The present research investigates a case study on thermal design and improvement of hydrazine monopropellant pipelines based on actual cases, in order to highlight the critical factors for thermal design when developing an onboard propulsion system for a
Kyun Ho Lee +3 more
doaj +1 more source
Development of a Laser Micro-Thruster and On-Orbit Testing
Laser micro-thrust technology is a type of propulsion that uses a laser beam to ablate a propellant such as a metal or plastic. The ablated material is expelled out the back of the spacecraft, generating thrust.
Jifei Ye +8 more
doaj +1 more source
Infrared Astronomical Satellite (IRAS) Scientific Data Analysis System [PDF]
The Jet Propulsion Laboratory's Scientific Data Analysis System will process Infrared Astronomical Satellite data and produce a catalog of perhaps a million infrared sources in the sky, as well as other vital information for astronomical ...
Duxbury, John H., Soifer, B. T.
core +1 more source
High-resolution tropospheric carbon monoxide profiles retrieved from CrIS and TROPOMI [PDF]
The Measurements of Pollution in the Troposphere (MOPITT) instrument is the only satellite-borne sensor in operation that uses both thermal (TIR) and near-infrared (NIR) channels to estimate CO profiles.
D. Fu +10 more
doaj +1 more source
Chebyshev super spectral viscosity method for water hammer analysis
In this paper, a new fast and efficient algorithm, Chebyshev super spectral viscosity (SSV) method, is introduced to solve the water hammer equations. Compared with standard spectral method, the method's advantage essentially consists in adding a super ...
Hongyu Chen +3 more
doaj +1 more source
Orbit Determination for All-Electric GEO Satellites Based on Space-Borne GNSS Measurements
Orbit accuracy of the transfer orbit and the mission orbit is the basis for the orbit control of all-electric-propulsion Geostationary Orbit (GEO) satellites.
Wenqiang Lu +3 more
doaj +1 more source
Forecast analysis on satellites that need de-orbit technologies: future scenarios for passive de-orbit devices [PDF]
Propulsion-based de-orbit is a space-proven technology; however, this strategy can strongly limit operational lifetime, as fuel mass is dedicated to the de-orbiting. In addition previous reliability studies have identified the propulsion subsystem as one
Kingston, Jennifer, Palla, Chiara
core +2 more sources
Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer [PDF]
Micro-propulsion Systems are low thrust engines that be used in space missions like keeping satellite in orbit and changing orbit. These engines have several kinds and liquid propellant micro-propulsion is used in this project.
Amirhossein Edalatpour +2 more
doaj +1 more source
Adult skeletal muscle stem cell migration is mediated by a blebbing/amoeboid mechanism [PDF]
Adult skeletal muscle possesses a resident stem cell population called satellite cells which are responsible for tissue repair following damage. Satellite cell migration is crucial in promoting rapid tissue regeneration but is a poorly understood ...
Collins-Hooper, Henry +4 more
core +1 more source
Fuel Consumption Estimation via Bookkeeping Method for Geostationary Satellites: Simple Application
This work focuses on the Satellite Propulsion Subsystem (UPS), a critical aspect of satellite technology that can be supported by various propulsion types: electrical, chemical, cold gas, and nuclear propulsion.
Tarek Badis +2 more
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