Statement of Work.pdf

PDF 85 KB Posted

Attached to
Accelerometer Measurement System Federal contract opportunity
Solicitation number
80NSSC230819
Issued by
National Aeronautics and Space Administration Shared Services Center

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STATEMENT OF WORK

1. Objective/Requirements

The On-orbit Servicing Assembly and Manufacturing Mission 1 (OSAM-1) is using a Flight Accelerometer Measurement System (AMS) to sense the acceleration of the spacecraft. This is the only unit used to collect this data for the mission. The non-flight version, or Engineering Test Unit (ETU), of the AMS will be used to aid in the development of software for the spacecraft and in troubleshooting issues at the spacecraft and space vehicle level. The AMS ETU will be used to verify flight software and run it with their AMS emulator and ensure that the results match. The AMS ETU will be used in conjunction with tests on the Spacecraft Integration and Test (I&T) floor that have been completed. The engineering unit shall be compatible with the Zin AMS Flight unit, ‘ZIN MMSAMS Unit’.

2. Characteristics, Scope, and Specs

The contractor shall configure the ZIN MMS AMS Unit and deliver the unit to Maxar Technologies in Palo Alto California.

3. Place of Performance Maxar Technologies – Palo Alto, California

4. Period of Performance Unit delivered by April 18, 2023.

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