Micro-miniature_Transducer_SOW.docx

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Kulite Micro-Miniature Transducers Federal contract opportunity
Solicitation number
NNM16608446Q
Issued by
National Aeronautics and Space Administration Marshall Space Flight Center

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Note Wire LEMO connectors are NOT needed and have been removed from the SOW.

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NNM16608446Q_Terms_and_Conditions_and_Statement_of_Work.pdf PDF

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NNM16608446Q

Statement of Work (SOW) For Kulite Semiconductor Products, Inc. in support of the Space Launch System (SLS) Ascent Unsteady Aerodynamics Wind Tunnel Test Model Project The Period of Performance for the entire effort is APT to 5/01/2017. Delivery of the pressure transducers is 18 to 22 weeks after authorization to proceed.

Base Effort: The Contractor shall provide Kulite-based ultra-miniature unsteady pressure transducers identified below to be used in SLS models tested in a wind tunnel at AMES to acquire updates including verification data required to move forward to the Critical to the Critical Design Review (CDR).

The test instrumentation is for use in the SLS ascent aeroacoustic testing and must be interchangeable with previously procured transducers Kulite XCL-072-15A installed in the SLS Ascent Aeroacoustic Test. Existing instrumentation cabling and hardware, including the transducer amplifiers and holders have been custom designed for the characteristics of the sensors proposed in this procurement.

The subject transducers must meet the following requirements:

Description
Qty

PRESSURE TRANSDUCER

Kulite XCL-072-15A .075” Diameter; .375 Long; 3 wire 57 KHz Bandwidth +- 0.5dB Pressure Range: 15 PSIA Consists of:

XCL-072 Base PL Flush Diaphragm No screen, RTV backfill ELD Special Calibration Terminates with Omnetics connector A12406 Compatible with MSFC B Screen Holder (see drawing below)

MSFC B Screen Holder

Delivery: 18 to 22 weeks After Receipt of Order (ARO) Shipping: F.O.B. destination Warranty: 12 months from date of manufacture image3.png image4.png image5.png image6.png image1.png image2.png

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