Reconstruction of aerothermal heating for the thermal protection system of a reusable launch vehicle

Brociek, Rafał; Hetmaniok, Edyta�; Słota, Damian

doi:10.1016/j.applthermaleng.2022.119405

Cited by 12 publications

(1 citation statement)

References 17 publications

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“…Based on research of the environmental factors' impact on the spacecraft and review of modern global trends [1][2][3][4][5][6][7], stages and procedures of the further research are stated. Further research involves the substantiation of the choice of solution options for the reusable spacecraft's protection systems, the choice of design and locations of the passive thermal protection system elements (thermal protection insulation of the spacecraft).…”

Section: High Vacuum Impact Protectionmentioning

confidence: 99%

Substantiation of the protection system’s technical outline for the aerospace objects

Lobunko,

Iskra

2023

Visnyk TNTU

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During their operational time, spacecraft are exposed to numerous factors, which are specific to the space environment. Spacecraft designing is a complex scientific and technical problem, which solution necessarily requires taking into account the possible effect of these factors on the structural elements and systems of the vehicle, including protective means in its concept and ensuring its functioning in the expected operational conditions. This paper presents a review of the main space environment factors, which affects the spacecraft, defines global trends in the protection systems’ development and substantiation of the perspective protection system’s technical configuration.

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