Features of Afterbody Radiative Heating for Earth Entry
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[1] Determination of the emissivity of materials , 1962 .
[2] W. D. Goodrich,et al. The aerothermodynamic environment of the Apollo command module during superorbital entry , 1972 .
[3] Chul Park. Comparison of electron and electronic temperatures in recombining nozzle flow of ionized nitrogen—hydrogen mixture. Part 1. Theory , 1973, Journal of Plasma Physics.
[4] C. Park,et al. Nonequilibrium Hypersonic Aerothermodynamics , 1989 .
[5] Richard A. Thompson,et al. A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30000 K , 1989 .
[6] Charles H. Kruger,et al. Ionization nonequilibrium induced by neutral chemistry in air plasmas , 1996 .
[7] Wolfgang L. Wiese,et al. Atomic Transition Probabilities of Carbon, Nitrogen, and Oxygen: A Critical Data Compilation , 1996 .
[8] Bourdon,et al. Three-body recombination rate of atomic nitrogen in low-pressure plasma flows. , 1996, Physical review. E, Statistical physics, plasmas, fluids, and related interdisciplinary topics.
[9] W. Willcockson. Stardust Sample Return Capsule Design Experience , 1998 .
[10] Mark Loomis,et al. Aerothermal analysis of the Project Fire II afterbody flow , 2001 .
[11] Sanford Gordon,et al. NASA Glenn Coefficients for Calculating Thermodynamic Properties of Individual Species , 2002 .
[12] Takashi Abe,et al. Assessment of Forebody and Backbody Radiative Heating Rate of Hypervelocity Reentry Capsule , 2003 .
[13] Chul Park,et al. Effect of Lymann Radiation on Nonequilibrium Ionization of Atomic Hydrogen , 2004 .
[14] Michael J. Wright,et al. Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design , 2006 .
[15] Christopher O. Johnston,et al. Non-Boltzmann Modeling for Air Shock-Layer Radiation at Lunar-Return Conditions , 2008 .
[16] Dinesh K. Prabhu,et al. Radiation Modeling for the Reentry of the Stardust Sample Return Capsule , 2008 .
[17] B. Hollis,et al. Spectrum Modeling for Air Shock-Layer Radiation at Lunar-Return Conditions , 2008 .
[18] Chul B. Park. The Limits of Two-Temperature Kinetic Model in Air , 2010 .
[19] Alireza Mazaheri,et al. LAURA Users Manual: 5.3-48528 , 2010 .
[20] Peter Jenniskens,et al. Observations of the Stardust Sample Return Capsule Entry with a Slitless Echelle Spectrograph , 2010 .
[21] S. Surzhikov,et al. Simulating Stardust Earth Reentry with Radiation Heat Transfer , 2011 .
[22] Christopher O. Johnston,et al. Shock Layer Radiation Modeling and Uncertainty for Mars Entry , 2012 .
[23] L. Marraffa,et al. Aerothermal analysis of the Phoebus capsule with radiative heating on the back body , 2012 .
[24] P. Omaly,et al. Global rate coefficients for ionization and recombination of carbon, nitrogen, oxygen, and argon , 2012 .
[26] Christopher O. Johnston,et al. Uncertainty Analysis of Air Radiation for Lunar-Return Shock Layers , 2012 .
[27] Marco Panesi,et al. QCT-based vibrational collisional models applied to nonequilibrium nozzle flows , 2012 .
[28] Alireza Mazaheri,et al. Radiative Heating Uncertainty for Hyperbolic Earth Entry, Part 1: Flight Simulation Modeling and Uncertainty , 2013 .
[29] Andrea Lani,et al. Collisional radiative coarse-grain model for ionization in air , 2013 .
[30] Andrea Lani,et al. Modeling of non-equilibrium phenomena in expanding flows by means of a collisional-radiative model , 2013 .
[31] A. Bourdon,et al. Consistent multi-internal-temperatures models for nonequilibrium nozzle flows , 2013 .
[32] C. Johnston,et al. Three-Dimensional Radiation Ray-Tracing for Shock-Layer Radiative Heating Simulations , 2013 .