Combustion possibility assessment for separating launch-vehicle components during atmospheric phase of descent trajectory

被引：9

作者：

Trushlyakov, V. ^{[1
]}

Zharikov, K. ^{[1
]}

Davydovich, D. ^{[1
]}

机构：

[1] Omsk State Tech Univ, 11 Mira Pr, Omsk 644050, Russia

来源：

ACTA ASTRONAUTICA | 2019年 / 159卷

基金：

俄罗斯科学基金会;

关键词：

HEAT-TRANSFER;

D O I：

10.1016/j.actaastro.2019.02.003

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The investigation is made of the processes associated with the combustion of separating launch vehicle components (LVCs) on the atmospheric phase of the descent trajectory. This allows us to provide a radical solution to the problem of reducing the areas of the LVC impact zones. Ballistic parameters values for the LVC motion are determined. Such areas are proposed for realizing LVC heating to the ignition temperature through the energy mixture burning. Further combustion of the LVC occurs when there is a sufficient amount of oxygen in the oncoming air stream.

引用

页码：540 / 546

页数：7

共 7 条

[1] Method of heating of the separated parts of launch vehicle during the atmospheric phase of the descent trajectory
Trushlyakov, V
Panichkin, A.
Lempert, D.
Shatrov, Ya
Davydovich, D.
ACTA ASTRONAUTICA, 2019, 157 : 1 - 8
[2] Terminal Phase Descent Trajectory Optimization of Reusable Launch Vehicle
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Maity, Arnab
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IFAC PAPERSONLINE, 2022, 55 (22): : 37 - 42
[3] A simulation of the thermal environment of a plastic body of a new type of launch vehicle at the atmospheric phase of the trajectory
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Yemets, Vitaly
Dron, Mykola
Yemets, Mykhailo
Golubek, Aleksandr
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2022, 94 (04): : 505 - 514
[4] Experimental research of thermal loading of the rocket payload fairing element during the atmospheric phase of the descent trajectory
Trushlyakov, V.
Iordan, Yu
Davydovich, D.
Zharikov, K.
Dron, M.
XI INTERNATIONAL SCIENTIFIC AND TECHNICAL CONFERENCE - APPLIED MECHANICS AND DYNAMICS SYSTEMS, 2018, 944
[5] Signal Strength Variations and Data Bit Synchronization Issues of High Dynamic NavIC/GPS Receiver During Ascent Phase of a Launch Vehicle Trajectory
Vinoj, V. S.
Biju, V. S.
Basim, Mohammad
Shankar, Anand O. T.
Pillai, C. Radhakrishna
Sasikumar, S.
2022 URSI REGIONAL CONFERENCE ON RADIO SCIENCE, USRI-RCRS, 2022, : 207 - 210
[6] Analytical solutions for the equations of motion of a space vehicle during the atmospheric re-entry phase on a 2-D trajectory
Mititelu, Gabriel
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2009, 103 (04): : 327 - 342
[7] Analytical solutions for the equations of motion of a space vehicle during the atmospheric re-entry phase on a 2-D trajectory
Gabriel Mititelu
Celestial Mechanics and Dynamical Astronomy, 2009, 103 : 327 - 342

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