THEMIS MRR I&T − 1 GSFC, January 5, 2007

Integration and Test

THEMIS MRR I&T − 2 GSFC, January 5, 2007

Integration Agenda

Recent Activities• Environmental Tests Completed• Delivery to Astrotech• Probe Processing• Fueling Preparations• Carrier Processing

Probe and Instrument Status• Instrument Status and Remaining Items• Probe Status and Remaining Items• Integration Plan

Review Process • RFAs in Work• Reviews Ahead

THEMIS MRR I&T − 3 GSFC, January 5, 2007

Environments

Thermal Vacuum

Acoustics

Spin Balance

EMC

VibrationMagnetics

THEMIS MRR I&T − 4 GSFC, January 5, 2007

Probe Processing

Bolt Cutter Installation

Performance Tests

Solar Array Illumination

Delivery to ASO

THEMIS MRR I&T − 5 GSFC, January 5, 2007

Probe Fueling Preps

FM2/FM3 Thermal Vacuum

Vibration

Thermal Vacuum

Acoustics Spin Balance

Storage

Dry Weigh & Pressurize Ready for Fuel

THEMIS MRR I&T − 6 GSFC, January 5, 2007

Carrier Processing

Vibration Acoustics Spin Balance

Storage

PC Unload

SSS Installation

Ready for Probes

THEMIS MRR I&T − 7 GSFC, January 5, 2007

Instrument Status

Instrument Status Flight Hardware Ready Flight Software Ready

Recent Activities

Performance Test

Remaining Items ESC Verification

SST/ESA Covers EFI Hats Contamination Samples

Instruments F1 F2 F3 F4 F5IDPU Complete Complete Complete Complete CompleteFSW 4.02 4.02 4.02 4.02 4.02EFI Complete Complete Complete Complete CompleteESA Complete Complete Complete Complete CompleteSST Complete Complete Complete Complete CompleteFGM Complete Complete Complete Complete CompleteSCM Complete Complete Complete Complete CompleteMagBoom Complete Complete Complete Complete CompleteIntegration Complete Complete Complete Complete CompleteTest Complete Complete Complete Complete CompleteEMC CompleteTV Complete Complete Complete Complete CompleteMagnetics Complete Complete Complete Complete CompleteESA Recal Complete Complete Complete Complete Complete

IDPU FSW F1 F2 F3 F4 F5Image1 4.02 4.02 4.02 4.02 4.02Image2 4.02 4.02 4.02 4.02 4.02Image3 4.02 4.02 4.02 4.02 4.02Image4 4.02 4.02 4.02 4.02 4.02ETC 5.A 5.B 5.C 5.D 5.EF5.BEB B0-c B0-c B0-c B0-c B0-cF6.BEB B1-c B1-c B1-c B1-c B1-cF7.BEB B2-c B2-c B2-c B2-c B2-cF8.BEB B3-c B3-c B3-c B3-c B3-cF9.DFB D1 D1 D1 D1 D1FA.DAP 12 12 12 12 12

THEMIS MRR I&T − 8 GSFC, January 5, 2007

Probe Status

Probe Status Hardware Complete Software Complete

Recent Activities at ASO Performance Tests Solar Array Illumination RCS Pressurization to

1.1*MEOP Dry Weigh

Remaining Items Fueling Flight Plugs Integrate to PC Attach Sep System

Probe F1 F2 F3 F4 F5Structures Complete Complete Complete Complete CompleteSep Systems Complete Complete Complete Complete CompleteSolar Arrays Complete Complete Complete Complete CompleteBAU 103 101 105 104 102FSW Image 1 V3.19 V3.19 V3.19 V3.19 V3.19FSW Image 2 V3.19 V3.19 V3.19 V3.19 V3.19RTS Complete Complete Complete Complete CompleteRCS Complete Complete Complete Complete CompleteTransponder Complete Complete Complete Complete CompleteAntenna Complete Complete Complete Complete CompleteBattery Complete Complete Complete Complete CompleteHarness Complete Complete Complete Complete CompleteIRU Complete Complete Complete Complete CompleteAEB Complete Complete Complete Complete CompleteBus CPT Complete Complete Complete Complete CompleteCTV Test CompleteInstrument I&T Complete Complete Complete Complete CompleteProbe CPT Complete Complete Complete Complete CompleteEMC CompleteVibration Complete Complete Complete Complete CompleteTV Complete Complete Complete Complete CompleteMagnetics Complete Complete Complete Complete CompleteSpin Balance Complete Complete Complete Complete CompletePressurize Complete Complete Complete Complete CompleteFuel Empty Empty Empty Empty EmptySafing Plugs NonFlight NonFlight NonFlight NonFlight NonFlight

THEMIS MRR I&T − 9 GSFC, January 5, 2007

Integration Flow

Probe Fueling Probe RCS Electr. Verif.

Weigh Wet Probes, Attach Pyro

PCA Funct.Spin Balance

PCA Comm Check @ Blockhouse

Install Pyro Signal SMDC/ Weigh PCA

Engr Walk-down/ Trans- port Preps

Move Probes to HPF

Weigh PCA

PCA Mate to 3rd Stage/ Clamp-band Instl

Transport to Pad

S/C Functional & RF Test

Launch Rehearsal

Power On & Stray Voltage

Install Fairing

Prop. Load Prep

2nd Stage Fueling, Ordnance

Launch Readiness Review

Laun

ch

Ship

ping

fr

om J

PL12/08/06

12/21/06

02/02/07

02/15/0702/14/07

ASTROTECH and Launch Pad Flow

12/11/06 12/12/06

01/08/07

01/15/07

01/13/0701/05/0712/22/06

12/13/06

02/03/07 02/05/07 02/12/07 02/13/07

PCA Functional

01/23/0701/22/07

12/23/06 01/02/07

Reserve

Christmas Shutdown

12/11/06to

12/18/06

12/19/06

12/15/06

12/11/06

THEMIS Launch

01/03/07

02/07/0702/06/07

12/15/0612/14/06 12/19/0612/15/06 12/20/0612/19/06

5 Probes plus EGSE, MGSE at ASO

Probe Carrier Unpack

Unpack, Setup EGSE

PC-VCO Electrical Test

Install Sep. Harness

Install SMDC Lines

F1 RCS MEOP, LPT, S/A Test

Install Bolt Cutters, Therm. Closeouts

F2-3 RCS MEOP, LPT, S/A Test

F4-5 RCS MEOP, LPT, S/A Test

Weigh, Move to Stands

Pre-VosMRR (GSFC)

01/0301/05

LVRR (KSC) 01/12Media Day 01/12

01/09/07 01/10/07 01/11/07 01/12/07

MRR (HQ) 01/23

01/24/07 01/25/07 01/26/07 01/27/07 01/29/07 01/30/07

LSRR (CCAFS) 02/01

01/3107 02/01/07

02/09/0702/08/07

LMCM (KSC) 02/13FRR (KSC) 02/12

THEMIS MRR I&T − 10 GSFC, January 5, 2007

RFAs

Issue SubmittedRCS Proof Tests Jan 17 2006BAU EEPROM Signal Plots Jun 23 2006Energy Balance in Deep Eclipse Jun 26 2006Launch Window Analysis Nov 09 2006

RFA StatusIncomplete: 0Complete: 308 Closed: 304Total: 308

Final Four Closure Method• RCS Proof Issue: Expected to Close with Risk Definition• BAU EEPROM Plots Provided were Insufficient to the reviewer

but it is no longer practical to obtain better plots.• Energy Balance was Provided using Best Thermal Model at the

time. Reviewer repeated request using new mission profile and correlated thermal model. This was delivered in December.

• Launch Window Analysis will be reviewed by GSFC by 1/15/07

THEMIS MRR I&T − 11 GSFC, January 5, 2007

Reviews Ahead

Start Event Description1/5/2007 MRR Mission Readiness Review

1/12/2007 LVRR Launch Vehicle Readiness Review1/17/2007 SMSR Systems and Safety Mission Assurance1/23/2007 MRB Mission Readiness Review2/1/2007 LSRR Launch Site Readiness Review

2/12/2007 FRR Flight Readiness Review 2/13/2007 LRR Launch Readiness Review