Nukleonika > 2015 > 60 > 2 > 257-261
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ISSN czasopisma : | 0029-5922 |
DOI | 10.1515/nuka-2015-0057 |
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Bibliografia
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1. Barral, S., Kurzyna, J., Szelecka, A., Rachubiński, H., Remírez, E., Martín, R., Ortiz, P., Alonso, J., Bottinelli, S., Mabillard, Y., Zaldívar, A., Rangsten, P., & Koppel, C. (2014). First experimental characterization of a pulsed plasma thruster with non-volatile liquid propellant. In Proceedings of Space Propulsion Conference, 19–22 May 2014. Cologne, Germany.
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2. Rezaeiha, A., & Schönherr, T. (2013). Overview of alternative propellants for use in PPT. In 29th International Symposium on Space Technology and Science ISTS, 2–9 June 2013. Nagoya, Japan.
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3. Barral, S., Kurzyna, J., Remírez, E., Martín, R., Ortiz, P., Alonso, J., Bottinelli, S., Mabillard, Y., Zaldívar, A., Rangsten, P., & Koppel, C. R. (2013). Development status of an open capillary pulsed plasma thruster with non-volatile liquid propellant. In Proceedings of the 33rd International Electric Propulsion Conference, 6–10 October 2013 (paper IEPC-2013-291). Worthington, OH: The Electric Rocket Propulsion Society.