MATEC Web Conf.
Volume 298, 2019International Conference on Modern Trends in Manufacturing Technologies and Equipment: Mechanical Engineering and Materials Science (ICMTMTE 2019)
|Number of page(s)||4|
|Published online||18 November 2019|
Reverse and pull-away engines for the carrier rocket sustainer
Udmurt Federal Research Center of the Ural Branch of the RAS, 426067 Izhevsk, Russia
2 Kalashnikov Izhevsk State Technical University, 426000 Izhevsk, Russia
3 International Network Center for Fundamental and Applied Research, 20036 Washington, USA
* Corresponding author: email@example.com
The work on the parameters of the engines for pulling away the spent rocket stage to the restricted zone is conducted with the use of the sustainer engine specially calculated for the present investigation. It is shown that a special block of engines having the functions of reverse and pull away can be the most effective solution of the problem. Depending on the aim and launch site and the location of the restricted zone the best variant is the mounting of the units of small special-purpose engines.
© The Authors, published by EDP Sciences, 2019
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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