Thermal-Mechanical Optimization of Folded Core Sandwich Panels for Thermal Protection Systems of Space Vehicles

Table 5

ITPS thermal-mechanical optimization results.

Case	(K)		(mm)	(mm)	(mm)	(mm)	(mm)	(mm)	(mm)	(mm)	(kg/m^2)
	423 K	0.006	89.90	109.30	59.56	86.32	20.00	1.73	3.93	1.00	38.08
	423 K	0.008	91.83	109.24	58.40	86.33	20.00	1.57	3.82	1.00	36.29
	423 K	0.01	92.24	109.38	57.04	86.30	20.00	1.44	3.76	1.00	35.07
	453 K	0.008	87.54	101.30	58.73	86.75	20.00	1.47	3.16	1.00	33.17
	473 K	0.008	84.72	96.72	58.04	86.00	20.00	1.44	2.84	1.00	31.69