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Optimization of Solenoid Parameters for a Magnetic Nozzle Assembly Using Design of Experiments

IEEE access, 2024, Vol.12, p.114618-114625

2024

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A systematic approach to the modelling and comparison of the geometries of spherical electrodes in inertial electrostatic confinement fusion devices

Scientific reports, 2024-01, Vol.14 (1), p.2261-2261, Article 2261

2024

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Feasibility Study of the Bare-Photovoltaic-Tether Concept: Prototypes and Experimental Performance Evaluation of the Photovoltaic Tether Segment

Aerospace, 2023-04, Vol.10 (4), p.386

2023

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Evidence for surface fusion in inertial electrostatic confinement devices

Physics of plasmas, 2018-11, Vol.25 (11)

2018

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Thermoelectric Generators on Satellites—An Approach for Waste Heat Recovery in Space

Energies (Basel), 2016-07, Vol.9 (7), p.541

2016

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Subgrid Turbulent Flux Models for Large Eddy Simulations of Diffusion Flames in Space Propulsion

Fluids (Basel), 2024-06, Vol.9 (6), p.124

2024

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An Experimental Test of the Classical Interpretation of the Kaluza Fifth Dimension

Physics (Online), 2020-12, Vol.2 (4), p.587-595

2020

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Combustion Regimes in Turbulent Non-Premixed Flames for Space Propulsion

Aerospace, 2023-08, Vol.10 (8), p.671

2023

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Electron guiding in macroscopic borosilicate capillaries with large bending angles

Scientific reports, 2021-04, Vol.11 (1), p.8345-8345, Article 8345

2021

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Characterisation and Design of Direct Numerical Simulations of Turbulent Statistically Planar Flames

Aerospace, 2022-10, Vol.9 (10), p.530

2022

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Surface Pressure Measurement of Truncated, Linear Aerospike Nozzles Utilising Secondary Injection for Aerodynamic Thrust Vectoring

Aerospace, 2024-07, Vol.11 (7), p.507

2024

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Highly miniaturized FEEP propulsion system (NanoFEEP) for attitude and orbit control of CubeSats

Acta astronautica, 2018-03, Vol.144, p.422-428

2018

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Electric Sail Mission Expeditor, ESME: Software Architecture and Initial ESTCube Lunar Cubesat E-Sail Experiment Design

Aerospace, 2023-08, Vol.10 (8), p.694

2023

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Force probes for development and testing of different electric propulsion systems

EPJ techniques and instrumentation, 2022-06, Vol.9 (1), p.1-12, Article 4

2022

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Reproducibility of operating potentials for a C12A7 electride plasma-based cathode with constant keeper current control

Journal of electric propulsion, 2024-10, Vol.3 (1), p.22, Article 22

2024

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Concerning the ignition of a C12A7 electride plasma-based cathode

Journal of electric propulsion, 2024-01, Vol.3 (1), p.2, Article 2

2024

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Characterization of a C12A7 electride plasma-based cathode using different keeper orifice sizes

Journal of electric propulsion, 2023-12, Vol.2 (1), p.25, Article 25

2023

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Investigation of the Alzofon weight reduction experiment using NMR spectroscopy

Measurement : journal of the International Measurement Confederation, 2024-09, Vol.237, p.115075, Article 115075

2024

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Development and testing of a low-current applied-field magnetoplasmadynamic thruster with a rectangular discharge channel

Journal of electric propulsion, 2022-11, Vol.1 (1), Article 23

2022

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Centrifugal balance for the detection of mass fluctuations in advanced propulsion concepts

Acta astronautica, 2023-11, Vol.212, p.270-283

2023

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EVALUATION OF THE INFLUENCE OF A FIELD-LESS ELECTROSTATIC POTENTIAL ON ELECTRON BEAM DEFLECTION AS PREDICTED BY WEBER ELECTRODYNAMICS

Progress in electromagnetics research M Pier M, 2021, Vol.105, p.1-8

2021

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Active Spacecraft Potential Control for the Magnetospheric Multiscale Mission

IEEE transactions on plasma science, 2012-02, Vol.40 (2), p.394-401

2012

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Experimental validation of a looped-tube thermoacoustic engine with a stub for tuning acoustic conditions

Energy conversion and management, 2018-12, Vol.177, p.292-305

2018

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Evaluation of the Influence of a Field-Less Electrostatic Potential on Electron Beam Deflection as Predicted by Weber Electrodynamics

Progress in electromagnetics research M Pier M, 2021-07, Vol.105, p.1

2021

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Optimization of Solenoid Parameters for a Magnetic Nozzle Assembly Using Design of Experiments

A systematic approach to the modelling and comparison of the geometries of spherical electrodes in inertial electrostatic confinement fusion devices

Feasibility Study of the Bare-Photovoltaic-Tether Concept: Prototypes and Experimental Performance Evaluation of the Photovoltaic Tether Segment

Evidence for surface fusion in inertial electrostatic confinement devices

Thermoelectric Generators on Satellites—An Approach for Waste Heat Recovery in Space

Subgrid Turbulent Flux Models for Large Eddy Simulations of Diffusion Flames in Space Propulsion

An Experimental Test of the Classical Interpretation of the Kaluza Fifth Dimension

Combustion Regimes in Turbulent Non-Premixed Flames for Space Propulsion

Electron guiding in macroscopic borosilicate capillaries with large bending angles

Characterisation and Design of Direct Numerical Simulations of Turbulent Statistically Planar Flames

Surface Pressure Measurement of Truncated, Linear Aerospike Nozzles Utilising Secondary Injection for Aerodynamic Thrust Vectoring

Highly miniaturized FEEP propulsion system (NanoFEEP) for attitude and orbit control of CubeSats

Electric Sail Mission Expeditor, ESME: Software Architecture and Initial ESTCube Lunar Cubesat E-Sail Experiment Design

Electric Sail Test Cube–Lunar Nanospacecraft, ESTCube-LuNa: Solar Wind Propulsion Demonstration Mission Concept

Force probes for development and testing of different electric propulsion systems

Reproducibility of operating potentials for a C12A7 electride plasma-based cathode with constant keeper current control

Concerning the ignition of a C12A7 electride plasma-based cathode

Characterization of a C12A7 electride plasma-based cathode using different keeper orifice sizes

Investigation of the Alzofon weight reduction experiment using NMR spectroscopy

Development and testing of a low-current applied-field magnetoplasmadynamic thruster with a rectangular discharge channel

Centrifugal balance for the detection of mass fluctuations in advanced propulsion concepts

EVALUATION OF THE INFLUENCE OF A FIELD-LESS ELECTROSTATIC POTENTIAL ON ELECTRON BEAM DEFLECTION AS PREDICTED BY WEBER ELECTRODYNAMICS

Active Spacecraft Potential Control for the Magnetospheric Multiscale Mission

Experimental validation of a looped-tube thermoacoustic engine with a stub for tuning acoustic conditions

Evaluation of the Influence of a Field-Less Electrostatic Potential on Electron Beam Deflection as Predicted by Weber Electrodynamics

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