Summary
Requirement for pressure sensing instrument. This SOW covers the provision of three distinct types of pressure-sensing instruments, including rocket motor ICP® dynamic pressure sensors, cryogenic ICP® pressure sensors, and high-pressure charge-mode ballistic pressure sensors, along with the required associated hardware such as charge converters, replacement cooling tube sets, low-noise coaxial cables, coaxial couplers, brass seals, and mechanical/ electrical adapters. To ensure clarity and compatibility with NASA procurement processes, each instrument class and associated hardware is defined as a unique Contract Item Line Number (CLIN), with its own requirements, quantities, and period of performance defined below. The vendor will furnish all labor and equipment necessary to (1) manufacture dynamic pressure sensors onsite, (2) calibrate sensors onsite, and (3) perform quality inspections onsite to meet technical specifications quoted above. Deliverables must meet the technical requirements outlined under each CLIN
and be suitable for integration into MSFC propulsion test facilities. The vendor will warrant that the sensors to be free of defects in materials and workmanship for a period of one (1) year from the date of original purchase. If the sensors fail during the warranty period, the vendor will repair, replace or exchange it without charge.