Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow

Table 1

Flight conditions.

Points	Height (km)	Mach number	Atmospheric pressure (Pa)	Atmospheric temperature (K)	Atmospheric density (kg/m^3)
	35.2	5.0	400	270	0.001189
	43.4	6.0	176	270	0.000935
	47.7	7.0	105	268	0.000772
	50.8	8.0	70	264	0.000654
	53.3	9.0	50	260	0.000562
	55.4	10.0	40	257	0.000488
	57.4	11.0	30	254	0.000425
(the worst)	60.6	12.0	24	251	0.000371