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GRC/OZ Monthly Tag Up – 1 Glenn Research Center Monthly ISS Payload Ops Review ISS Payload Integration, Planning & Operations April 26, 2012
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GRC/OZ Monthly Tag Up – 2 Glenn Research Center The Increments 29-30 Flight Sequence - 42P (Return), 45P, 28S (11/14/2011), 27S ( Return ), 29S (12/21/2011 ), 45P (Return ), 46P, ATV-3, SpX-D, 47P, and 28S (Return) (4/27/2012) ISS Payloads Manifest for Inc. 29-30 Mission Integration and Planning Increments 29-30 – ISS Payloads Planning (Sept. 22, 2011 – April 27, 2012) IPM: IPM: C. Maender/ C. Hopper LIS Rep: Mark Stovall / Cindy Romero / Vlad Shargorodskiy Flights (Launch Dates) (Undock Dates) 45P (10/30/2011) (1/25/2012) 27S (6/7/2011) (11/22/2011) 46P (1/26/2012) (4/19/2012) SpaceX – D (5/7/2012) (TBD) Payload AscentCIR - FOMA Calibration Unit MDCA/FLEX-2 - Radiometer PACE - LED Kit (LED Base, Power/Data Cable, FIR Power Cable) DescentFCF - Fiber Optic Jack Cleaner, SHERE-II Science Data Tapes (To be returned on SpX-D - CEF #3304) PACE - Pipette Assemblies FCF - Lint-Free Wipes MDCA - Fuel Reservoir (FR) - FR Connector Cover/Protective Cap - Needle 1 & 2 Holders CIR - Manifold #2 Bottle 2.25L - Bottle Valve Cover - Absorber Cartridge SHERE-II - Rheometer - Interface Box - Tool Box - Fluid Modules Stowage Tray - Fluid Modules (25) - Cables & Keyboard - Science Data Tapes
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GRC/OZ Monthly Tag Up – 3 Glenn Research Center CEF CEF # 2665 – Updated FCF Hardware on flights 45P, SpX-D3, SpX-1, ATV-3 and crew time in the Inc. 29/30 PTP CEF # 2665 – Updated FCF Hardware on flights 45P, SpX-D3, SpX-1, ATV-3 and crew time in the Inc. 29/30 PTP CEF # 3155 – FCF Trash PACE-2 consumable items on 42P CEF # 2737 – Change crew time required for MDCA/FLEX-2 from 16 hrs to 26.55 hrs to accomplish the revised science matrix CEF # 2781 - Update CFE-2 crew time requirements in Inc. 29-30. (from 46.8 hrs to 61.5 hrs to complet CFE-2 science objectives) CEF # 3063 – Request the descent of MSG digital tapes contain science data for SHERE-II experiment on flight 27S and SHERE-II fluid modules (26) on flight SpX-1 CEF # 3062 – Update BCAT activity times in Inc. 29/30 CEF# 3092 - Add one CIR gas bottle ready for return and delete LMM-Bio Tissue kit from the SpX-D return manifest CEF# 3119 – SHERE hardware returned on SPX-D and the acceleration of SHERE fluid modules from SPX-1 to SPX-D CEF# 3194 - Trash FCF Items on 45P (PACE Oil Dispenser, FCF Lint Free Wipes) CEF # 3200 – Additional SHERE Hardware on SpaceX Demo Descent (camera arm/cover/cable, keyboard and cable, power/video/data/motor cables. These items will be upgraded for use in SHERE-III) CEF # 3201 - Update FCF Return manifest on Space X Demo CEF # 3276 - Trash FCF Consumable items ( PACE-Oil Dispensers, FCF Lint Free Wipes (10)) – on 46P Status; Approved Status: Approved Mission Integration and Planning Increments 29-30 – ISS Payload Planning (Cont’d) IPM: IPM: C. Maender/ C. Hopper LIS Rep: Mark Stovall / Cindy Romero / Vlad Shargorodskiy
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GRC/OZ Monthly Tag Up – 4 Glenn Research Center CEF CEF# 3306 - Trash the MDCA Radiometer which was recently replaced by the crew with the newer and improved MDCA Radiometer II. The MDCA Radiometer (P/N 67235MFAC13900) has a mass of 1.07 kg and dimensions of 12.4 x 8.2 x 8 cm. CEF # 3155 - Trash several consumable items used during the PACE-2 investigation consisting of: 2 X PACE Oil Dispenser (P/N S1051MFA0009, S/N 2013 + 2007) 2 X FCF Lint Free Wipes (P/N ST-1, S/N NA) (The FCF Lint Free Wipes are disposed of within the bags containing the PACE Oil Dispensers) - on flight 42P CEF # 3220 - Trash fiber optic jack cleaner, P/N6366 on 45P CEF # 3304 – Return of two MSG tapes for SHERE on SpaceX-D (Two science tapes that could not be packed for the 27S Soyuz back in November. The tapes are the Disk Alignment + Camera Scale Tests (DIMSG344M) and Satoshi's Dry Run (DIMSG337M)) CEF# 3360 - Correct FCF H/W Return on SpaceX Demo Descent ( This CEF corrects the return quantity of a specific CIR Gas Bottle which was mistakenly manifested for return twice.) Status: Approved Status: Approved Mission Integration and Planning Increments 29-30 – ISS Payload Planning (Cont’d) IPM: IPM: C. Maender/ C. Hopper LIS Rep: Mark Stovall / Cindy Romero / Vlad Shargorodskiy
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GRC/OZ Monthly Tag Up – 5 Glenn Research Center Mission Integration and Planning Flight 47 Progress was launched on 4/20/2012 and successfully docked to the ISS on 4/22/2012. The Flight 28 Soyuz is scheduled to undocked on 4/27/2012. Space-X Demo (SpX-D) launch date has been changed from April 30, 2012 to May 7, 2012. The SHERE, CIR and MDCA hardware items will be returned on SpX-D. There is no open work for the hardware returning on SpX-D. Participated in the OZ and OB CoFR Reviews for flights 46P, 47P, and SpaceX-Demo. The CoFR endorsement packages for flight SpX-D have been submitted to the HQ, JSC/Payload Office, and MSFC/MSG Office. IPM: IPM: C. Maender/ C. Hopper LIS Rep: Mark Stovall / Cindy Romero / Vlad Shargorodskiy Increments 29-30 – ISS Payload Planning (Cont’d)
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GRC/OZ Monthly Tag Up – 6 Glenn Research Center MSG Utilization Schedule
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GRC/OZ Monthly Tag Up – 7 Glenn Research Center MSG Utilization Schedule
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GRC/OZ Monthly Tag Up – 8 Glenn Research Center ISS Physical Sciences Research Traffic Model Revision date: 03/29/12
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GRC/OZ Monthly Tag Up – 9 Glenn Research Center Mission Integration and Planning Increments 31-32 – GRC Payload Planning (April 30, 2012 – September 17, 2012) IPM: IPM: B. Rhone/ D. McConnell LIS: John Love LIS Rep: Parneet Kaur / Andrew Tucker / Jason Levy Flights (Launch Dates) (Undock Dates) HTV-3 (7/21/2012) Space X-1 (8/18/2012) (9/20/2012) Payloa d AscentACE-1A - Samples LMM - 2.5X Lens CIR - Chamber Windows Coated (2) - Manifold #2 Bottle 2.25 L MDCA-FLEX-1 - Needle Holders 1 & 2 (4) - Needle Covers (4) - Fuel Reservoirs (4 ) BCAT - Adaptor CIR – FLEX-2 * - Windows Coated (2) - IAM F/O Cables #1 (2) * - Manifold #1 Bottle 2.25L (3) * - Bottle Valve Cover (4) - Manifold #3 Bottle 3.80 L * - Package Connector Covers (2) - LCTF DCM –s/n 2011 * ( Liquid Crystal Tunable Filter Diagnostic Control Module) CFE-2 - Vessels (2) DescentCCF- Data Disc/Tape s BASS - Data Disc/Tapes (52) SPICE – Camera Assembly SLIC - Gas Bottles - Data Disc/Tapes (26) BASS - Samples CIR - Gas Bottles The Increments 31-32 Flight Sequence – OrbD1 (Orbital Demo 1), 30S, HTV-3, 29S (Return), 31S, 48P, SpX-1, and 30S (Return) ISS Payloads Manifested for Inc. 31-32
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GRC/OZ Monthly Tag Up – 10 Glenn Research Center Mission Integration and Planning Increments 31-32 – GRC Payload Planning (Cont’d) IPM: IPM: B. Rhone/ D. McConnell LIS Rep: Parneet Kaur / Andrew Tucker / Jason Levy CEF CEF # 2770 – Update crew time for BASS ops (65 hrs), use of 15 Liters of Nitrogen, and other general updates in the Inc. 31-32 PTP. CEF # 3105 - Add CEF-2 Vessels to SpX-1 and SpX-2 manifests CEF # 2770 – Update crew time for BASS ops (65 hrs), use of 15 Liters of Nitrogen, and other general updates in the Inc. 31-32 PTP. CEF # 3105 - Add CEF-2 Vessels to SpX-1 and SpX-2 manifests CEF # 3197 – Add FCF supply to HTV-3 to support FLEX-2 experiment CEF # 3212 - Add ACE-1 to HTV-3 as late load (L-80hr) CEF # 3228 – Delete CVB investigation from Inc. 31/32 Status: Approved Status: Approved Status: Approved Status: Approved Status: Approved
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GRC/OZ Monthly Tag Up – 11 Glenn Research Center Mission Integration and Planning Increments 31-32 – GRC Payload Planning (Cont’d) IPM: IPM: B. Rhone/ D. McConnell LIS Rep: Parneet Kaur / Andrew Tucker / Jason Levy CEF CEF # 3222 – SLICE removal from Inc 31/32 CEF # 3216 – Update GRC Inc 31/32 PTP CEF # 3145 -Delete BXF from Increment 31-32 IDRD. BXF was returned on ULF7 and no longer on ISS. CEF# 3194 - Add FCF Resupply to HTV-3 flight CEF # 3306 - This CEF is to trash the MDCA Radiometer which was recently replaced by the crew with the newer and improved MDCA Radiometer II. The MDCA Radiometer (P/N 67235MFAC13900) has a mass of 1.07 kg and dimensions of 12.4 x 8.2 x 8 cm. The MDCA Radiometer is no longer needed on orbit and is not required for return. CEF# 3307 - Correct the HTV3 manifest and update SpaceX-1 upmass request ( Deletes one FCF H/W Item from HTV3, corrects the mass for two hardware items, and corrects a part name and part number for another H/W Item. Due to the correction of the two mass numbers total FCF Resupply on HTV3 goes up 1.2 kg. Additionally this CEF adds additional H/W to SpaceX-1. This additional hardware adds 28.8 kg to the FCF Resupply previously shown in the PTP) CEF# 3361- Reduce the FCF Launch Manifest aboard HTV3 ( One pair of MDCA Needles will not be able to make the HTV3 flight having failed a critical flow test and verification. The MDCA Needles are used to deliver liquid fuel within the CIR for combustion experiments) CEF # 3362 - Add BCAT Adaptor to HTV3 ( This CEF adds a new component to support the BCAT series of experiments. In October 2011, Mike Fossum created a new setup when installing the BCAT-6 sample module. The new set up provided BCAT with several efficiencies and benefits, however also introduced an unanticipated and undesirable sway of the module resulting in less than perfect imaging over long term sessions. To avoid this, BCAT requires almost daily crew intervention to re-align the set up. (tweaking both camera and sample positions) This new component would eliminate the sway and thereby result in more stable images and result in less crew intervention as well as improve the quality of the images and thereby improving obtained science data. ) Status: Approved Status: Approved Status: Approved Status: Approved
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GRC/OZ Monthly Tag Up – 12 Glenn Research Center Mission Integration and Planning Increments 31-32 – GRC Payload Planning (Cont’d) IPM: IPM: B. Rhone/ D. McConnell LIS Rep: Parneet Kaur / Andrew Tucker / Jason Levy CEF CEF # 3400 - Correct FCF HTV3 Manifest to include a Part 3 Item (Add needle covers to MDCA Needles) This CEF is to correct the HTV3 manifest for FCF Hardware. A Part 3 item was missed as part of the original manifest. This correction has NO impacts to mass, volume, PTP, operations, verifications, safety or otherwise. CEF # 3412 - Additional SPICE & BASS hardware return on SPX-1 (the return of the SPICE Camera and 41 additional tapes for the BASS experiment to return on SPX-1. This accounts for 52 total digital tapes for BASS and 26 tapes for SLICE. ) CEF # 3416 - Correct MDCA Needle Holder 2 Dimension -This CEF Corrects a Typo in the MR Loader for the MDCA Needle Holder 2 (P/N 67235MFAL21001) The CORRECT Dimensions are 17.20 x 6.40 x 7.50 CM Status: Approved The final On-Orbit Operations Summary (OOS) was released on April 10, 2012. Due to I-30 rollover, planned trouble-shooting, and shortend Increment duration, Increment 31/32 crew time is completely FULL. Some prime requirements in Stage 32-6 were moved below the line based on science priority because of the limited allocation available for Utilization in this Stage. Any new requirements which adds crew time cannot be accommodated unless it is replaced with high priority science.
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GRC/OZ Monthly Tag Up – 13 Glenn Research Center The Increments 33 - 34 Flight Sequence – Orb1 (Orbital 1), 32S, 49P, 33S, SpX-2, 50P, 51P, ATV-4, and 32S (Return) ISS Payloads Manifest for Inc. 33-34 Mission Integration and Planning Increments 33-34 – ISS Payload Planning (Sept. 17, 2012 – Mar. 19, 2013) IPM: IPM: Anita Weaver LIS: Steven Huning LIS Rep: Cindy Romero / Gina Calderon / Chris Loyd Flights (Launch Dates) SpaceX-2 (12/15/2012) (1/16/2013) ATV-4 (2/28/2013) PayloadAscentACE-1A - Samples CFE-2 - Vessels (5) (CEF # 3105) CSLM-3 - SPU (6) ICE - GA (Italian Combustion Experiment for Green Air) FCF Resupply & Consumables DescentInSPACE-3 - Data Disc/Tape s CSLM-3 - SPU (6) FCF - Consumables items (Returned for refurbishment)
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GRC/OZ Monthly Tag Up – 14 Glenn Research Center Mission Integration and Planning CEF CEF # 3291 – Request to re-run of both Experiment Units (EU) of the CCF experiment in Increment 33/34 utilizing 6.5 hrs of crew time CEF# 3356 - Request for additional crew time for InSPACE-3 activities in Inc 33/34 and add SSE info to PTP ( Two new InSPACE activities need a total of 10 hours prior to InSPACE Ops. Also add SSE required for both Inc 31/32 (reserve) & 33/34 PTP InSPACE reqires two cameras (MSG supplied cameras) to be replaced on their hardware. This activity is outside the MSG work volume and would require the MWA. The other activity is a InSPACE Vial (sample) Inspection, which mixes and inspects all six new vials prior to operations ) CEF # 3413 – Update the downlink rate for ACE-1 from 38.9 to 22.2 per TCM comment. CEF # 3420 - Request the launch, operation, and return of CSLM-3 on SPX-2 ( Request 6 CSLM-3 Sample Processing Units (SPUs) with a mass of 39.0 kg and a total volume of 0.0819 to launch on SPX-2, operate during SPX-2 docking with 20 hours of crew time and the return of all 6 SPUs on SPX-2 descent) Status: Approved Status: Approved Status: Open Increments 33-34 – ISS Payload Planning (Cont’d) IPM: IPM: Anita Weaver LIS: Steven Huning LIS Rep: Cindy Romero / Gina Calderon / Chris Loyd SPX-2: The amount of late load cargo from L-24 hours to L-12 hours is limited to one powered double locker and three Cargo Transfer Bags (CTB). The SPX-2 cargo currently exceeds this limitation. The Increment 33-34 Science Symposium is planned for June 20-21, 2012. The DECLIC HTI-R, will be presented on June 21, 2012.
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GRC/OZ Monthly Tag Up – 15 Glenn Research Center The Increments 35 - 36 Flight Sequence – 34S, Orb-2 (Orbital 2), 51P, 52P, 35S, HTV-4, 3R, SpX-3, 53P, and 34S (Return) ISS Payloads Manifest for Inc. 35-36 Mission Integration and Planning Increments 35 –36 ISS Payload Planning ( Mar. 19, 2013 – Sept. 16, 2013) IPM: IPM: TBD LIS: TBD LIS Rep: Gina Calderon / Brian Dolan / Jason Levy Flights ( Launch Dates) (Undock Dates) Orb-2 (4/8/2013) HTV-4 (6/10/2013) Space X -3 (7/1/2013) (7/31/2013) Payloads Ascent CIR/FIR - Resupply CIR/FIR - Resupply ACE-1B - Samples CIR/FIR - Resupply DescentCIR/FIR - Consumables The Increment 35-36 Research Plan (IRP) was presented to the Multilateral Payloads Control Board (MPCB) on April 19, 2012. The IRP has been approved.
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GRC/OZ Monthly Tag Up – 16 Glenn Research Center 2 Inc 37/38 (O. Kotov - RS) Inc 37/38 (S. Ryazansky – RS) Inc 36/37 (K. Nyberg - USOS) Inc 36/37 (M. Suraev - RS) Inc 35/36 Expeditions 35 & 36 crews Inc 39/40 Expeditions 39 & 40 crews Inc 38/39 (R. Mastracchio – USOS) Inc 38/39 (M. Tyurin– RS) Inc 38/39 (K. Wakata – USOS) Inc 37 Inc 38 Inc 36/37 ( L.Parmitano– USOS) Inc 37/38 (M. Hopkins – USOS) 2013 36S Sep 30 37S Nov29 35S Rtn 36S Rtn Mar 17 Nov 15 34S Rtn Sep 16 ATV-5 Feb 28 54P Oct 23 55P Feb 16 SpX-4 Oct 7 Increments 37 & 38 Flight Sequence OZ4/Rod Lofton – 4/2012 SpX-4 Rtn Nov 8 Orb-3 RS-Node Feb 1 Dec 5 2014
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GRC/OZ Monthly Tag Up – 17 Glenn Research Center Increments 37 & 38 RP Requirements Definition Planning Schedule Sep 19 MPCB RP presentation Sep 5/6 (TBD) MRPWG/MIT PTP document approval telecons RP inputs Freeze for Feasibility Assessment (FA) Development Jul 13 Increment Research Plan (IRP) Spreadsheet available for review Jun 25 RPWG review of experiments/payloads start (3-pagers and PTP data input) - Reviews at RPWG telecons (NASA-only and bi-laterals) Jun 18 May 21 Payload Candidate Lists Due; RPWG initial review of Increments 37 & 38 proposed payload list to begin Apr 23 √ Call for inputs; formal requested data submittal package released Apr 9/11, 2012 Kick-off Presentation (includes allocations to International Partners) Jul 9 Aug 31 IRP Presentation review @ RPWG and MRPWG Jul 30 (TBC) Feasibility Assessment (including Conditioned Stowage) presentation to RPWG BDC strategy approach presentation @ IRT IRP available for approval TBD Aug 13/15 Sep 12 IRP Presentation to PCB - 3-Pager info, PTP Workbook Tables, Investigation Summary Forms - Research Planning Teams review of Investigation Summary Overview page to occur during this period Data input accepted through (Research Planning Teams review of Investigation Jul 30 NASA Investigation Priority List Available Final RP inputs due for IRP developmentAug 3 19 OZ4/Rod Lofton – 4/2012
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National Aeronautics and Space Administration www.nasa.gov Binary Colloidal Alloy Test-6 (BCAT-6) Ops Complete (to date) Ops Planned (next month) Ops Planned (to completion) Harvard 3 and 4P & G samples 1 and 2, Harvard 5 NYU 6 and 7 STATUS Completed Harvard samples 3 and 4 Great initial results wit NYU samples 6 and 7 (seeded crystal growth) Data form samples 1,2,3,4,5,6 an 7 under review UPENN temperature samples 8,9 and 10 on hold ISSUES UPENN samples need some temperature variation. Present JEM thermal control does not support samples. Working to return BCAT-5 on SpX-2 18
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National Aeronautics and Space Administration www.nasa.gov Binary Colloidal Alloy Test-6 (BCAT-6) Ops Complete (to date) Ops Planned (next month) Ops Planned (to completion) Harvard 3 and 4P & G samples 1 and 2, Harvard 5 NYU 6 and 7 STATUS Completed Harvard samples 3 and 4 Great initial results wit NYU samples 6 and 7 (seeded crystal growth) Data form samples 1,2,3,4,5,6 an 7 under review UPENN temperature samples 8,9 and 10 on hold ISSUES UPENN samples need some temperature variation. Present JEM thermal control does not support samples. Working to return BCAT-5 on SpX-2 19
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National Aeronautics and Space Administration www.nasa.gov BASS On-Orbit Operations Status Ops Complete (to date) Ops Planned (next months) Ops Planned (to completion) 2 cm PMMA sphere 1/7 1 cm PMMA sphere 1/3 2 cm SIBAL flat 2/9 NOMEX blend 1/2 ULTEM sample 0/2 PMMA flat sample 0/4 Started ops 3-30-12 Next scheduled ops 5/22/12 Highlight BASS operated on Apr 9, 2012, by Don Pettit. The BASS 1 cm PMMA sphere was ignited 3 times with different air flow conditions for test points 43, 44, and 45. BASS operated on Apr 5, 2012, by Don Pettit. The BASS SIBAL (50% cotton, 50% fiberglass) sample was ignited and burned per the BASS test matrix. Don also ignited and burned a NOMEX sample. BASS operated on Mar 30, 2012 by Don Pettit. The BASS SIBAL sample was ignited and burned. The 2 cm PMMA sphere was ignited and burned for one minute, and the 1 cm PMMA sphere was ignited and burned for 1 minute. BASS was set up in the MSG on Mar 26, 2012 by Don Pettit. The BASS hardware was installed, the soot clean up procedure, fan calibration procedures were run.
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National Aeronautics and Space Administration www.nasa.gov CFE-2 On-Orbit Operations Status Ops Complete (to date) Ops Planned (next months) Ops Planned (to completion) ICF1 – 16/16 tests ICF2 – 14/16 tests VG1 – 90/60 tests VG2 – 40/60 tests Complete Increment 31/32 30 additional test points Increment 31/32 Next scheduled operations 5/22/12 Highlight Dan Burbank operated Interior Corner Flow 1 (ICF-1) on March 6, 2012. This series of tests used ICF-1 to isolate a bubble in the transport tube and study the compression of the bubble. Dan Burbank operated Vane Gap-2 (VG-2) on March 5, 2012. This series of test was locate the wetted critical angle for the for VG-2 vessel in the Quadrant 2. Dan Burbank operated Vane Gap 2 (VG-2) on March 1, 2012. This series of test was with VG-2 and open perforations in Quadrant 1. The 10 test points were per the test matrix for Vane Gap 2.
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National Aeronautics and Space Administration www.nasa.gov FLEX-2 On-Orbit Operations Status Ops Complete (to date) Ops Planned (next month) Ops Planned (to completion) 25~ 8-12~ 400 April Highlight –Diagnostic Control Module (DCM-1) was removed and replaced on April 10, 2012 –Operations resumed April 12-13, 2012. There were no signs of DCM communication problems. This issue seems to be resolved. It appears the propylbenzene is does not ignite as easily as previous fuels. Soot production from propylbenzene combustion is significant but has not impeded imaging or data acquisition. –A Project Control Board was held April 17; a change of flight the iso-octane flight fuel to toluene was approved –A briefing was given to Tom Hartline, GRC Director of Engineering, et al, regarding the shipment and launch of n-octane rather than iso-octane to ISS Lessons Learned and process mitigations were briefed –The FLEX-2 team continues to obtain Surrogate Fuel test points using 100% propylbenzene (pure) and 50% n-decane/50% propylbenzene (50/50 mixture). –Twenty-five test points have been achieved to date. The PI team is very pleased with the quality of the droplet deployments and combustion data. Issues –Two months of operations lost due to boot up failure and IPSU Stack Anomaly (DCM failure)
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