On Developing the Design of the Protective Heat Shield for the Interhelio-Zond Spacecraft
- 10 Downloads
This article describes the design of the protective heat shield for the Interhelio-Zond spacecraft, accepted for full-scale engineering development. The material proposed for making the shield’s parts is a carbon-carbon composite material (CCCM). The technology of making and mating of the CCCM shield parts is determined.
Keywordsprotective heat shield carbon-carbon composite materials
Unable to display preview. Download preview PDF.
- Andreeva, A.V., Osnovy fizikokhimii i tekhnologii kompozitov: uchebnoe posobie dlya vuzov (Foundations of Physical Chemistry and Technology for Composites. Student’s Book for Universities), Moscow: IPRZhR, 2001.Google Scholar
- https://doi.org/solarprobe.gsfc.nasa.gov/SolarProbePlus_pre.pdf. Cited September 20, 2016. https://doi.org/www.mai.ru/science/trudy/published.php?ID=63029. Cited September 20, 2016.
- Krit, B.L., Tikhonov, S.A., Sorokin, V.A., Frantskevich, V.P., and Somov, O.V., Improved combined methods for processing aerospace materials by concentrated energy fluxes, Vestn. NPO im. S.A. Lavochkina, 2014, no. 4, pp. 62–67.Google Scholar
- Lyubomudrov, A.A., How the ionized cloud of spacecraft self outer atmosphere influences onto shielding properties of its structure, Vestn. NPO im. S.A. Lavochkina, 2016, no. 2, pp. 44–46.Google Scholar