Last updated: 5 July 1997, 7:30 am PDT
Mission Sequence Planner: AHM
Rover Driver: XX
| SCET | PDT | LST | ||
|---|---|---|---|---|
| Expected uplink time: | 185-00:00 | 00:00 | ||
| Nominal sequence activation time: | 185-00:00 | 00:00 | SOL/00:00 | |
| Nominal sequence abort time: | 185-00:00 | 00:00 | SOL/00:00 | (during command [xxxx]) |
Previous sequence 50110A will nominally be aborted at command [xxxx]
| SCET | PDT | LST | ||
|---|---|---|---|---|
| Expected uplink time: | 185-00:00 | 00:00 | ||
| Nominal sequence activation time: | 185-00:00 | 00:00 | SOL/00:00 | |
| Nominal sequence abort time: | 185-00:00 | 00:00 | SOL/00:00 | (during command [xxxx]) |
Previous sequence 50210T will nominally be aborted at command [xxxx]
| SCET | PDT | LST | ||
|---|---|---|---|---|
| Expected uplink time: | 185-00:00 | 00:00 | ||
| Nominal sequence activation time: | 185-00:00 | 00:00 | SOL/00:00 | |
| Nominal sequence abort time: | 185-00:00 | 00:00 | SOL/00:00 | (during command [xxxx]) |
If used, sequence 50240T will abort sequence 50220T will nominally be aborted at command [xxxx]
MISSION SEQUENCE PLANNER REPORT
SEQUENCE DESCRIPTION
| X Position (m) | Y Position (m) | Heading (deg) | |
|---|---|---|---|
| At Sequence Start** | 0.00 | 0.90 | 0 |
| At End of Sol 2* (predicted) | 0.90 | 0.00 | 0 |
** Vehicle positions are in lander coordinate frame until
sun-finding establishes surface-fixed frame
* at completion of planned SOL's traverse activities assuming nominal execution
| Image Type | X (m) | Y (m) | Z (m) | Imaging Opportunity |
|---|---|---|---|---|
| S-009 | ||||
| S-010 | ||||
Sol 2 Sequence Nominal Downlink (by APID) (Predicted telemetry volume generated between activation of sequence 50210T on SOL 2 and nominal abort of sequence 50220T on morning of SOL 3):
| APID | Name | Predicted #Pkts | Predicted #Mbits |
|---|---|---|---|
| 4 | Health Status | 74 | 0.17227 |
| 5 | Ops/Engr | 38 | 0.02422 |
| 6 | Sequence Status | 61 | 0.01510 |
| 7 | Error Reports | 0 | 0.00000 |
| 8 | Science Imaging | 0 | 0.00000 |
| 9 | Technology Imaging | 0 | 0.00000 |
| 10 | Lander Imaging | 0 | 0.00000 |
| 12 | APXS Results | 0 | 0.00000 |
| 23 | Priority Ops/Engr. | 0 | 0.00000 |
| 24 | Auto Imaging | 0 | 0.00000 |
| 25 | Ops Imaging | 0 | 0.00000 |
| 29 | Traverse Reporting | 0 | 0.00000 |
| TOTAL | 173 | 0.21159 |
SEQUENCE IMPLEMENTATION REPORT
SCIENCE/TECHNOLOGY OBJECTIVES REPORT
| Image Log # | Status | Command | Image Type | APID | Camera | Exposure | Compression | Rows | Columns |
|---|---|---|---|---|---|---|---|---|---|
| ACCEPTED | [1421] | lander | 10 | left | auto | Y | 245-485 | 152-664 | |
| ACCEPTED | [1422] | lander | 10 | left | reuse | Y | 5-245 | 152-664 | |
| ACCEPTED | [1423] | lander | 10 | right | auto | Y | 245-485 | 92-604 | |
| ACCEPTED | [1424] | lander | 10 | right | reuse | Y | 5-245 | 92-604 | |
| ACCEPTED | [1425] | lander | 10 | rear | auto | N | 105-485 | 204-560 | |
| APXS Log # | Status | Time (UTC) | Command # | APXS Command |
|---|---|---|---|---|
| MAE Log # | Status | Time (UTC) | Command # | MAE Command |
|---|---|---|---|---|
| ACCEPTED | 186 02:10:18 | [1429] | Set Parameter: dust_cvr to 800 | |
| ACCEPTED | 186 02:10:22 | [1430] | MAE Experiment | |
| ACCEPTED | 186 05:15:11 | [1437] | Set Parameter: dust_cvr to 800 | |
| ACCEPTED | 186 05:15:15 | [1438] | MAE Experiment | |
| ACCEPTED | 187 02:49:49 | [1472] | Set Parameter: dust_cvr to 800 | |
| ACCEPTED | 187 02:49:53 | [1473] | MAE Experiment | |
| ACCEPTED | 187 04:53:07 | [1479] | Set Parameter: dust_cvr to 800 | |
| ACCEPTED | 187 04:53:11 | [1480] | MAE Experiment | |
| WAE Log # | Status | Time (UTC) | Command # | WAE Command |
|---|---|---|---|---|
| Soil Log # | Status | Time (UTC) | Command # | Soil Mechanics Command |
|---|---|---|---|---|
PRESS RELEASE
The primary objective for rover operations during SOL 2 is to diagnose and correct the rover/lander communications anomaly that was first detected during SOL 1 operations. If the problem is corrected early in SOL 2, then rover standup and ramp egress will be performed.
Web Page Author: Andrew H. Mishkin
All information on this site, including text and images describing the Rover is copyright © 1997, Jet Propulsion Laboratory, California Institute of Technology and the National Aeronautics and Space Administration.