Results 11 to 20 of about 61,268 (302)
Conceptual Design of Microwave Electrothermal Thruster of Satellite [PDF]
Microwave electrothermal thruster is the propellant that converts microwave energy into heat energy. nowadays, with the technology development of electric thrusters are very important in terms of producing high specific impact and low fuel consumption ...
Sahar noori +2 more
doaj +1 more source
Development and Application Prospect of Space Electric Propulsion Technology
Space electric propulsion technology has entered a new stage of maturity and full application in China. In order to further promote and accelerate the development of electric propulsion technology, this paper adopted the methods of investigation and ...
Hai GENG +8 more
doaj +1 more source
Design of the Propulsion System of Nano satellite: StudSat2
6 pages, 13 figures, Accepted and Presented in Proceeding of International Conference on Mechanical and Aerospace Engineering (ICMAE-17), Kathmandu, Nepal on 30th Dec 2017, ASAR International ...
Roshan Sah +3 more
openaire +2 more sources
A Review of Low-Power Electric Propulsion Research at the Space Propulsion Centre Singapore
The age of space electric propulsion arrived and found the space exploration endeavors at a paradigm shift in the context of new space. Mega-constellations of small satellites on low-Earth orbit (LEO) are proposed by many emerging commercial actors ...
George-Cristian Potrivitu +6 more
doaj +1 more source
Exploring the first aerosol indirect effect over Southeast Asia using a 10-year collocated MODIS, CALIOP, and model dataset [PDF]
Satellite observations and model simulations cannot, by themselves, give full insight into the complex relationships between aerosols and clouds.
A. D. Ross +6 more
doaj +1 more source
Nanosatellite orbit control using MEMS cold gas thrusters; pp. 279–285 [PDF]
We introduce nanosatellite orbit control using a novel miniaturized cold gas propulsion module based on microelectromechanical systems (MEMS) technology.
Urmas Kvell +6 more
doaj +1 more source
Design Tradeoffs in Full Electric, Hybrid and Full Chemical Propulsion Communication Satellite
Full electric propulsion system becomes popular recently and getting more common in the communication satellite industry. Full electric or hybrid propulsion selection causes results in significant reduction in satellite propellant mass. Conventional full
Ü.cezmi Yılmaz, İbrahim Oz
doaj +1 more source
Comparison between Different Re-Entry Technologies for Debris Mitigation in LEO
The population of satellites in Low Earth Orbit is predicted to growth exponentially in the next decade due to the proliferation of small-sat constellations.
Francesco Barato
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Adelis-SAMSON is a nano-satellite mission aimed at performing geo-location of target signals on Earth using a tight three-satellite formation in space. To maintain formation, each nano-satellite is equipped with a cold gas propulsion system.
Michael Zaberchik +3 more
doaj +1 more source
This paper presents the development, construction and testing of a new type of solar–thermal propulsion system which can be used for low earth orbit (LEO) satellites.
Constantin Sandu +6 more
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