SOW.pdf
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- Solicitation number
- 8NSSC23838938Q
About this file
This document outlines requirements for a turbo pumping station procurement opportunity with the National Aeronautics and Space Administration. The Cryogenics and Fluids Branch at NASA Goddard Space Flight Center requires a HiCube 300 PRo/ACP 15 Turbo pumping station, model number DN 100 CF-F, to simulate lunar-like environments and measure thermophysical properties of engineered lunar soil samples as part of ongoing research and development work funded by NASA. Key requirements for the turbo pumping station include an operating pressure of less than 10-7 mbar and the ability to achieve and maintain high, stable vacuum conditions for extended periods of time. Offerors should reference solicitation number 8NSSC23838938Q for additional details on response requirements and evaluation criteria.
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Text version
Pfeiffer Vacuum Inc. Turbo pumping station Procurement
1. Objective/Requirements The Cryogenics and Fluids Branch (Code 552) at the NASA Goddard Space Flight Center (GSFC) requires the procurement of a turbo pumping station for the effective thermal conductivity measurement of engineered lunar soil work. This is a research and development work funded by NASA NESC to further develop for future ISRU applications. This pumping station will be used to simulate lunar-like environment and to measure thermophysical properties of target samples.
2. Requirements of the system
The contractor shall provide the turbo pumping station with the following specifications:
1. Operating pressure: < 10-7 mbar or <10-8 Torr
3. Place of Performance NASA-GSFC located in Building 7, Room 039A.
4. Period of Performance The pumping station shall be delivered to GSFC Branch 552 within 38 weeks of ARO.
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