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 |
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Keywords: launch rocket, spacecraft, rocket and space system, low Earth orbit |
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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).