Anyone have any design guidlines for composite parts vacuum bag invar tooling? Specifically plate thicknesses and egg crate cutout criteria relating to heat dissapation?
snipped-for-privacy@tagaerospace.com
Anyone have any design guidlines for composite parts vacuum bag invar tooling? Specifically plate thicknesses and egg crate cutout criteria relating to heat dissapation?
snipped-for-privacy@tagaerospace.com
Forgot to mention, 250 deg cure, high production rates and large (aircraft fuselage frames, C sections with flanged lightning holes)
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