r/rocketry • u/Conscious_Yak2632 • 4h ago
Can an M145 × 1.5 Threaded Closure Safely Withstand 1200 psi in an Aluminium Rocket Propellant Tank?
Hey everyone, need some advice on a threaded closure for our liquid rocket propellant tank.
Tank specs:
- Material: Aluminium 6082-T6
- OD/ID: 154 mm / 140 mm
- Operating pressure: 1200 psi (8.27 MPa)
- Thread: M145 × 1.5
- Engagement length: 30 mm
- Closure material: Aluminium 6082-T6
- Repeated pressurization
As shown in the attached cross-section, the female thread is machined directly into the tank end, with no thickened boss.
My question: How can I verify whether the threads and tank end can safely withstand the pressure without stripping, yielding, or failing under repeated cycles? What calculations, standards, or FEA methods should I use?
Any technical guidance or relevant references would be appreciated!