An overview of cube-satellite propulsion technologies and trends

AR Tummala, A Dutta - Aerospace, 2017 - mdpi.com
CubeSats provide a cost effective means to perform scientific and technological studies in
space. Due to their affordability, CubeSat technologies have been diversely studied and …

Electric propulsion for small satellites

M Keidar, T Zhuang, A Shashurin, G Teel… - Plasma Physics and …, 2014 - iopscience.iop.org
Propulsion is required for satellite motion in outer space. The displacement of a satellite in
space, orbit transfer and its attitude control are the task of space propulsion, which is carried …

Survey of propulsion technologies applicable to cubesats

J Mueller, R Hofer, J Ziemer - Joint Army-Navy-NASA-Air Force …, 2010 - ntrs.nasa.gov
At present, no Cubesat has flown in space featuring propulsion. This was acceptable as long
as CubeSats were flown mostly as university experiments. As CubeSats become of interest …

Propulsion options for very low Earth orbit microsatellites

M Leomanni, A Garulli, A Giannitrapani, F Scortecci - Acta Astronautica, 2017 - Elsevier
The growing competitiveness in the commercial space market has raised the interest in
operating small spacecraft at very low altitudes. To make this feasible, the space industry …

Development and testing of a 3-d-printed cold gas thruster for an interplanetary cubesat

EG Lightsey, T Stevenson… - Proceedings of the …, 2018 - ieeexplore.ieee.org
This paper describes the development and testing of a cold gas attitude control thruster
produced for the BioSentinel spacecraft, a CubeSat that will operate beyond Earth orbit. The …

[PDF][PDF] Design and testing of a cold gas thruster for an interplanetary CubeSat mission

TK Imken, TH Stevenson, EG Lightsey - Journal of Small Satellites, 2015 - jossonline.com
A cold gas thruster has been developed by the Texas Spacecraft Laboratory (TSL),
University of Texas at Austin (UT-Austin), for an interplanetary CubeSat mission called …

Experimental effects of nozzle geometry on flow efficiency at low Reynolds numbers

AR Bruccoleri, R Leiter, M Drela… - Journal of Propulsion and …, 2012 - arc.aiaa.org
IN THE past decades, technology for microelectromechanical systems (MEMS) has
expanded greatly, enabling orders-ofmagnitude reductions in the size of aerospace …

一种用于微小推力冲量测量的扭摆系统参数标定方法

金星, 洪延姬, 周伟静, 常浩 - 推进技术, 2015 - jpt.tjjsjpt.com
扭摆系统通常用来测量航天微推力器的微推力和微冲量. 为了实现扭摆的系统参数精确标定,
根据扭摆系统阶跃响应的特点, 深入分析稳态扭转角和极值扭转角及其对应时间等特征点与系统 …

Fabrication and preliminary testing of hydroxylammonium nitrate (HAN)-based ceramic microthruster for potential application of nanosatellites in constellation …

K Markandan, Z Zhang, J Chin, KH Cheah… - Microsystem …, 2019 - Springer
Constellation formation flying of nanosatellites (< 10 kg) is becoming a trend for future space
exploration missions. Liquid chemical micropropulsion that can provide high thrusting force …

Design and characterization of a 3D-printed attitude control thruster for an interplanetary 6U CubeSat

T Stevenson, G Lightsey - 2016 - digitalcommons.usu.edu
This paper describes the design and testing of a miniature, 3D-printed cold gas attitude
control thruster for the NASA Ames Research Center BioSentinel mission, an interplanetary …