Applying the method of direct statistical modeling to the rocket measurements of air density
- Authors: Shtyrkov O.V.1, Yushkov V.A.1, Zhurin S.V.2, Kusov A.L.3
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Affiliations:
- Central Aerological Observatory
- Korolev Rocket and Space Corporation Energiya
- Central Research Institute of Machine Building
- Issue: Vol 42, No 12 (2017)
- Pages: 817-826
- Section: Article
- URL: https://journals.rcsi.science/1068-3739/article/view/230449
- DOI: https://doi.org/10.3103/S106837391712010X
- ID: 230449
Cite item
Abstract
A new approach to the calculation of aerodynamic characteristics ofthe rocket sensor with the oncoming gas flow using the method of direct statistical modeling and software allows computing the factor of aerodynamic interaction between the instrument and the oncoming air flow and thereby linking the measured air density with the density of the unperturbed atmosphere for the Mach number range of 0-3 and Knudsen number range of 10-3 -10. On the base of the obtained results the method of air density measurement using meteorological rockets is developed.
About the authors
O. V. Shtyrkov
Central Aerological Observatory
Email: olegvalsh@yandex.ru
Russian Federation, Pervomaiskaya 3, Dolgoprudnyi, Moscow oblast, 141700
V. A. Yushkov
Central Aerological Observatory
Author for correspondence.
Email: olegvalsh@yandex.ru
Russian Federation, Pervomaiskaya 3, Dolgoprudnyi, Moscow oblast, 141700
S. V. Zhurin
Korolev Rocket and Space Corporation Energiya
Email: olegvalsh@yandex.ru
Russian Federation, ul. Lenina 4A, Korolev, Moscow oblast, 141070
A. L. Kusov
Central Research Institute of Machine Building
Email: olegvalsh@yandex.ru
Russian Federation, ul. Pionerskaya 4, Korolev, Moscow oblast, 141070