Impact of mission requirements and constraints on conceptual launch vehicle design

Authors: Rahn M.; Schottle U.M.; Messerschmid E.

Source: Aerospace Science and Technology, Volume 3, Number 6, September 1999 , pp. 391-401(11)

Publisher: Elsevier

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

Language: English

Document Type: Research article

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

Affiliations: 1: aMAN Technologie AG, Aerospace Division, RS, P.O. Box 1347, 85751, Karlsfeld, Germany

Publication date: 1999-09-01

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