| Issue |
MATEC Web Conf.
Volume 102, 2017
V International Forum for Young Scientists “Space Engineering”
|
|
|---|---|---|
| Article Number | 01011 | |
| Number of page(s) | 4 | |
| Section | Applied Aerospace Engineering | |
| DOI | https://doi.org/10.1051/matecconf/201710201011 | |
| Published online | 15 March 2017 | |
Research of the launch vehicle design made of composite materials under the aerodynamic, thermal and acoustic loadings
Omsk State Technical University, 644050 Omsk, Russia
* Corresponding author: iordanyuliya@gmail.com
The experimental research of the carbon composite material sample of payload fairing half structural element was carried out under different types of loading. Mathematical and physical modeling of the sample loading using aerodynamic flow was conducted. Heat loading was researched by the method of a thermal analysis during which typical heat dots corresponding to the changes in the sample structure were determined. Ultrasonic influence on the sample characteristics was considered. As a result, the value of heat leak to the structure surface while moving in the atmospheric phase of the descent was determined.
© The Authors, published by EDP Sciences, 2017
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