000 01695nab a2200325 c 4500
001 vtls000550117
003 RU-ToGU
005 20220414175234.0
007 cr |
008 180311|2015 ru s a eng dd
024 7 _a10.1134/S0010508215050147
_2doi
035 _ato000550117
040 _aRU-ToGU
_brus
_cRU-ToGU
100 1 _aLempert, D. B.
_9396604
245 1 0 _aEstimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing
_cD. B. Lempert, V. I. Trushlyakov, V. E. Zarko
504 _aБиблиогр.: 6 назв.
520 3 _aIt 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 reaction of pyrotechnic mixtures. Various pyrotechnic mixtures for use in the nose fairing are discussed.
653 _aгорение
653 _aобтекатели
653 _aракеты-носители
653 _aпиротехнические смеси
655 4 _aстатьи в журналах
_9681159
700 1 _aTrushlyakov, V. I.
_9366127
700 1 _aZarko, Vladimir E.
_9103027
773 0 _tCombustion, explosion, and shock waves
_d2015
_gVol. 51, № 5. P. 619-622
_x0010-5082
852 4 _aRU-ToGU
856 7 _uhttp://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000550117
908 _aстатья
999 _c333230