Table 1.
Origin of a collagen kind as a part of scaffold | Compression stress at a strain value 10%, kPa | Compression stress at a strain value 50%, kPa | The thickness of the scaffold |
---|---|---|---|
Collagen №1 (n = 5) | 0.50 ± 0.06 | 9.18 ± 0.90 | 1.86 ± 0.09 |
Collagen №2 (n = 5) | 0.49 ± 0.05 | 5.61 ± 0.26 * | 1.75 ± 0.05* |
Note: * – p < 0.05 – Wilcoxon test.