Results 1 to 10 of about 88 (87)
This paper continues the publication cycle on developing the ion plasma electrically powered spacecraft propulsion (EPSP) of the spacecraft. For monitoring and control of the EPSP operation, a feedback system based on a signal proportional to the EPSP ...
Dyubo Dmitry +6 more
doaj +2 more sources
Spacecraft impacts with advanced power and electric propulsion [PDF]
A study was performed to assess the benefits of advanced power and electric propulsion systems for various space missions. Advanced power technologies that were considered included multi-band gap and thin-film solar arrays, lithium batteries, and flywheels. Electric propulsion options included Hall effect thrusters and ion thrusters.
L.S. Mason, S.R. Oleson
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A number of characteristics of ionic and ion-plasma accelerators laboratory samples designed for electrically powered spacecraft propulsion were investigated in the experimental research.
Tsybin Oleg +6 more
doaj +1 more source
Аn analytical electrodynamic algorithm has been developed in order to study physical processes and calculate mechanical forces in an ion accelerator. This algorithm is combined with computer simulation of the electromagnetic field and charged particles ...
Dyubo Dmitry, Tsybin Oleg
doaj +1 more source
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model [PDF]
The National Aeronautics and Space Administration (NASA) Solar Electric Propulsion Technology Demonstration Mission (SEP TDM), in conjunction with PC Krause and Associates, has created a Simulink-based power architecture model for a 50 kilo-Watt (kW) solar electric propulsion system.
Jeffrey Csank +2 more
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Jovian planet missions for solar cell powered electric propulsion spacecraft [PDF]
Missions for solar-electric propulsion spacecraft, calculating flyby and elliptic capture missions to Jupiter, Saturn, Uranus and ...
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The paper describes mathematical models used to select design parameters of an electric propulsion unit for station keeping on low orbit of an Earth observation satellite. Mathematical models are developed with consideration for limited power supply on board of spacecraft.
G P Anshakov +3 more
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MW-Scale High-Voltage Direct-Current Power Conversion for Large-Spacecraft Electric Propulsion
This paper proposes a megawatt (MW)-scale high-voltage (HV) electrical power-conversion element for large-spacecraft electric propulsion (EP) systems. The proposed scheme is intended for long-term and crewed missions, and it is driven by a nuclear electric propulsion (NEP) that acts as a heat source. The scheme includes (i) A two-rotor generator (TRG),
Ghazaleh Sarfi, Omid Beik
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The Psyche Magnetometry Investigation. [PDF]
Weiss BP +17 more
europepmc +1 more source
Carbon Nanocomposites in Aerospace Technology: A Way to Protect Low-Orbit Satellites. [PDF]
Weerasinghe J +6 more
europepmc +1 more source

