Forthcoming articles

 


International Journal of Aerospace System Science and Engineering

 

These articles have been peer-reviewed and accepted for publication in IJASSE, but are pending final changes, are not yet published and may not appear here in their final order of publication until they are assigned to issues. Therefore, the content conforms to our standards but the presentation (e.g. typesetting and proof-reading) is not necessarily up to the Inderscience standard. Additionally, titles, authors, abstracts and keywords may change before publication. Articles will not be published until the final proofs are validated by their authors.

 

Forthcoming articles must be purchased for the purposes of research, teaching and private study only. These articles can be cited using the expression "in press". For example: Smith, J. (in press). Article Title. Journal Title.

 

Articles marked with this shopping trolley icon are available for purchase - click on the icon to send an email request to purchase.

 

Articles marked with this Open Access icon are freely available and openly accessible to all without any restriction except the ones stated in their respective CC licenses.

 

Register for our alerting service, which notifies you by email when new issues of IJASSE are published online.

 

We also offer RSS feeds which provide timely updates of tables of contents, newly published articles and calls for papers.

 

International Journal of Aerospace System Science and Engineering (1 paper in press)

 

Regular Issues

 

  • Design and Implementation of Low-Power Low-Cost Quasi Steady-State Magnetoplasmadynamic Propulsion using Ar-He and N2-He Gas Mixtures   Order a copy of this article
    by Clyde Stoute, Brendan Quine 
    Abstract: Current miniature plasma propulsion technologies use ion or Hall propulsion to provide thrust for miniature satellites. The problem with ion and Hall thrusters is the low thrust-to-power ratio (30 50 mN/kW), and it is not enough for sharp manoeuvres in deep-space missions. Alternatively, magnetoplasmadynamic propulsion provides higher thrust to miniature satellites than ion thrusters without the increase in mass. Magnetoplasmadynamic propulsion is a technology that the plasma is accelerated electromagnetically. This research investigates the design and performance of a low-cost magnetoplasmadynamic thruster built for micro and nano-satellites. Gas mixtures are tested in this research to observe any improvement in the overall performance. The gases used in the thruster are pure helium, nitrogen, and argon; also, gas mixtures of 50% helium 50% nitrogen and 50% helium 50% argon. The specific impulse, impulse bit, thrust efficiency, and thrust-weight ratio of 50% helium 50% nitrogen are 801 seconds, 6.29
    Keywords: magnetoplasmadynamics; propulsion; electric; space; astronautics; plasma.