| IOC-MIPS_035a | 10030E | ||||||||
| Title: | Combined Electronics EEPROM Test | ||||||||
| Objective: | Validate combined electronics EEPROM | ||||||||
| Description: | EEPROM check - transition to BOOT, checksum boot and operate images, dump EEPROM, leave CE | ||||||||
| powered for 24 hours to monitor thermal performance, send time code update every hour to monitor | |||||||||
| S/C to CE clock synchronization | |||||||||
| Place in Schedule: | After CE aliveness check. | ||||||||
| Required Conditions: | None -- CE must remain on for 24 hours. | ||||||||
| Resources: | |||||||||
| duration (best estimate) | 0.25 hrs | for actual tests, but CE must remain on for 24 hrs | |||||||
| real time downlink (Y / N) | Yes | ||||||||
| special post event actions (Y / N) | No | ||||||||
| Outcome: | |||||||||
| description | CE telemetry data. | ||||||||
| can proceed in parallel with other activity | Yes | ||||||||
| must outcome be confirmed before next event / test /activity | Yes | ||||||||
| method of confirmation (sensor TLM, data analysis, etc.) | TLM diagnostic data | ||||||||
| estimate of data turn around if required for confirmation | 6 hrs | ||||||||
| Unique or included in planned uplink or downlink/analysis tool | Unique. | ||||||||
| Contingency Plan: | Find CE software bug and reload flight software. | ||||||||
| "What if..." | |||||||||
| IOC Critical | Yes | ||||||||
| Data Volume: | None -- RT telemetry | ||||||||
| References: | |||||||||
| Template last updated: | 23-Jun-99 | ||||||||
| Template written by: | William B. Latter | ||||||||