View Larger Image View Larger Image Adapting AM Materials for Spaceflight ApplicationsSamie Murch2021-09-10T02:26:41-05:00 Project Description Primary Purpose: Flammability Resistance Secondary Purpose: Strength / Durability NASA GRC and Zin Tech looked at AM as a solution to hardware development challenges must meet stringent flammability, electrical bonding and environmental requirements Material qualification 5530 HT, coated with 0.004” +0.003/-0.001” Cu + Ni (made by TTH): Flammability – “A” rating at 10 psi, 30% 02 Toxic Off-gassing – “A” rating Adhesion Durability Protective Capability View Peformance Testing on ISS Project Details Categories: Flammability ResistanceStrength / Durability