IGF::OT::IGF8 FOOT HIGH TEMPERATURE TUNNEL MACH 6 NOZZLE. THE SCOPE OF THIS TASK ORDER IS TO PROCURE ALL MATERIALS AND HARDWARE REQUIRED FOR THE FABRICATION OF THE M6N AND TO FABRICATE THE NOZZLE BASED ON THE COMPLETED AND APPROVED DESIGN PRODUCED UNDER SMAAART CONTRACT NNL10AA05B, TASK NNL15AB92T. THE NOZZLE HARDWARE TO BE FABRICATED IS DEPICTED IN FIGURE 1 (EXHIBIT A OF THE STATEMENT OF WORK [SOW]). DRAWINGS OF THE NOZZLE COMPONENTS ARE INCLUDED AS AN ATTACHMENT TO THE SOW. THE NOZZLE CONSISTS OF COMPONENTS DENOTED AS PRESSURE VESSELS AND LINERS. THE LINERS ARE THE ACTIVELY COOLED COMPONENTS THAT FORM THE NOZZLE INTERNAL FLOW PATH. THE PRESSURE VESSELS ARE THE COMPONENTS INTO WHICH THE LINERS ARE ASSEMBLED. THE PRESSURE VESSELS SHALL BE AMERICAN SOCIETY OF MECHANICAL ENGINEERS (ASME) CODE STAMPED COMPONENTS RATED FOR THE MAXIMUM EXPECTED PRESSURE AND TEMPERATURE CONDITIONS POSSIBLE IN EACH NOZZLE SECTION. THE FABRICATED NOZZLE COMPONENTS SHALL MEET THE REQUIREMENTS OF LPR1710.40 REV M, LANGLEY RESEARCH CENTER PRESSURE SYSTEMS HANDBOOK, LPR1710.15 REV J, WIND TUNNEL MODEL SYSTEMS CRITERIA, AND THE ASME BOILER AND PRESSURE VESSEL CODE (LATEST REVISION), AS APPLICABLE.