IGF::OT::IGF PHENOLIC INFUSION OF GLASS PREFORMS THE THERMAL PROTECTION MATERIALS BRANCH (CODE TSM) REQUIRES THE PURCHASE OF TOOLING AND PHENOLIC IMPREGNATION OF GLASS PREFORMS IN ORDER TO INVESTIGATE INSULATING MATERIALS FOR HIGH TEMPERATURE, VARIOUS DURATION HEATING ENVIRONMENTS. APPLICATIONS INCLUDE LANDING PAD STRUCTURES FOR VERTICAL TAKEOFF AND LANDING AIRCRAFT OPERATIONS (E.G. V-22 OSPREY AND F-35B), AIR-BREATHING AND ROCKET PROPULSION TEST STANDS, AND LAUNCH AND RECOVERY PADS FOR ROCKET LAUNCH SYSTEMS AND RETURNING RETRO-PROPULSION SPACECRAFT. VENDOR TO PROVIDE DESIGN, TOOLING, MOLDING, AND FINISHING OF TWO (2) ARC-FURNISHED 3D E-GLASS FIBER PREFORMS WITH THE FOLLOWING DIMENSIONS: 24" X 24" X 0.5 USING THE FOLLOWING PROCESSES: PHENOLIC RESIN INFUSION USING VACUUM ASSISTED RESIN TRANSFER MOLDING OR EQUIVALENT SURFACE DENSIFICATION TO LIMIT LIQUID PERMEABILITY DEGASSING, COMPRESSION MOLDING, AND CURING DIAMOND SAW TRIMMING AND POST-TRIM SEALING OF EXPOSED EDGES