Interface between the long-term propagation and the destructive re-entry phases exploiting the overshoot boundary-Reference-Cited by-同舟云学术

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Interface between the long-term propagation and the destructive re-entry phases exploiting the overshoot boundary

Published:2022-06 Issue:2 Volume:9 Page:174-181
ISSN:2468-8967
Container-title:Journal of Space Safety Engineering
language:en
Short-container-title:Journal of Space Safety Engineering

Author:

Fusaro Christian,Trisolini Mirko^ORCID,Colombo Camilla

Funder

European Research Council

Horizon 2020

Publisher

Elsevier BV

Subject

Safety, Risk, Reliability and Quality,Aerospace Engineering

Reference17 articles.

1. End-of-life re-entry for highly elliptical orbits: the INTEGRAL mission;Colombo;Adv. Astronaut. Sci.,2014

2. End-of-life disposal of high elliptical orbit missions: the case of integral;Armellin;Adv. Space Res.,2015

3. Orbit aspects of end-of-life disposal from highly eccentric orbits;Merz,2015

4. Planetary Orbital Dynamics (PlanODyn) Suite for long term propagation in perturbed environment;Colombo,2016

5. Introduction to Astrodynamic Reentry;Hicks,2009

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Student paper competition at the eleventh IAASS space safety conference, ‘Managing Risk in Space’ in 2021;Journal of Space Safety Engineering;2022-06

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