I have a circuit board that is delaminating during the frabracation process. 
The laminate material is Rogers (RO4003) with Pre-Preg supplied from Gore 
(Speedboard-C). The laminate is a Hydrocarbon/woven glass material and the 
Pre-Preg is PTFE material. My question is this a highly realible combination 
of material? Could this combination be used for space applications? How will 
this hold up to thermal extreems of (-60° Celcius to +85° Celcuis) and 
vibration/shock over 8Gs?



Gary Bremer
Manucaturing Engineer CID

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