Inserting a maximum-mass spacecraft into a target orbit using a limited-thrust engine with releasing the separable part of its launch vehicle into the Earth's atmosphere
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Publication:6567828
DOI10.1134/S000511792401003XzbMATH Open1543.70018MaRDI QIDQ6567828
Author name not available (Why is that?)
Publication date: 5 July 2024
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