Tab 04 4 Statement of Work
Updated
A PDF document (470 KB) attached to High-precision X-ray beamline slits for integration into a custom-built X-ray reflectometer system, from the National Aeronautics and Space Administration. Due Nov 3, 2026, 9:00 AM (UTC-6).
File name: SATPC0043050 Tab 04 4 SOW.pdf
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Statement of Work – High-precision slits for new X-ray ray reflectometer system MSFC ST12 requires the procurement of two high-precision, vacuum-compa ble, X-ray beamline slit screens that are capable of remote blade mo on for use in a custom X-ray reflectometer system currently in development. The two slit screens specifica ons are listed below:
4 Blade Slit: 30 mm x 30 mm max aperture; 1 micron step resolu on; 4 independently ac vated, highly polished WC blades with 0.5 deg knife-edge; integrated high-precision guiding rail system and stepping motors. Special prepara on for enabling high-vacuum compa bility (<1e-6 mbar; <1e-6 Torr). Custom mounted DN100/40CF reducer flange mounted upstream and downstream.
2 Blade Slit: 8 mm x 8mm maximum aperture; 1.016 micron step resolu on for aperture, 0.508 micron step resolu on for transla on; 2mm-thick WC blades with 2 deg knife-edge; Special prepara on for enabling high-vacuum compa bility (<1e-6 mbar);
Requirements:
Vendor to customize and provide a 4-blade X-ray beam slit (IB-C30-HV) and a 2-blade X-ray beam slit (AT-C8-HV-DEMI) for integra on into custom-built X-ray ray reflectometer system for thin film coa ng characteriza on and research and development.
Es mated period of performance or lead- me for delivery: 6-8 weeks
Place of Performance: Marshall Space Flight Center, 35812-0001
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