Ballistic aspects of large-size space debris flyby at low Earth near-circular orbits

DOI10.1134/S106423071504005XzbMATH Open1338.93261OpenAlexW2347698523MaRDI QIDQ295610

A. A. Baranov, D. A. Grishko

Publication date: 13 June 2016

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s106423071504005x

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05)

Related Items (5)

Spacecraft transfer optimization with releasing the additional fuel tank and the booster to the Earth atmosphere ⋮ Dynamics of highly eccentric and highly inclined space debris ⋮ Mathematical modeling of space debris evolution in near-earth orbits ⋮ Title not available (Why is that?) ⋮ Orbital effects in a cloud of space debris making a close approach with the earth

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