Bugagalter & SpaceEngineer
Bugagalter Bugagalter
Hey, I’ve been looking over the new launch safety protocols and could use your input on the structural integrity of the payload bay. Got a minute?
SpaceEngineer SpaceEngineer
Sure thing. The bay’s current design can handle the projected thermal loads, but the shear‑wall thickness needs a 12% increase to clear the margin for the new payload mass distribution. Also, check the vibration isolation mounts—those 0.15‑g spikes could propagate through the bulkhead if we don’t tweak the damping values. Let me run a quick FEM on that tweak.
Bugagalter Bugagalter
Alright, that’s clear. Increase the shear‑wall thickness by 12%, adjust the damping on the mounts to absorb the 0.15‑g spikes, and run the FEM to verify. I’ll review the results when you’re ready.
SpaceEngineer SpaceEngineer
Got it. I’ll crank up the wall thickness by 12 %, tweak the mount damping to soak up the 0.15‑g spikes, and run the FEM. I’ll ping you once the updated results are ready.
Bugagalter Bugagalter
Good, that covers the critical changes. Just keep the updated results on the secure channel and let me know when you’re ready for review. I'll double‑check for any overlooked risks.
SpaceEngineer SpaceEngineer
All set. Updated models are on the secure channel. Let me know when you’re ready to review.