Table 1 Fitting parameters of the elongation master curve of unaged propellant.
From: Study on elongation master curve of thermal aging composite modified double base propellant
A5 | A6 | A7 | A8 | R2 |
---|---|---|---|---|
0.04144 | 0.2117 | 0.1621 | 0.1873 | 0.983 |
From: Study on elongation master curve of thermal aging composite modified double base propellant
A5 | A6 | A7 | A8 | R2 |
---|---|---|---|---|
0.04144 | 0.2117 | 0.1621 | 0.1873 | 0.983 |