Results 41 to 50 of about 295,166 (297)

Plasma Accelerator Utilizing the Medium of Near-Earth Space for Orbital Transfer Vehicles

open access: yesApplied Sciences, 2023
The development of plasma accelerators for spacecraft propulsion that can capture space matter and energy shows great promise for spacecraft advancement.
Alexander R. Karimov   +3 more
doaj   +1 more source

Aerocapture: Enabling Small Spacecraft Direct Access to Low-Circular Orbits for Planetary Constellations

open access: yesAerospace, 2023
Small satellite constellations in multiple-inclination, low-circular orbits around Mars and Venus have the potential to perform a range of high-value science investigations within cost-constrained missions.
A. Girija, S. Saikia, J. Longuski
semanticscholar   +1 more source

Orbital Maintenance of a Constellation of CubeSats for Internal Gravity Wave Tomography

open access: yesIEEE Journal of Selected Topics in Applied Earth Observations and Remote Sensing, 2020
The advent of radio occultation (RO) instruments aboard CubeSats leads to the possibility of a mission to sound atmospheric internal gravity waves if such satellites are deployed in close-flying constellation.
Stephen Leroy   +4 more
doaj   +1 more source

Electrically powered ion acceleratot with contact ionixation for perspertive electrically powered thrusters

open access: yesSt. Petersburg Polytechnical University Journal: Physics and Mathematics, 2020
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

A review of air-breathing electric propulsion: from mission studies to technology verification

open access: yesJournal of Electric Propulsion, 2022
Air-breathing electric propulsion (ABEP) allows for lowering the altitude of spacecraft operations below 250 km, in the so-called Very Low Earth Orbits (VLEOs).
T. Andreussi, E. Ferrato, V. Giannetti
semanticscholar   +1 more source

Displaced geostationary orbit design using hybrid sail propulsion [PDF]

open access: yes, 2011
Because of an increase in the number of geostationary spacecraft and the limits imposed by east–west spacing requirements, the geostationary orbit is becoming congested. To increase its capacity, this paper proposes to create new geostationary slots by
Becerra V. M.   +14 more
core   +1 more source

Scalable Microfabrication of Multi-Emitter Arrays in Silicon for a Compact Microfluidic Electrospray Propulsion System

open access: yesACS Applied Materials and Interfaces, 2022
The recent proliferation of SmallSats and their use in increasingly demanding applications require the development of onboard electric propulsion compatible with the power, mass, and volume constraints of these spacecraft.
Albert Cisquella-Serra   +2 more
semanticscholar   +1 more source

Air-breathing electric propulsion: mission characterization and design analysis

open access: yesJournal of Electric Propulsion, 2022
Air breathing electric propulsion (atmosphere-breathing electric propulsion) (ABEP) has attracted significant interest as an enabling technology for long duration space missions in very low Earth orbit (VLEO) altitudes below about 300 km.
P. Crandall, R. Wirz
semanticscholar   +1 more source

Plasmas for spacecraft propulsion

open access: yesJournal of Physics D: Applied Physics, 2009
This review presents the basics of plasma discharges applied to electric spacecraft propulsion. It briefly reports on the mature and flown technologies of gridded ion thrusters and Hall thrusters before exploring the recent yet immature technology of plasma thrusters based on expansion from low pressure high density inductively coupled and wave-excited
openaire   +3 more sources

Numerical comparison of exhaust plume flow behaviors of small monopropellant and bipropellant thrusters. [PDF]

open access: yesPLoS ONE, 2017
In general, a space propulsion system has a crucial role in the normal mission operations of a spacecraft. Depending on the types and number of propellants, a monopropellant and a bipropellant thrusters are mostly utilized for low thrust liquid rocket ...
Kyun Ho Lee
doaj   +1 more source

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