nmp / eo-1 nmp eo-1 leo handbook 1 - 1 september 24-26, 2000 section 1 master timeline (day 1-10)

NMP / EO-1 NMP EO-1 LE&O HANDBOOK

1 - 1September 24-26, 2000

Section 1Master Timeline (Day 1-10)


1 - 2September 24-26, 2000

Launch

Recover Configuration from Safehold

Verify Sun-pointing

Acquire Earth- pointing

Turn on Ali Red Htr Turn on IRU Htr Turn on AST Turn on GPS

Use AST for Kalman Filter

Safehold Logic Test

60 sec Test Propulsion Burn

Pitch, Roll, Yaw, 90 degrees slews for IRU/TAM Cal

Use GPS for time to M5

EO-1 L&EODays 1-3

Thursday, May 18, 2000


1 - 3September 24-26, 2000

End TestBurn

Ali Power On

Power on WARP

X-Band Dump

Format Memory WARP RS 422 Test

X-Band Power On

Short and Normal Images

Ali HOPA Activations and Cover Test

Ali Tests and Internal Cals

EO-1 L&EODays 4-10

cont.



1 - 4September 24-26, 2000

Test ASP Test LAmps Internal Cals &Tests Cover Tests Images

Ali Outgas Mode

Hyperion Power on

AC turn on

AC Images TEC-1 * 2 TEC-2 * 2 TEC-3 * 2

TDRSS Data Rate Tests

Outgassing Mode Check Cryo operation

EO-1 L&EODays 4-10 (cont.)

cont.



1 - 5September 24-26, 2000

Day-By-Day Key Activities Description

. . . Joe Howard


1 - 6September 24-26, 2000

Day 1 Launch

– Fairing Separation First Acquisition through TDRSS at

2k from ATS Non_Coherent– Test Command through TDRSS

AOS McMurdo – Test Command through McMurdo

LOS McMurdo ATS goes to TDRSS– Separation From Launch Vehicle

into B-dot Mode– Solar Array Deployment

AOS Norway at 2k Send Command to switch rate to 32K

– Switch to ATS Buffer B – Playback SSR Launch Data– Close Data Set I

Monitor B-dot

Orbit 3– Drop off TDRSS coverage

but keep transponder on and configured between GN passes

Orbit 4– Verify sun pointing

acquisition– Turn on ALI outgas heater– Turn on IRU heater– Turn on AST– Turn on GPS

Orbit 6– Allow ACS to use Kalman

filter if converged Night Orbits

– Check TDRS 4,6,8 Kbps telemetry


1 - 7September 24-26, 2000

Day 2 Orbit 12 – Update M5 time if needed

Orbit 14– Move Solar Array 10 deg off index– Start ACE Safehold– Monitor safehold control

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

Orbit 17– Acquire Earth pointing mode

Orbit 18– Use GPS for timing in M5


1 - 8September 24-26, 2000

Day 3 Orbit 20– Load ATS– Turn off Slew control for safety

Orbit 28– Enable slew logic

Orbit 29– Pitch Slew out Settle 15 minutes and return (Execute

from ATS)(TDRSS) Orbit 31

– Yaw Slew out and back (from ATS)(TDRSS) Orbit 32

– Roll Slew out and back (from ATS)(TDRSS) Orbit 34

– Enable EFF in Monitor mode


1 - 9September 24-26, 2000

Day 4 Orbit 45

– Turn on X-band RSN– Turn on X-band RF without

WARP RF exciter– Playback S-band WARP RS422

data Orbit 46

– Dump WARP files X-band (Norway and SGS overlap)

Orbit 49– Re-dump WARP X-band data

(Wallops) Orbit 50

– WARP Memory test

Orbit 37– Load ATS

Orbit 41– Update any Power parameters– Turn off ALI radiator heaters– Allow DeltaV logic to execute

Orbit 42– Monitor 60 second thruster

burn from ATS (over Wallops) Orbit 43

– Turn back on the ALI rad heaters

Orbit 44– Turn on WARP and format

memory– RS-422 test


1 - 10September 24-26, 2000

Day 5 Orbit 60

– Enable RTSs for ALI cover opening DCE via ATS

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

Orbit 62– S-band dump of 8 sec DCE– Another 30 sec DCE via ATS

Orbit 64– X-band dump of all ALI data


Orbit 55– Turn on ALI– Turn off ALI radiator heaters

Orbit 56– ALI comprehensive test

Orbit 57– 8 second ALI lamp cal– S-band WARP replay– 30 second test pattern ALI data

collect Orbit 58

– X-band WARP playback Orbit 59

Release Launch Latch for ALI CoverRelease Launch Latch for ALI DiffuserOpen ALI CoverClose ALI Cover


1 - 11September 24-26, 2000

Day 6 Orbit 76

– AC Dark Earth image at TEC 1 for S-band downlink

Orbit 77– AC image at TEC 1 for S-band

downlink Orbit 78

– AC Dark Earth image at TEC 1 for X-band downlink

Orbit 79– AC image at TEC 1 for X-band

downlink– Test TDRSS pass at 4 Kbps

Orbit 80– Test TDRSS pass at 6 Kbps

Orbit 82– Test TDRSS pass at 8 Kbps

Orbit 83– Load ATS– X-band playback of AC data


Orbit 70– Close ALI cover– Turn off ALI radiator heater

Orbit 71– Increase FDC limits in prep for Delta

V– Allow for Delta V to execute

Orbit 72– Monitor 13 minute Delta V via ATS

(TDRSS scheduled as needed) Orbit 73

– Reset FDC limits Orbit 74

– Re-open ALI cover– Re-turn on ALI radiator heaters

Orbit 75– Turn on ALI


1 - 12September 24-26, 2000

Day 7 Orbit 84– Power on Hyperion– Release WARP files with AC data

Orbit 85– Test ASPs– Test HYP Lamps

Orbit 86– HYP short internal cal

Orbit 87– HYP Cryo static drive test– S-band playback of short cal

Orbit 88– HYP heater test

Orbit 89– Heaters back to normal

Orbit 90– Cover open full– Cover open to sun cal position– cover close


1 - 13September 24-26, 2000

Day 8 Orbit 92– Load ATS

Orbit 99– HYP full length cal

Orbit 100– Close ALI cover– Turn off ALI radiator heater– X-band dump of Hyperion data– Allow for Delta V to go

Orbit 101– 12 min Delta V from ATS

Orbit 103– Open ALI cover– Turn on ALI radiator heater– Release Launch Latches on LFSA– Deploy LFSA

Orbit 104– Another full length Hyperion cal

Orbit 107– X-band playback of Hyperion data to Wallops


1 - 14September 24-26, 2000


Orbit 114– Close ALI cover– Turn off ALI radiator heater– Allow for Delta V to execute– Monitor 9 minutes Delta V

Orbit 115– Return ACS to 60 second burn limit

Orbit 116– Open ALI cover– Turn on ALI radiator heater

Orbit 117– HYP Cryo check start

Orbit 118– HYP Cryo check stop

Orbit 119– Hyperion heaters on for outgassing


1 - 15September 24-26, 2000


Orbit 129– All instrument DCE (Procedure or ATS)

Orbit 130– X-band downlink (Alaska)

Orbit 131– X-band downlink (Wallops)

Orbit 132– All instrument short DCE

Orbit 133– S-band dump of short DCE

nmp / eo-1 nmp eo-1 leo handbook 1 - 1 september 24-26, 2000 section 1 master timeline (day 1-10)

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