Step 1: Write formula for escape velocity.
\[
V_e = \sqrt{\frac{2GM}{R}}
\]
Step 2: Substitute new mass and radius.
For the planet:
\[
M' = 3M,\quad R' = 3R
\]
Step 3: Calculate new escape velocity.
\[
V'_e = \sqrt{\frac{2G(3M)}{3R}} = \sqrt{\frac{2GM}{R}} = V_e
\]
Step 4: Conclusion.
The escape velocity remains unchanged.