Multidisciplinary Design Optimization of a Two-Stage LOX/Methane Partially Reusable Microlauncher

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Detaylı Bibliyografya
Yayımlandı:	Aerospace vol. 12, no. 11 (2025), p. 1030-1090
Yazar:	Onel Alexandru-Iulian
Diğer Yazarlar:	Tudorel-Petronel, Afilipoae, Popescu Oana-Iuliana, Ichim Georgiana, Popescu, Alexandra
Baskı/Yayın Bilgisi:	MDPI AG
Konular:	European Space Agency > ESA Design optimization Multidisciplinary design optimization Mathematical models Polar orbits Aerodynamics Methane Liquid oxygen Reusable launch vehicles Algorithms Engines Research & development > R&D Satellites Cost estimates Vehicles
Online Erişim:	Citation/Abstract Full Text + Graphics Full Text - PDF
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