1. Solar Probe Plus FIELDS Main Electronics Package iPER Agenda Feb 2, 2017

2. Agenda

3. Review Team

4. Purpose The Instrument PER (I-PER) has two main purposes:
To evaluate the planned environmental test and calibration plans, test flow, and ground support equipment and facilities to assure that they meet the instrument needs
To assure that a proper baseline of performance has been established for the instrument, and that it is ready to begin a qualification test program to demonstrate end-to-end or system performance
Top level I-PER assumptions are :
All flight hardware is fabricated and tested at the board/component level;
Flight Instrument is assembled and initial Comprehensive Performance Test (CPT) is complete;
All flight software functions have been coded and unit-, integration-, and system-tested;
The test verification matrix is complete with updates for tests that have completed;
Test procedures include stimuli, measurement tolerances, and contamination control;
Test facilities have been identified and are approved for use;
Baseline test plan is distributed;
Test Procedures are available for review;
Exceptions to “test as you fly; fly as you test” are documented.

5. SPP/FIELDS MEP Two Sides Each has a Spacecraft I/F
Each has a Magnetometer
Each has Antenna Biasing
Each has a Power Supply
FIELDS1 also has
Data Controller Board
Radio Frequency Spectrometer
Digital Fields Board
SCM Calibration Control
Absolute Time Sequencer
TDS I/F
FIELDS2 also has
Time Domain Sampler
DCB I/F
SWEAP I/F
MEP

6. SPP/FIELDS Unchanged from CDR Five voltage sensors
V2 electric antenna
Unchanged from CDR
Five voltage sensors
Two Fluxgate magnetometers
One Search-Coil Magnetometer
Main Electronics Package
V3 electric antenna
MAGi, MAGo
MEP
V4 electric antenna
V5, SCM
V1 electric antenna

7. EM MEP TV Photo

8. Entrance Criteria

9. References and Document List
Source: ftp://apollo.ssl.berkeley.edu/pub/FIELDS/1_Management/1.7_Meetings/PhaseC_ _MEP_PER/Documents/

10. Success Criteria