1 / 11

Integration and Test

Integration and Test. 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

kalli
Download Presentation

Integration and Test

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Integration and Test

  2. 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

  3. Environments Magnetics Vibration Acoustics EMC Thermal Vacuum Spin Balance

  4. Probe Processing Delivery to ASO Bolt Cutter Installation Solar Array Illumination Performance Tests

  5. Probe Fueling Preps Vibration Acoustics Spin Balance Dry Weigh & Pressurize Ready for Fuel FM2/FM3 Thermal Vacuum Thermal Vacuum Storage

  6. Carrier Processing PC Unload Vibration Acoustics Spin Balance Ready for Probes Storage SSS Installation

  7. 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

  8. 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

  9. Integration Flow ASTROTECH and Launch Pad Flow THEMIS Launch 12/08/06 to Shipping from JPL 12/11/06 12/13/06 12/19/06 12/20/06 12/12/06 12/11/06 12/14/06 12/15/06 12/15/06 12/19/06 12/21/06 Install Bolt Cutters, Therm. Closeouts F4-5 RCS MEOP, LPT, S/A Test F2-3 RCS MEOP, LPT, S/A Test 5 Probes plus EGSE, MGSE at ASO F1 RCS MEOP, LPT, S/A Test Unpack, Setup EGSE Move Probes to HPF 12/11/06 Probe Carrier Unpack 12/15/06 PC-VCO Electrical Test 01/13/07 01/09/07 01/11/07 12/22/06 01/08/07 01/10/07 01/12/07 12/23/06 01/03/07 01/05/07 01/02/07 Weigh Wet Probes, Attach Pyro PCA Funct. Spin Balance Christmas Shutdown Probe RCS Electr. Verif. Weigh, Move to Stands Weigh PCA Probe Fueling 12/18/06 Install Sep. Harness 01/03 01/12 Pre-Vos LVRR (KSC) 01/05 MRR (GSFC) 01/12 Media Day 12/19/06 Install SMDC Lines 01/23/07 01/24/07 01/26/07 01/29/07 01/25/07 01/27/07 01/30/07 01/3107 02/01/07 01/22/07 02/02/07 01/15/07 Install Pyro Signal SMDC/ Weigh PCA PCA Mate to 3rd Stage/ Clamp-band Instl PCA Comm Check @ Blockhouse Engr Walk-down/ Trans- port Preps Transport to Pad PCA Functional Reserve 01/23 02/01 MRR (HQ) LSRR (CCAFS) 02/08/07 02/12/07 02/13/07 02/14/07 02/05/07 02/03/07 02/06/07 02/07/07 02/09/07 02/15/07 2nd Stage Fueling, Ordnance Launch Readiness Review Install Fairing Power On & Stray Voltage Launch Launch Rehearsal Prop. Load Prep S/C Functional & RF Test FRR (KSC) 02/12 02/13 LMCM (KSC)

  10. RFAs • RFA Status • Incomplete: 0 • Complete: 308 • Closed: 304 • Total: 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

  11. Reviews Ahead

More Related