High fidelity model for the atmospheric re-entry of CubeSats equipped with the Drag De-Orbit Device-Reference-Cited by-同舟云学术

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High fidelity model for the atmospheric re-entry of CubeSats equipped with the Drag De-Orbit Device

Published:2019-03 Issue: Volume:156 Page:134-156
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Rafano Carná S.F.^ORCID,Bevilacqua R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. CubeSat Design Specification Rev. 13, Tech. rep., the CubeSat Program,2014

2. CubeSat: a new generation of picosatellite for education and industry low-cost space experimentation;Heidt,2000

3. Launch Services Program, Program Level Dispenser and CubeSat Requirements Document, Tech. rep., LSP-REQ-317.01 Revision B;NASA,2014

4. Spacecraft deorbit point targeting using aerodynamic drag;Omar;J. Guid. Contr. Dynam.,2017

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