Last updated: 09/18/97
Mission Sequence Planner: Art Thompson
Rover Driver: BC
| SCET | PDT | LST | ||
|---|---|---|---|---|
| Nominal sequence activation time: | 262-01:16 | SOL75-10:20 | ||
| Nominal sequence abort time: | 263-01:01 | SOL76-09:34(during command [25094]) |
Previous sequence 57410 will nominally be aborted at command 24112
MISSION SEQUENCE PLANNER REPORT
SEQUENCE DESCRIPTION
| X Position (m) | Y Position (m) | Heading (deg) | |
|---|---|---|---|
| At Sequence Start** | -11.502 | -3.006 | 302.43 |
| At End of Sol 76* (predicted) | -12.038 | -3.456 | 120 |
** 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 |
|---|---|---|---|---|
| S0055 (EOD) | -88.930 | -13.268 | -0.114 | After 11:30 LST |
| S0055 | -83.675 | -32.978 | -0.114 | |
| S0055 | -4.334 | -0.732 | -0.114 | |
| S0055 | -4.067 | -1.733 | -0.114 | |
SEQUENCE IMPLEMENTATION REPORT
SCIENCE/TECHNOLOGY OBJECTIVES REPORT
Web Page Author: Art Thompson
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.