Numerical Simulation of Coupling Thermal and Mechanical Influence on Submerged Nozzle in Solid Rocket Motor

Table 3

Material properties of carbon-carbon composite.

			/		/			/		/		/
300	1890	65.8	86.5	1.3E-6	1.2E-6	920	42.5E3	64.8E3	22.5E3	20.6E3	0.22	0.11
500		60.6	84.2			1001
800		59.5	81.2			1279
1100		55.1	71.2			1487
1400		51.3	62.5	1.4E-6	1.3E-6	1567
1700						1785
2000
2300