1. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 1 September 24-26, 2000 Section 1 Master Timeline (Day 1-10)

2. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 2 September 24-26, 2000

3. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 3 September 24-26, 2000

4. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 4 September 24-26, 2000

5. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 5 September 24-26, 2000 Day-By-Day Key Activities Description... Joe Howard

6. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 6 September 24-26, 2000 Day 1 u Launch –Fairing Separation u First Acquisition through TDRSS at 2k from ATS Non_Coherent –Test Command through TDRSS u AOS McMurdo –Test Command through McMurdo u LOS McMurdo ATS goes to TDRSS –Separation From Launch Vehicle into B-dot Mode –Solar Array Deployment u AOS Norway at 2k Send Command to switch rate to 32K –Switch to ATS Buffer B –Playback SSR Launch Data –Close Data Set I u Monitor B-dot u Orbit 3 –Drop off TDRSS coverage but keep transponder on and configured between GN passes u Orbit 4 –Verify sun pointing acquisition –Turn on ALI outgas heater –Turn on IRU heater –Turn on AST –Turn on GPS u Orbit 6 –Allow ACS to use Kalman filter if converged u Night Orbits –Check TDRS 4,6,8 Kbps telemetry

7. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 7 September 24-26, 2000 Day 2 u Orbit 12 –Update M5 time if needed u Orbit 14 –Move Solar Array 10 deg off index –Start ACE Safehold –Monitor safehold control u Orbit 16 –Exit safehold –Turn back on IRU heaters –Turn back on AST power –Turn back on GPS power –Turn back on ALI outgas heater –Use Kalman filter u Orbit 17 –Acquire Earth pointing mode u Orbit 18 –Use GPS for timing in M5

8. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 8 September 24-26, 2000 Day 3 u Orbit 20 –Load ATS –Turn off Slew control for safety u Orbit 28 –Enable slew logic u Orbit 29 –Pitch Slew out Settle 15 minutes and return (Execute from ATS)(TDRSS) u Orbit 31 –Yaw Slew out and back (from ATS)(TDRSS) u Orbit 32 –Roll Slew out and back (from ATS)(TDRSS) u Orbit 34 –Enable EFF in Monitor mode

9. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 9 September 24-26, 2000 Day 4 u Orbit 45 –Turn on X-band RSN –Turn on X-band RF without WARP RF exciter –Playback S-band WARP RS422 data u Orbit 46 –Dump WARP files X-band (Norway and SGS overlap) u Orbit 49 –Re-dump WARP X-band data (Wallops) u Orbit 50 –WARP Memory test u Orbit 37 –Load ATS u Orbit 41 –Update any Power parameters –Turn off ALI radiator heaters –Allow DeltaV logic to execute u Orbit 42 –Monitor 60 second thruster burn from ATS (over Wallops) u Orbit 43 –Turn back on the ALI rad heaters u Orbit 44 –Turn on WARP and format memory –RS-422 test

10. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 10 September 24-26, 2000 Day 5 u Orbit 60 –Enable RTSs for ALI cover opening DCE via ATS u Orbit 61 –One 8 second and two 30 sec DCE execution out of ATS (out of view) –Move cover to outgas position –Turn Heaters on to outgassing mode –Turn on Radiator Heaters u Orbit 62 –S-band dump of 8 sec DCE –Another 30 sec DCE via ATS u Orbit 64 –X-band dump of all ALI data u Orbit 52 –Load ATS u Orbit 55 –Turn on ALI –Turn off ALI radiator heaters u Orbit 56 –ALI comprehensive test u Orbit 57 –8 second ALI lamp cal –S-band WARP replay –30 second test pattern ALI data collect u Orbit 58 –X-band WARP playback u Orbit 59 Release Launch Latch for ALI Cover Release Launch Latch for ALI Diffuser Open ALI Cover Close ALI Cover

11. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 11 September 24-26, 2000 Day 6 u Orbit 76 –AC Dark Earth image at TEC 1 for S- band downlink u Orbit 77 –AC image at TEC 1 for S-band downlink u Orbit 78 –AC Dark Earth image at TEC 1 for X- band downlink u Orbit 79 –AC image at TEC 1 for X-band downlink –Test TDRSS pass at 4 Kbps u Orbit 80 –Test TDRSS pass at 6 Kbps u Orbit 82 –Test TDRSS pass at 8 Kbps u Orbit 83 –Load ATS –X-band playback of AC data u Orbit 66 –Load ATS u Orbit 70 –Close ALI cover –Turn off ALI radiator heater u Orbit 71 –Increase FDC limits in prep for Delta V –Allow for Delta V to execute u Orbit 72 –Monitor 13 minute Delta V via ATS (TDRSS scheduled as needed) u Orbit 73 –Reset FDC limits u Orbit 74 –Re-open ALI cover –Re-turn on ALI radiator heaters u Orbit 75 –Turn on ALI

12. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 12 September 24-26, 2000 Day 7 u Orbit 84 –Power on Hyperion –Release WARP files with AC data u Orbit 85 –Test ASPs –Test HYP Lamps u Orbit 86 –HYP short internal cal u Orbit 87 –HYP Cryo static drive test –S-band playback of short cal u Orbit 88 –HYP heater test u Orbit 89 –Heaters back to normal u Orbit 90 –Cover open full –Cover open to sun cal position –cover close

13. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 13 September 24-26, 2000 Day 8 u Orbit 92 –Load ATS u Orbit 99 –HYP full length cal u Orbit 100 –Close ALI cover –Turn off ALI radiator heater –X-band dump of Hyperion data –Allow for Delta V to go u Orbit 101 –12 min Delta V from ATS u Orbit 103 –Open ALI cover –Turn on ALI radiator heater –Release Launch Latches on LFSA –Deploy LFSA u Orbit 104 –Another full length Hyperion cal u Orbit 107 –X-band playback of Hyperion data to Wallops

14. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 14 September 24-26, 2000 Day 9 u Orbit 109 –Load ATS u Orbit 114 –Close ALI cover –Turn off ALI radiator heater –Allow for Delta V to execute –Monitor 9 minutes Delta V u Orbit 115 –Return ACS to 60 second burn limit u Orbit 116 –Open ALI cover –Turn on ALI radiator heater u Orbit 117 –HYP Cryo check start u Orbit 118 –HYP Cryo check stop u Orbit 119 –Hyperion heaters on for outgassing

15. NMP / EO-1 NMP EO-1 LE&O HANDBOOK 1 - 15 September 24-26, 2000 Day 10 u Orbit 121 –Load ATS u Orbit 129 –All instrument DCE (Procedure or ATS) u Orbit 130 –X-band downlink (Alaska) u Orbit 131 –X-band downlink (Wallops) u Orbit 132 –All instrument short DCE u Orbit 133 –S-band dump of short DCE