btrueblood,
thanks for your answer. I would like to contact prime and/or agency only after the internal review (we are still in a development phase...so we have time) and now your answer clarify a bit my doubt. I knew that the question was too generic but this was because we could use aluminum...
Thanks Cory.
Yuo're right, it was written in a bad way.
The question is if it is possible to use aluminum and aluminum alloy without anodizing or passivating os S/C parts or on payload.
Bye,
Emilio
Thanks for your answer. Actually we are still open to different solutions. Main ontraints are the max temperature reachable (290 °C), compatibility with our propellant (so probably solithane or Nytemp are not aplicable) and dimensions M2 and M3. So the best solution could be helicoil (screw lock...
I saw that in the thread24-131607 Timelord suggest Helicoil as screw locker. For space application is there any standard? Could you suggest company for space qualified helicoil?
Thanks,
emilio
Hi guys,
Good morning to everybody!
I hope you can help me.
I wonder if it is possible to use Aluminum or Aluminum alloys on the spacecrafts or is it mandatory to anodize (alodyne or others) the AL parts? Could you indicate me a NASA std or ECSS to find something?
Thanks in advance,
Emilio
