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Impact of mission requirements and constraints on conceptual launch vehicle design

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Keywords: Flugbahnoptimierung; System- und Missionsoptimierung; airbreathing vehicle; conceptual vehicle design; konzeptioneller Fahrzeugentwurf; luftatmendes Tragersystem; nichtlineare Programmierung; nonlinear programming; raketengetriebenes Tragersystem; rocket vehicle; system and mission optimization; trajectory optimization

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S1270-9638(00)86429-9

Affiliations: aMAN Technologie AG, Aerospace Division, RS, P.O. Box 1347, 85751, Karlsfeld, Germany

Publication date: September 1, 1999

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