Integral performance optimization for the two-stage-to-orbit RBCC-RKT launch vehicle based on GPM

Title
Integral performance optimization for the two-stage-to-orbit RBCC-RKT launch vehicle based on GPM
Authors
Keywords
-
Journal
AERONAUTICAL JOURNAL
Volume -, Issue -, Pages 1-26
Publisher
Cambridge University Press (CUP)
Online
2019-06-17
DOI
10.1017/aer.2019.41

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