11 / 11
Д.Я. Баринов, П.В. Просунцов
32
ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение. 2016. № 6
[3]
Crouch R.K., Walberg G.D. An investigation on ablation behavior of AVCOAT 5026/39M
over a wide range of thermal environments.
NASA Technical Memorandum
. 1969, no. X-1778.
36 p.
[4]
Alifanov O.M., Budnik S.A., Nenarokomov A.V., Netelev A.V. Identification of the ma-
thematical models of heat transfer in destruction materials.
Teplovye protsessy v tekhnike
[Thermal Processes in Engineering], 2011, vol. 3, no. 8, pp. 338–347 (in Russ.).
[5]
Nikitin P.V., Sotnik E.V. Features of the mechanism of destruction glass-reinforced heat-
shielding materials at variable parameters thermal exposure.
Teplovye protsessy v tekhnike
[Thermal Processes in Engineering], 2011, vol. 3, no. 8, pp. 348–359 (in Russ.).
[6]
Chen Y.-K., Milos F.S. Ablation and thermal response program for spacecraft heatshield
analysis.
Journal of Spacecraft and Rockets
, 1999, vol. 36, no. 3, pp. 475–483.
DOI: 10.2514/2.3469
[7]
Dec J.A., Braun R.D., Lamb B. Ablative thermal response analysis using the finite element
method.
Journal of Thermophysics and Heat Transfer
, 2012, vol. 26, no. 2, pp. 201–212.
DOI: 10.2514/1.T3694
[8]
Zemlyanskiy B.A., Lunev V.V., Timoshenko V.P., et al. Some heat exchange problems
of hypersonic aircraft of gliding descent.
Trudy NPO “Molniya”
, 1985, no. 1, pp. 34–61
(in Russ.).
[9]
Alifanov O.M., Artyukhin E.A., Nenarokomov A.V. Obratnye zadachi v issledovanii
slozhnogo teploobmena [Inverse problems in complex heat exchange investigation]. Moscow,
Yanus-K Publ., 2009. 300 p.
[10]
Isaev K.B. Teplofizicheskie kharakteristiki materialov v shirokikh diapazonakh tempera-
tur i skorostey nagreva [Material thermophysical properties in wide temperature band]. Kiev,
Kupriyanova Publ., 2008. 240 p. (in Russ.).
[11]
MSC Marc Volume A: Theory and user information. MSC Software Corporation, 2013.
876 p.
[12]
Wertheimer T.B., Laturelle F. Thermal decomposition analysis of rocket motors and
other thermal protection systems using MSC. Marc-ATAS.
Proc. 14-th Thermal
&
Fluid
Analysis Workshop
, 2003. 16 p.
[13]
Davis B.A. International Space Station (ISS) Soyuz vehicle descent module evaluation
of thermal protection system (TPS) penetration characteristics.
NASA Technical Report
, 2013,
JSC-66527. 396 p.
[14]
GOST 4401–81. Atmosfera standartnaya. Parametry [State standard 4401–81. Standard
atmosphere. Parameters]. Moscow, Izd-vo standartov Publ., 1981. 180 p.
Barinov
D.Ya. —
engineer at Federal State Unitary Enterprise All-Russian Scientific Research
Institute of Aviation Materials (Radio ul. 17, Moscow, 105005 Russian Federation).
Prosuntsov P.V.
— Dr. Sci. (Eng.), Professor of Rocket and Space Composite Structures De-
partment, Bauman Moscow State Technical University (2-ya Baumanskaya ul. 5, Moscow,
105005 Russian Federation).
Please cite this article in English as:
Barinov
D.Ya., Prosuntsov P.V. Modeling of Heat Transfer in Decomposable Materials of
Thermal Protection Coating of Reentry Vehicle.
Vestn. Mosk. Gos. Tekh. Univ. im. N.E. Bau-
mana, Mashinostr.
[Herald of the Bauman Moscow State Tech. Univ., Mech. Eng.], 2016,
no. 6, pp. 22–32. DOI: 10.18698/0236-3941-2016-6-22-32