A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system
Crossref DOI link: https://doi.org/10.1007/s00158-015-1304-2
Published Online: 2015-08-22
Published Print: 2016-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Fazeley, H. R.
Taei, H.
Naseh, H.
Mirshams, M.
Text and Data Mining valid from 2015-08-22