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Launch rockets potential analysis in their orbital injection

Authors: Stepanova S.V., Zamyatin D.A.
Published in issue: #7(12)/2017
DOI: 10.18698/2541-8009-2017-7-121


Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Keywords: launch rocket, spacecraft, rocket and space system, low Earth orbit
Published: 28.06.2017

The purpose of the article was to prove the necessity of correct choice of a transport system for injecting into orbit infoware spacecraft of a large mass and overall dimensions.


References

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[3] Vse preimushchestva “Angary”: “Proton”, ustupite mesto dame [All advantages of “Angara”: “Proton”, give place to lady]. Available at: www.vesti.ru/doc.html?id=2589856 (accessed 15 September 2016).