SATPC0041497 Tab 04 4 SOW..pdf
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- Attached to
- Fiber Optic Sensor for Use in a Novel Microwave Ignition System. Federal contract opportunity
- Solicitation number
- 80NSSC26936316Q
About this file
This is a Statement of Work (SOW) for fiber optic instrumentation to support NASA Marshall Space Flight Center's (MSFC) testing of a novel microwave ignitor system for the Advanced Space Propulsion Formulation Task. The contractor must provide fiber optic sensors capable of simultaneously reading temperature and pressure, capable of withstanding up to 500 psi and transient temperatures up to 1500°C with resistance to electromagnetic interference (EMI). The work includes delivery of an integrator to convert optical signals to computer-readable electric signals, associated software for instrumentation operation, and fiber optic cable connections from the test article to the test bed instrumentation.
Specific deliverables include four NovaPT™-E600 sensors, one Fasedyne-1000-4-custom integrator, four optical fiber cables, with a required lead time of 10 weeks. All deliverables must be shipped to Marshall Space Flight Center, Huntsville, AL 35812. The SOW does not specify pricing, response dates, award dates, or contract vehicle information.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0041497 Tab 10 RFQ Open Market Template.pdf | ||
| SATPC0041497 Tab 06 BNJ..pdf |
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Text version
Fiber Optic Instrumentation for Use with Microwave Ignitor
STATEMENT OF WORK
1. Objective/Requirements
NASA Marshall Space Flight Center (MSFC) requires the capability to test and measure the data of a novel microwave ignitor system. The use of fiber optic instrumentation severely reduces any risk of electromagnetic interference (EMI) to both instrumentation and facility computer systems. This effort is in support of the center’s Advanced Space Propulsion Formulation Task.
2. Engineering Requirements
a. Fiber optics sensors capable of reading both temperature and pressure a single sensor.
b. Being able to withstand up to 500 psi
c. Being able to withstand transient temperatures up to 1500°C
d. Resistance to EMI
e. Integrator able to convert optical signal into a electric signal readable by a computer
f. Any software associated with operation of instrumentation.
g. Fiber optical cable from test article to test bed instrumentation bed.
3. Shipping:
Contractor shall ship all deliverables to:
Marshall Space Flight Center Huntsville, AL 35812
4. Deliverables
1. NovaPT™-E600, Quantity 4
2. Fasedyne-1000-4-custom, Quantity 1
3. Optical fiber cable, Quantity 4
4. Lead Time: 10 Weeks
File details come from the government source that posted it. Updated .