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Nuri-Derived SmallSat-Dedicated Launch Vehicle: Staging Design, Vehicle Sizing, and MDO-Based Feasibility Assessment

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By Hyeonjun Kim, Daeban Seo
| preprints.org
You are already at the latest version The increasing demand for SmallSats requires launch systems providing responsive, independent, and mission-specific access to orbit. This study presents the conceptual design and feasibility assessment of a Nuri-derived SmallSat-dedicated launch vehicle for delivering a 500 kg-class payload to a 500 km sun-synchronous orbit.
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