard the Delfi-1 University Satellite
A.-M. Wijnans et al. |
|
High
Thrust Density Electric Propulsion for Heavy Payload In-Space Transportation
M. Auweter-Kurtz et al. |
|
MOA:
Magnetic Field Oscillating Amplified Thruster
N. Frischauf et al. |
|
Electrodeless
Plasma Thruster Design & Modeling
G. Emsellem et al. |
|
Assessment
of Possibility of Advanced Solar Thermal Propulsion Use for Mars Exploratiomission
H. Chang et al. |
|
Nano-Propellants
for Space Propulsion
L. Galfetti |
|
Advanced
Kinetic Model for Electrodynamic Space Tether 141
J.-M. Deux et al. |
|
The
Advanced Developments Of Orbital Thermal-Electric Microthrusters
A. Niatin et al. |
|
Recent
Advancements in MPD Technology at Centrospazio
M. Zuin et al. |
|
New
Performance and Reliability Results of the HEMP-Thruster
G. Kornfeld et al. |
|
MPD
Thruster Discharge Stability Criteria
M. Andrenucci et al. |
|
Optical
studies accompanying a performance test of a HEMP thruster in the JUMBO
test facility
S. Weis et al. |
|
Preferable
Hall-Effect Thruster Performances for Orbit Transfer in a Resistive Medium
A. Bober |
|
Development
of a Prototype Thrust Steering Device for Hall-Effect Thrusters
O. Duchemin et al. |
|
Testing
the PPS®X000 Plasma Thruster at High Discharge Voltage
O. Duchemin et al. |
|
Electromagnetic
Interference with hall thruster operation
K. Kirdyashev et al. |
|
GOCE
IPCU: The Electronic Driving a Ion Propulsion System
C. Tato et al. |
|
High
Power Processing Unit for Stationary Plasma Thruster
E. Bourguignon et al. |
|
Power
Supply and Control Unit for Gridded Ion Thruster
E. Bourguignon et al. |
|
Evolution
of extraction grid erosion with ion thruster operation time
M. Tartz et al. |
|
Investigation
of a Water-Fed Pulsed Plasma Thruster
C. Scharlemann et al. |
|
Design
and Development of the Precision Adjustable Liquid Regulator
R. Meinhold et al. |
|
Influence
of Space Propulsions and Plasma Sources on Electric-Discharge Phenomena
on the ISS
E. Tverdokhlebova et al. |
|
C-R
Modeling of Ar Plasmas: Low Temperature Validation
Katsonis, K.*; Siskos, A.*; Dzierzega, K.**; Pellerin, S.***; Tanguy, Michel****; *Univ. Paris-sud, LPGP,**M. Smoluchowski Inst. of Physics,***LASEP, Univ. d'Orléans, ****Ecole Polytechnique |
|
Low
Temperature Validation of a Xe Plasma C-R Model
Katsonis, K.*; Rouillé, C.*; Siskos, A.*; Tanguy, M.**; *Univ. Paris-sud, LPGP,**Ecole Polytechnique |
|
Ariane
5 SCA Comparison and Correlation between Thermal Tests and Thermal Mathematical
Modelling
Holzwarth, M.; Gralher, M.; Rogall, H.; EADS Space Transportation |
|
Applications
for Solid Propellant Gas Generator Technology
van der List, M.*; Put, P.A.G.*; Elst, J.W.E.C.*; Vliet, L.D.**; Sanders, H.M.**; *BRADFORD engineering B.V.,**TNO-PML |
|
Curret
driven high frequency oscillations in Hall Thrusters |
|
A
Micro-scale Quadrupole Mass Spectrometer for Ion Species Analysis
King, L.; Michigan Technological University |
|
Low
Cost Propulsion for 21st Century Small Satellite Missions
Baker, A.; Gibbon, D.; Surrey Satellite Technology Ltd. |
|
Study
of the Electron Energy Distribution Function Formation Dynamics based
on the 3D3V PIC Hall-type Thruster Model
Pereslavtsev, A.; Khartov, S.; Moscow Aviation Institute |
|
Experimental
study of the electron energy distribution function formation in the near
outside region between cathode and exhaust plane of a Hall-type thruster
Pereslavtsev, A.; Khartov, S.; Moscow Aviation Institute |
|
Selection
of Optimal Dimension of Multimode Hall Thruster
Pridannikov, S.*; Kozubskiy, K.*; Rumiantsev, A.V.**; *EDB Fakel,**Kaliningrad State University |
|
Thermal
Highly Temperature Microflowmeter of Gas
Roumjanzev, A.; Shevchenko, P.; Kaliningrad State University |
|
Adaptive
Grid Simulation of Ultrafast Laser Ablation for Space Propulsion
Batishchev, O.*; Batishcheva, A.**; *MIT,**Delta Search Labs Inc. |
|
Hybrid
Modeling of Plasma Production in VASIMR Engine
Batishchev, O.*; Molvig, K.; MIT |
|
Comparative
Analysis of Carbon Nanostrycture-Based Emitters
Nikolai, N.; Yasinskaya, E.; Kaliningrad State University |
|
The
High Frequency Stabilization of a Magnetoplasmadynamic Thruster
Kirdyashev, K.; Russian Academy of Sciences |
|
Conceptions
and Results of Design for Micro Satellites
Loyan, A.*; Belan, N.*; Dranovskiy, V.**; Koshkin, M.**; Dgur, E.***; Hitko, A.***; *National aerospace University "KhAI",**Design bureau "Yuzhnoe",***Dnepropetrovsk National University |
|
Mathematical
Modeling and Optimization of Development Process of Self-Dependent Electrical
Discharge in Hollow Cathode for Electric Propulsion System
Lobov, S.; National Airspace University "KhAI" |
|
Calculation
Studies for Plasma Parameters in Pulsed Plasma Thruster
Khrustalev, M.; Lyubinskaya, N.; RIAME MAI |
|
The
Use of Colloid Thrusters for Nano satellites
Nicolini, D.*; Kent, B.**; Stark, J.***; Stevens, B.**; Alexander, M.***; *ESA/ESTEC,**Rutherford Appleton Laboratory,***Queen Mary University |
|
Traceable
Calibration of the 3 axis Thrust Vector in the mN range
Hughes, B.; Oldfield, S.; National Physical Laboratory |