|
Teplofizika vysokikh temperatur, 2013, Volume 51, Issue 3, Pages 456–470
(Mi tvt98)
|
|
|
|
This article is cited in 17 scientific papers (total in 17 papers)
Heat and Mass Transfer and Physical Gasdynamics
Checking computation data on radiative and convectional heating of next generation spacecraft
S. T. Surzhikovab, M. P. Shuvalovc a Ishlinskii Institute for Problems in Mechanics, Russian Academy of Sciences, Moscow, Russia
b Moscow Institute of Physics and Technology, Dolgoprudnyi, Russia
c Korolev RKK Energy, Moscow Region, Korolev, Russia
Abstract:
The results of testing correlation equations in calculating convective and radiative heating of landers are presented for the examples of Apollo 4 and Stardust, for which we have a great amount of numerical data by other authors. Using these correlation dependences, the analysis of heating of the landing module is performed in the flight experiment Fire-II. With the use of special developed two-dimensional and three-dimensional computer codes NERAT(2D,3D)+ASTEROID, we performed calculations on radiative-gasdynamics at some entry points on the trajectories of the Stardust and Fire-II landers. The correlation dependences and computer codes NERAT(2D,3D)+ASTEROID were used in giving a prognosis of the aerothermodynamics of promising spacecrafts of large size. The reasons for the discrepancy in numerical data are discussed.
Received: 25.12.2012
Citation:
S. T. Surzhikov, M. P. Shuvalov, “Checking computation data on radiative and convectional heating of next generation spacecraft”, TVT, 51:3 (2013), 456–470; High Temperature, 51:3 (2013), 408–420
Linking options:
https://www.mathnet.ru/eng/tvt98 https://www.mathnet.ru/eng/tvt/v51/i3/p456
|
Statistics & downloads: |
Abstract page: | 384 | Full-text PDF : | 193 | References: | 86 |
|