Reverse and pull-away engines for the carrier rocket sustainer
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...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2019-01-01
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| Series: | MATEC Web of Conferences |
| Online Access: | https://www.matec-conferences.org/articles/matecconf/pdf/2019/47/matecconf_icmtmte18_00082.pdf |