nach oben

Erschienen in:

01.09.2023

Calculation of Heat Loads in Analysis of Superorbital Entry of Spacecraft into Atmosphere of the Earth

verfasst von: D. L. Reviznikov, A. V. Nenarokomov, M. S. Konstantinov, I. A. Nikolichev, A. V. Morzhukhina, L. M. Chernova

Erschienen in: Journal of Engineering Thermophysics | Ausgabe 3/2023

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

Correlations for calculation of heat loads during a return of spacecraft at the second cosmic velocity are given. Analysis of the heat transfer for a model descent trajectory has been carried out. The convective and radiative heat fluxes, the relative heat transfer coefficient, and the radiative-equilibrium surface temperature have been calculated. The results obtained are a basis for design and optimization of the heat shield of spacecraft.

Vorheriger Artikel Thermal Conductivity and Thermal Diffusivity of Mg–Ca Eutectic Alloys in Solid State

Nächster Artikel Energy Recovery Based on Exhaust Gas Recirculation and Heat Regeneration Processes Applied in a Firewood Boiler

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Tirskii, G.A., Sakharov, V.I., Kovalev, V.L., Egorov, I.V., et al., Giperzvukovaya aerodinamika i teplomassoobmen spuskaemykh kosmicheskikh apparatov i planetnykh zondov (Hypersonic Aerodynamics and Heat-Mass Transfer of Landing Spacecraft and Planetary Space Sensors), Moscow: Fizmatlit, 2011.

Viviani, A. and Pezzella, G., Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles, Springer, Switzerland, 2015.CrossRef

Surzhikov, S.T., Komp’yuternaya aerofizika spuskaemykh kosmicheskikh apparatov. Dvumernye modeli (Computer Aerophysics of Landings Spacecraft. 2D Models), Moscow: Fizmatli, 2018.

Salomatov, V.V. and Salomatov, V.V., Computational Modeling of Turbulent Flows, J. Eng. Therm., 2020, vol. 29, no. 1, pp.156–169; https://doi.org/10.1134/S1810232820010117.CrossRef

Surzhikov, S.T., Radiation Gas Dynamics of the Frontal Surface of the Command Module of Apollo-4 at Superorbital Entry into the Atmosphere, Izv. RAN. MZHG, 2017, vol. 6, pp. 108–124.

Surzhikov, S.T., Radiation Aerothermodynamics of the Stardust Space Vehicle, J. Appl. Math. Mech., 2016, vol. 80, no. 1, pp. 44–56; https://doi.org/10.1016/j.jappmathmech.2016.05.008.ADSMathSciNetCrossRefMATH

Egorov, I.V. and Nikol’skii, V.S., Viscous Hypersonic Currents for Various Aerophysical Models, Izv. RAN. MZHG, 1996, vol. 4, pp. 151–161.

Gurvich, L.V., Veitz, I.V., et al., Termodinamicheskie svoistva individual’nykh veshchestv: spravochnoe izdanie v 4-kh tomakh (Thermodynamic Properties of Individual Substances: Reference Edition in 4 Volumes), Moscow: Nauka, 1982.

Park, C., Howe, J., and Jaffe, R., Review of Chemical-Kinetic Problems of Future NASA Mission, II: Mars Entries, J. Therm. Heat Transfer, 1994, vol. 8, no. 1, pp. 9–23; https://doi.org/10.2514/3.496.ADSCrossRef

10.

Wood, W.A. and Eberhardt, S., Dual-Code Solution Strategy for Chemically-Reacting Hypersonic Flows, AIAA Paper, 1995, vol. 95–0158; https://doiorg/10.2514/6.1995-158.

11.

Afonina, N.E., Gromov, V.G., and Kovalyov, V.L., Heat Transfer with Catalytic Surfaces of Heat Shield of Spacecraft Entering the Atmosphere of Mars, Mat. Model., 2000, vol. 12, no. 7, pp. 79–86.

12.

Alnak, D.E., Koca, F., and Alnak, Y.A., Numerical Investigation of Heat Transfer from Heated Surfaces of Different Shapes, J. Eng. Therm., 2021, vol. 30, no. 3, pp. 494–507; https://doi.org/10.1134/ S1810232821030127.CrossRef

13.

Zel’dovich, Ya.B. and Raiser, Yu.P., Fizika udarnykh voln i vysokotemperaturnykh gidrodinamicheskikh yavlenii (Physics of Shock Waves and High-Temperature Hydrodynamic Phenomena), Moscow: Fizmatlit, 2008.

14.

Reviznikov, D.L. and Sukharev, T.Yu., Hypersonic Flow around Blunt Bodies in the Atmosphere of the Earth and Mars. Comparative Analysis of Mathematical Models, Tepl. Prots. Tekhn., 2018, vol. 10, nos. 1/2, pp. 5–15.

15.

Nomura, W., Determination of Heat Flux Density at Critical Point of Blunt Body in Hypersonic Flux at Small Reynolds Numbers, AKT, 1984, vol. 2, no. 7.

16.

Johnston, C.O., Hollis, B.R., and Sutton, K., Nonequilibrium Stagnation-Line Radiative Heating for Fire-II, JSR, 2008, vol. 45, no. 6, p. 1185; https://doi.org/10.2514/1.33008.ADSCrossRef

17.

Cornette, E.S., Forebody Temperatures and Calorimeter Heating Rates Measured during Project Fire II Reentry at 11.35 km/s, NASA TM X-13 05, 1966.

18.

Olynick, D.R., Henline, W.D., Hartung, L.C., and Candler, G.V., Comparison of Coupled Radiative Navier–Stokes Flow Solutions with the Project Fire-II Flight Data, AIAA, 1994; https://doi.org/10.2514/6.1994-1955.

19.

Surzhikov, S.T. and Shuvalov, M.P., Testing of Calculated Data on Radiation and Convective Heating of Landing New-Generation Spacecraft, Teplofiz. Vys. Temp., 2013, vol. 51, no. 3, pp. 456–470.

20.

Surzhikov, S.T. and Shuvalov, M.P., Analysis of Radiation-Convective Heating of Four Types of Landing Spacecraft, Fiz.-Khim. Kinet. Gaz. Din., 2014, vol. 15, no. 4.

21.

Shevelev, Yu.D. and Syzranova, N.G., Influence of Chemical Reactions on Heat Transfer in the Boundary Layer, Fiz.-Khim. Kinet. Gaz. Din., 2010, vol. 10, no. 2, pp. 91–126.

22.

Brandis, A.M. and Johnston, C.O., Characterization of Stagnation-Point Heat Flux for Earth Entry, AIAA, 2014; https://doi.org/10.2514/6.2014-2374.

23.

Samarskii, A.A. and Gulin, A.V., Chislennye metody (Numerical Methods), Moscow: Nauka, 1989.

24.

Avduevskii, V.S. and Koshkin, V.K., Osnovy teploperedachi v aviatsionnoi i raketno-kosmicheskoi tekhnike (Basics of Heat Transfer in Aviation and Rocket-Space Technology), Moscow: Mashinostroenie, 1992.

25.

Fay, J.A. and Ridell, F.R., Theory of Stagnation Point Heat Transfer in Dissociated Air, J. Aeronavt. Sci., 1958, vol. 25, no. 2, pp. 73–82; https://doi.org/10.2514/8.7517.

26.

Tauber, M.E. and Sutton, K., Stagnation-Point Radiative Heating Relations for Earth and Mars Entries, J. Spacecraft, 1991, vol. 28, no. 1, p. 40; https://doi.org/10.2514/3.26206.ADSCrossRef

27.

Johnson, J.E., Starkey, R.P., and Lewis, M.J., Aerothermodynamic Optimization of Reentry Heat Shield Shapes for a Crew Exploration Vehicle, J. Spacecraft Rockets, 2007, vol. 44, no. 4, p. 849; https://doi.org/ 10.2514/1.27219.ADSCrossRef

Titel: Calculation of Heat Loads in Analysis of Superorbital Entry of Spacecraft into Atmosphere of the Earth
verfasst von: D. L. Reviznikov
A. V. Nenarokomov
M. S. Konstantinov
I. A. Nikolichev
A. V. Morzhukhina
L. M. Chernova
Publikationsdatum: 01.09.2023
Verlag: Pleiades Publishing
Erschienen in: Journal of Engineering Thermophysics / Ausgabe 3/2023
Print ISSN: 1810-2328
Elektronische ISSN: 1990-5432
DOI: https://doi.org/10.1134/S1810232823030050

Premium Partner

Marktübersichten

Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.

Zur Marktübersicht

Springer Professional

Abstract

Bitte loggen Sie sich ein, um Zugang zu Ihrer Lizenz zu erhalten.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Weitere Artikel der Ausgabe 3/2023

Resource Characteristics of Tubular Copper Electrodes in Electric Arc Plasma Torches¹

Experimental and Numerical Investigation of Al2O3 Nanofluids Based Crude Oil in Shell and Tube Heat Exchanger

Experimental Investigation of Parabolic Trough Solar Collector Thermal Efficiency Enhanced by Different Reflective Materials

Significance of Thermal Boundary Layer Analysis of MHD Chemically Radiative Dissipative Casson Nanofluid Flow over a Stretching Sheet with Heat Source

Entropy and Exergy Analysis in an Experimental Thermal System Used GO–DW Nanofluid Having Straight Copper Pipes with Different Diameters

Boiling Heat Transfer with Freon R-21 in Vertical Downflow for Assembly of Minichannels with Inclined Texture

Premium Partner

Marktübersichten