Hello,
What are you guys' thoughts on using prepreg as the layup material for T2T?
My concern is that since there is already the optimal ratio of resin in the fiber matrix, it does not leave much adhesive for bonding to the air frame and fin surfaces.
In addition, do you guys think that the fin/air frame can handle 300 deg Fahrenheit for curing the prepreg? They were obtained from RocketryWarehouse.
Let me know what you guys think!
Thanks!
Alexis
What are you guys' thoughts on using prepreg as the layup material for T2T?
My concern is that since there is already the optimal ratio of resin in the fiber matrix, it does not leave much adhesive for bonding to the air frame and fin surfaces.
In addition, do you guys think that the fin/air frame can handle 300 deg Fahrenheit for curing the prepreg? They were obtained from RocketryWarehouse.
Let me know what you guys think!
Thanks!
Alexis