[1] [1] LIEBHART H, HERDRICH G, FASOULAS S. Advances for radiation modeling for earth re-entry in PARADE: application to the STARDUST atmospheric entry, AIAA-2012-3196 ［R］. New orleans, Louisiana: AIAA, 2012.

[2] [2] GRINSTEAD J H, JENNISKENS P, CASSELL A M, et al.. Airborne observation of the hayabusa sample return capsule reentry, AIAA -2011-3329 ［R］. Honolulu, Hawaii: AIAA, 2011.

[3] [3] HERMANN T, LHLE S, ZANDER F, et al... Characterization of a reentry plasma wind-tunnel flow with vacuum-ultraviolet to near-infrared spectroscopy ［J］. Journal of Thermophysics and Heat Transfer, 2016, 30(3): 673-688.

[4] [4] PORAT H, MORGAN R G, MCINTYRE T J. Study of radiative heat transfer in Titan atmospheric entry ［C］. Proceedings of 28th International Congress of the Aeronautical Sciences, Launceston, 2012.

[5] [5] JOHNSTON C O, GNOFFO P A, MAZAHERI A. Influence of coupled radiation and ablation on the aerothermodynamic environment of planetary entry vehicles ［J］. RTO Lecture Series, Von Karman Inst. for Fluid Dynamics, Rhode-St-Genèse, Belgium, 2013, 218: 1-36.

[6] [6] BRANDIS A M, JOHNSTON C O. Characterization of stagnation-point heat flux for earth entry AIAA-2014-2374 ［R］. Atlanta: AIAA, 2014.

[7] [7] GUPTA R N. Aerothermodynamic analysis of stardust sample return capsule with coupled radiation and ablation ［J］. Journal of Spacecraft and Rockets, 2000, 37(4): 507-514.

[8] [8] GNOFFO P A, JOHNSTON C O, KLEB B B. Challenges to computational aerothermodynamic simulation and validation for planetary entry vehicle analysis, NASA RTO-EN-AVT-186 ［R］. Washington: NASA, 2010.

[9] [9] JACOBS P, MORGAN R, BRANDIS A, et al.. Design, operation and testing in expansion tube facilities for super-orbital re-entry ［C］. STO-AVT-VKI Lecture Series Radiation and Gas-Surface Interaction Phenomena in High Speed Re-Entry (2013-AVT-218). 2013: 5-1-5-65.

[10] [10] JACOBS C M, MCLNTYRE T J, MORGAN R G, et al.. Radiative heat transfer measurements in low-density titan atmospheres ［J］. Journal of Thermophysics and Heat Transfer, 2015, 29(4): 835-844.

[11] [11] HOLLIS B R, STRIEPE S A, WRIGHT M J, et al.. Prediction of the aerothermodynamic environment of the huygens probe. AIAA-2005-4816 ［R］. Toronto: AIAA, 2005.

[12] [12] PARK C. Nonequilibrium Air Radiation (NEQAIR) Program: User's Manual, NASA-TM-86707 ［R］. Washington: NASA, 1985.

[13] [13] THOMAS G M, MENARD W A. Experimental measurements of nonequilibrium and equilibrium radiation from planetary atmospheres ［J］. AIAA Journal, 1966, 4(2): 227-237.

[14] [14] GKEN T. N2-CH4-Ar chemical kinetic model for simulations of atmospheric entry to Titan, AIAA-2004-2469 ［R］. Portland: AIAA, 2004.

[15] [15] BOSE D, WRIGHT M J, BOGDANOFF D W, et al.. Modeling and experimental assessment of CN radiation behind a strong shock wave ［J］. Journal of Thermophysics and Heat Transfer, 2006, 20(2): 220-230.

[16] [16] LABRACHERIE L, BILLIOTTE M, HOUAS L. Shock-tube analysis of argon influence in Titan radiative environment ［J］. Journal of Thermophysics and Heat Transfer, 1996, 10(1): 162-168.

[17] [17] LEWIS S W, MORGAN R G, MCINTYRE T J, et al.. Expansion tunnel experiments of earth reentry flow with surface ablation ［J］. Journal of Spacecraft and Rockets, 2016, 53(5): 887-899.

[18] [18] SHEIKH U A, MORGAN R G, MCINTYRE T J. Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tube ［J］. AIAA Journal, 2015, 53(12): 3589-3602.

[19] [19] SHEIKH U A, JACOBS C, LAUX C O, et al.. Measurements of radiating flow fields in the vacuum ultraviolet ［C］. Proceedings of the 29th International Symposium on Shock Waves, Springer, 2013: 653-658.

[20] [20] BRANDIS A M, MORGAN R G, MCINTYRE T J, et al.. Nonequilibrium radiation intensity measurements in simulated Titan atmospheres ［J］. Journal of Thermophysics and Heat Transfer, 2010, 24(2): 291-300.

[21] [21] YANG Q S, YU X L, JIANG N B, et al.. Spectral measurement of nitrogen emission behind normal shock wave ［J］. Experiments and Measurements in Fluid Mechanics, 2000, 14(3): 57-60+65. (in Chinese)

[22] [22] YANG H, ZHANG Y SH, DING W ZH. Detectability of airship infrared detection system to hypersonic vehicle ［J］. Chinese Optics,2016, 9(5): 596-605. (in Chinese)

[23] [23] MENG F SH, XIONG R SH, LIU CH H. Analysis of hypersonic reentry radiation model ［J］. Opt. Precision Eng., 2006, 14(8): 574-578. (in Chinese)

[24] [24] LIN X, YU X L, LI F, et al.. Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere ［J］. Acta Mechanica Sinica, 2012, 28(5): 1293-1302.

[25] [25] BRANDIS A M, GOLLAN R J, SCOTT M P, et al.. Expansion tube operating, conditions for studying nonequilibrium radiation relevant to Titan aerocapture, AIAA-2006-4517［R］. Sacramemto: AIAA, 2006.