New concept for electric/ion/plasma propulsion, high thermal efficiency, high thrust density, large range of operational parameters
High efficiency multi-stage plasma (HEMP) thruster : final report on a feasibility study ; Laufzeit des Vorhabens: 01.07.2000 - 31.05.2003
Hoch-effizienter Mehrstufen-Plasmaantrieb (HEMP-Antrieb)
2003
Online-Ressource (55 p. = 4,50 MB)
ill., many graphs
Contract BMBF 50 JR 0043
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Also available as printed version
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Electronic Resource
English , German
BKL: | 55.60 Raumfahrttechnik |