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A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system

Fazeley, H. R. / Taei, H. / Naseh, H. / Mirshams, M.

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A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system

Fazeley, H. R. / Taei, H. / Naseh, H. / Mirshams, M.

A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system

Fazeley, H. R. / Taei, H. / Naseh, H. / Mirshams, M.

Zugriff

Zugriff über TIB

Verfügbarkeit in meiner Bibliothek prüfen

Bestellung bei Subito €

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Ähnliche Titel

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Titel:

A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system

Beteiligte:

Fazeley, H. R. (Autor:in) / Taei, H. (Autor:in) / Naseh, H. (Autor:in) / Mirshams, M. (Autor:in)

Erschienen in:

STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION ; 53 ; 145-160

Erscheinungsdatum:

01.01.2016

Format / Umfang:

16 pages

ISSN:

1615-147X

Medientyp:

Aufsatz (Zeitschrift)

Format:

Sprache:

Englisch

Klassifikation:

DDC: 624.17713

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