Step 1: Write the thin-cylinder stress formulas.
For a thin cylindrical vessel of diameter \(D\) and wall thickness \(t\) under internal pressure \(p\), the hoop stress is \(\sigma_h = \dfrac{pD}{2t}\) and the longitudinal stress is \(\sigma_l = \dfrac{pD}{4t}\), so \(\sigma_l = \sigma_h/2\).
Step 2: Write the hoop strain using Hooke's law for biaxial stress.
At the outer surface the radial stress is negligible for a thin shell, so this is a biaxial stress state. The circumferential strain is \(\varepsilon_h = \dfrac{1}{E}(\sigma_h - \nu\sigma_l) = \dfrac{1}{E}\left(\dfrac{pD}{2t} - \nu\dfrac{pD}{4t}\right) = \dfrac{pD}{2tE}\left(1 - \dfrac{\nu}{2}\right)\).
Step 3: Solve for the pressure.
Rearranging, \(p = \dfrac{2tE\varepsilon_h}{D(1 - \nu/2)}\). With \(t = 0.015\) m, \(E = 210 \times 10^9\) Pa, \(D = 3\) m, \(\nu = 0.3\) (so \(1-\nu/2 = 0.85\)) and \(\varepsilon_h = 0.00034\):
\(p = \dfrac{2 \times 0.015 \times 210 \times 10^9 \times 0.00034}{3 \times 0.85} = \dfrac{2.142 \times 10^6}{2.55} = 8.4 \times 10^5\) Pa.
Final Answer:
Converting to kPa gives the permissible pressure directly from the allowable strain.
\[ \boxed{p = 840.0 \ \text{kPa}} \]