franck
Aerospace
- May 29, 2001
- 48
Hi all,
I would like to qualify our bonding process for the heaters that are going to remain permanently attached on a Spacecraft.
I am trying to calculate an Acceleration Factor for the adhesive (Scotchweld 3M). Currently I am guessing a Coffin-Manson exponent of 6 but I am not convinced if it is conservative enough.
Do you have some value or some reference to suggest?
Franck
I would like to qualify our bonding process for the heaters that are going to remain permanently attached on a Spacecraft.
I am trying to calculate an Acceleration Factor for the adhesive (Scotchweld 3M). Currently I am guessing a Coffin-Manson exponent of 6 but I am not convinced if it is conservative enough.
Do you have some value or some reference to suggest?
Franck
