Estimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing
It is proposed to carry out burning of the launch vehicle nose fairing after it has completed its mission on the descent trajectory from the moment of separation to an altitude of 5-10 km. Burning is carried out in the Earth atmosphere with additional heating of the faring material due to the reacti...
| Published in: | Combustion, explosion, and shock waves Vol. 51, № 5. P. 619-622 |
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| Main Author: | |
| Other Authors: | , |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Online Access: | http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000550117 Перейти в каталог НБ ТГУ |