Micropropulsion using laser ablation
The micro-laser plasma thruster ({/content/3U34JN9D1AK4JRRE/xxlarge956.gif}LPT) is a new micropropulsion device that uses laser ablation to create very small thrusts (0.1--100 {/content/3U34JN9D1AK4JRRE/xxlarge956.gif}N) for pointing and positioning micro- and nano-satellites. In this paper, we disc...
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Veröffentlicht in: | Applied physics. A, Materials science & processing Materials science & processing, 2004-09, Vol.79 (4-6), p.1385-1389 |
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Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | The micro-laser plasma thruster ({/content/3U34JN9D1AK4JRRE/xxlarge956.gif}LPT) is a new micropropulsion device that uses laser ablation to create very small thrusts (0.1--100 {/content/3U34JN9D1AK4JRRE/xxlarge956.gif}N) for pointing and positioning micro- and nano-satellites. In this paper, we discuss the expected performance of the {/content/3U34JN9D1AK4JRRE/xxlarge956.gif}LPT. For a ms-pulse device, target materials are restricted to those of low thermal conductivity, e.g. polymers. Volume ablation theory adequately describes their behavior. In a ns-pulse version, exhaust velocity can be an order of magnitude higher with correspondingly lower thrust-to-power ratio. The theory for surface absorbers describes the observed behavior. |
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ISSN: | 0947-8396 1432-0630 |
DOI: | 10.1007/s00339-004-2787-7 |