Electric propulsion methods for small satellites: A review
D O'Reilly, G Herdrich, DF Kavanagh - Aerospace, 2021 - mdpi.com
Over 2500 active satellites are in orbit as of October 2020, with an increase of~ 1000
smallsats in the past two years. Since 2012, over 1700 smallsats have been launched into …
smallsats in the past two years. Since 2012, over 1700 smallsats have been launched into …
[HTML][HTML] Review of alternative propellants in Hall thrusters
VG Tirila, A Demairé, CN Ryan - Acta Astronautica, 2023 - Elsevier
Hall thrusters, the most common type of electric propulsion system, typically use xenon as
the propellant, given its inertness, its ability to be stored at a high density under pressure …
the propellant, given its inertness, its ability to be stored at a high density under pressure …
Ion thrusters for electric propulsion: Scientific issues developing a niche technology into a game changer
K Holste, P Dietz, S Scharmann, K Keil… - Review of Scientific …, 2020 - pubs.aip.org
The transition from old space to new space along with increasing commercialization has a
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
[图书][B] An introduction to laboratory space and fusion plasma
A Piel - 2010 - Springer
The enlarged new edition of this textbook provides a comprehensive introduction to the
basic processes in plasmas and demonstrates that the same fundamental concepts describe …
basic processes in plasmas and demonstrates that the same fundamental concepts describe …
Space propulsion technology for small spacecraft
As small satellites become more popular and capable, strategies to provide in-space
propulsion increase in importance. Applications range from orbital changes and …
propulsion increase in importance. Applications range from orbital changes and …
Enhanced smoothing technique for indirect optimization of minimum-fuel low-thrust trajectories
Indirect methods used for solving optimal-control problems, when combined with proper
initialization and homotopy approaches, remain attractive for space trajectory optimization …
initialization and homotopy approaches, remain attractive for space trajectory optimization …
Deep-space optical navigation for M-ARGO mission
V Franzese, F Topputo, F Ankersen… - The Journal of the …, 2021 - Springer
Abstract The Miniaturised Asteroid Remote Geophysical Observer (M-ARGO) mission is
designed to be ESA's first stand-alone CubeSat to independently travel in deep space with …
designed to be ESA's first stand-alone CubeSat to independently travel in deep space with …
High-power, null-type, inverted pendulum thrust stand
KG Xu, MLR Walker - Review of Scientific Instruments, 2009 - pubs.aip.org
This article presents the theory and operation of a null-type, inverted pendulum thrust stand.
The thrust stand design supports thrusters having a total mass up to 250 kg and measures …
The thrust stand design supports thrusters having a total mass up to 250 kg and measures …
Indirect Forward–Backward Shooting for Low-Thrust Trajectory Optimization in Complex Dynamics
Y Sidhoum, K Oguri - Journal of Guidance, Control, and Dynamics, 2024 - arc.aiaa.org
OVER the last decades, low-thrust propulsion has gained signifi-cant appeal due to its high
specific impulse, allowing a greater payload fraction to be delivered at a lower cost …
specific impulse, allowing a greater payload fraction to be delivered at a lower cost …
The Moon 35 years after Apollo: What's left to learn?
CR Neal - Geochemistry, 2009 - Elsevier
With the cancellation of the Apollo program after Apollo 17 returned from the Moon in 1972,
the focus of NASA switched to other areas of the Solar System. Study of the Moon did …
the focus of NASA switched to other areas of the Solar System. Study of the Moon did …