Thermodynamic model of the evaporation process of liquid residues of the propellant components in the orbital stage of the launch vehicle-Reference-Cited by-同舟云学术

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Thermodynamic model of the evaporation process of liquid residues of the propellant components in the orbital stage of the launch vehicle

Published:2018-09 Issue: Volume:150 Page:63-72
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Trushlyakov V.,Kudentsov V.,Matyushin D.,Buryak A.

Funder

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference47 articles.

1. Modelling of the space debris evolution based on continua mechanics;Smirnov;Space Debris,2001

2. Space traffic hazards from orbital debris mitigation strategies;Smirnov;Acta Astronaut.,2015

3. Mathematical Modeling of Space Debris Evolution in the Near Earth Orbits;Smirnov,2002

4. Update of the IADC space debris mitigation guidelines. IADC-11-02. Beijing.

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. Reasonable testing of hypergolic fuels;Acta Astronautica;2020-11

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