1. Solar Probe Plus FIELDS V5 Mechanical Pre-Ship Review April 10, 2017
David Glaser
FIELDS Mechanical Engineer
Space Sciences Lab
University of California, Berkeley

2. Attached Documents
SPF ANT 076 Rev A V5 Indentured Drawings List (Drawings available for viewing on request)
SPF ANT PRC 016 Rev B V5 As-Built Assembly Procedure
SPF ANT PRC 018 Rev A V5 Integration Procedure
SPF ANT ICD 005 Rev A V5 Antenna MICD
SPF ANT 069 Rev D V5 FM Vibe Test Procedure_RevD

3. 1. As Built Data
The included document SPF-ANT-PRC-016 V5 As-Built Assembly Procedure contains all relevant as-built data, including part description.
The included document SPF-ANT-076RA V5 FIELDS V5 Indentured Drawings List-signed contains a list of all drawings and their revisions.

4. 1. Storage and Integration Requirements
Storage of the V5 instrument requires ESD safety precautions. A connector saver will be on the pigtail connector, and a shorting connector on the connector saver. The instrument does not require purging or an inert atmosphere.
The included document SPF-ANT-PRC-018 V5 Integration Procedure contains instructions for integration.
The included document SPF-ANT-ICD-005 V5 Antenna MICD contains all relevant mechanical interface data.
Mechanically, the most vulnerable parts of the V5 instrument are the two small antennas. Care must be taken to not bump into them.
Prior to I&T, the instrument will be stored in it’s shipping container.
During I&T, when on the spacecraft, the V5 instrument will usually have its red-tag cover on.
During I&T, when not on the spacecraft, the V5 will be stored on a grounded bench stand and covered with conductive plastic.
Except in the case of observatory level environmental tests, the V5 instrument will be inside a protective red tag cover.

5. 1. As Built Data – Final Configuration Photographs
Additional Photographs of the flight hardware are located at:

6. 1. As Built Data – Final Configuration Photographs
Red Tag
Cover

7. Evidence of Acceptance by Developer QA
See SPF ANT PRC 016 V5 As-Built Flight Assembly Procedure

8. 9. Storage and Integration Requirements
Storage of the V5 instrument requires ESD safety precautions. A connector saver will be on the pigtail connector, and a shorting connector on the connector saver.
The instrument does not require purging or an inert atmosphere.
Prior to I&T, the instrument will be stored in it’s shipping container.
During I&T, when not on the spacecraft, the V5 will be stored on a grounded bench stand and covered with conductive plastic.
Except in the case of observatory level environmental tests, the V5 instrument will be inside a protective red tag cover.