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MOL The Mission Operations Laboratory MOL The Mission Operations Laboratory NASA MSFC Engineering Directorate Huntsville, Alabama Training Strategy Team.

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Presentation on theme: "MOL The Mission Operations Laboratory MOL The Mission Operations Laboratory NASA MSFC Engineering Directorate Huntsville, Alabama Training Strategy Team."— Presentation transcript:

1 MOL The Mission Operations Laboratory MOL The Mission Operations Laboratory NASA MSFC Engineering Directorate Huntsville, Alabama Training Strategy Team APEX-Cambium Meeting #1, rev. 1 January 9, 2008 Karen D. Somers EO20 256-544-7351 karen.d.somers@nasa.gov

2 MOL The Mission Operations Laboratory Page 2 NASA MSFC Engineering Directorate Huntsville, Alabama Agenda  Crew Training Template  Training Strategy Team (TST) Products  Payload Operations  Crew Training Curriculum and Hours  Proposed Payload Training Hardware (PD-Provided)  Proposed Payload Training Support Hardware (NASA-Provided)  Payload Instructor Certification  Payload Training Data Set  Schedule

3 MOL The Mission Operations Laboratory Page 3 NASA MSFC Engineering Directorate Huntsville, Alabama Crew Training Template From Payload Training and Implementation Plan (PTIP), June 2006 Continued on next page

4 MOL The Mission Operations Laboratory Page 4 NASA MSFC Engineering Directorate Huntsville, Alabama Crew Training Template From Payload Training and Implementation Plan (PTIP), June 2006

5 MOL The Mission Operations Laboratory Page 5 NASA MSFC Engineering Directorate Huntsville, Alabama Training Strategy Team (TST) Products The purpose of the TST is to define and/or baseline the:  Training Objectives  Training Curriculum  Training Time  Trainer Type and Fidelity  Training Tools and Development Schedule  Instructor Selection and Certification Plan  Overall Schedule (Level 4)

6 MOL The Mission Operations Laboratory Page 6 NASA MSFC Engineering Directorate Huntsville, Alabama Other Training Products The TST also oversees development of:  Lesson Plans (Payload Instructor)  Courseware (Payload Instructor)  Training Tools  Procedures & agreement on how they are validated  Displays  Usability Test/Trial  Training Equipment  Payload Simulator Test Procedures  Baselined Training Data Set (submit ECRs to NPOCB)

7 MOL The Mission Operations Laboratory Page 7 NASA MSFC Engineering Directorate Huntsville, Alabama Payload Operations - Nominal #TitleNotes Estimated Inflight Crew Time Estimated Training Time Training Responsibilities 1Transfer ABRS from Shuttle to ISSABRS Installation & Checkout30 minutes maximumSOC 2TAGES HarvestPerformed 3 times for Runs 1 and 2; once during Run 3 60 minPOIF 3Transfer of samples to MELFIPerformed 3 times for Runs 1 and 2; once during Run 3 15 min (nominally 10 min) 0POIF/Covered in MELFI Training 4Water reservoir refillPerformed once per week30 minPOIF 5Loop Cambium plant stemsPerformed once for each of three runs 45 minPOIF 6Harvest Cambium plant stemsPerformed once after Run 1 and twice during Run 2; in conjunction with TAGES harvest 60 minPOIF 7Air Filter changeoutPerformed once per month30 minPOIF 8Transfer samples to Shuttle for returnBoth live (ambient) and preserved (frozen) 45 min (live stow) + 30 min (transfer) SOC

8 MOL The Mission Operations Laboratory Page 8 NASA MSFC Engineering Directorate Huntsville, Alabama Proposal - Crew Training Curriculum and Hours  ABRS Facility Training 1/1 1 hr, I-10 to I-3 months  Objectives  1. Overview of facility operations (15 min.)  2. Activation/Deactivation of ABRS Facility (10 min.)  3. Air Filter Replacement (10 min.)  4. Experiment Monitoring/Data Download (10 min.)  5. Water Refill (5 min.)  6. Discuss off-nominals and malfunctions (10 min.)  Classroom instruction, hands-on practice  Training Tools: ABRS Facility, ABRS Root Trays (both of the two types should be available), ABRS Syringe Bag (with Refill), ABRS Photogrid, ABRS Air Filter, ABRS Water Sample Kit (includes Waste Water Bag, Water Sample Bag and Water Reservoir), EXPRESS Rack Simulator, ELC running IPV, ELC running payload software/displays.

9 MOL The Mission Operations Laboratory Page 9 NASA MSFC Engineering Directorate Huntsville, Alabama Proposal - Crew Training Curriculum and Hours  APEX-Cambium Operations Training 1/1 2.0 hrs, I-10 to I-3 months  Objectives  1. Overview of operations (30 min.)  2. Cambium Stem Looping (30 min.)  3. Cambium Harvest (30 min.)  4. Cambium Run Replant (10 min.) (same as 6?)  5. TAGES Harvest (10 min.)  6. Off-Nominal: Cambium and TAGES Spares Replant (10 min.)  Classroom instruction, hands-on practice  Training Tools: APEX-Cambium Harvest Kit (incl. Looping Tool), KFT Kit (incl. RNALater KFT, Formaldehyde KFT, KFT Actuator, KFT Actuator Handle), Sample Tube, Petri Plate, ABRS Root Trays (both of the two types should be available), ABRS Photogrid  Support Hardware: Maintenance Work Area (MWA), Digital Still Camera

10 MOL The Mission Operations Laboratory Page 10 NASA MSFC Engineering Directorate Huntsville, Alabama Proposal – PD Supplied Equipment TrainerFidelityQuantity Advanced Biological Research System (ABRS) Functional1 at JSC ABRS Root Tray Functional2 at JSC ABRS Syringe Bag ABRS Refill Syringe Functional1 at JSC ABRS Photogrid Functional1 at JSC ABRS Air Filter Functional1 at JSC ABRS Water Sample Kit ABRS Waste Water Bag ABRS Water Sample Bag ABRS Water Reservoir Functional1 at JSC APEX-Cambium Harvest Kit APEX-Cambium Looping Tool (need a list of other tools in the kit) Functional1 at JSC APEX-Cambium Science Spare Functional? APEX-Cambium KFT Kit APEX-Cambium RNALater KFT APEX-Cambium Formaldehyde KFT APEX-Cambium KFT Actuator APEX-Cambium KFT Actuator Handle Functional1 at JSC APEX-Cambium Sample Tube Functional1 at JSC APEX-Cambium Petri Plate Functional?

11 MOL The Mission Operations Laboratory Page 11 NASA MSFC Engineering Directorate Huntsville, Alabama Proposal – JSC Supplied Equipment Options at JSC:  Payload Training Complex (PTC) - Building 5 (Recommended)  Rack Buildup Area (RBA)/Classroom/U.S. Lab/ Slab  RBA is a locked room dedicated to POIF  EXPRESS Rack Simulator, tables and chairs  Includes power and Ethernet LAN  ABRS could be on table or in EXPRESS Rack  Computer projector and external power supply available  Space Station Mockup Training Facility (SSMTF) – Building 9  High Fidelity Mockup/Node/Etc.  Payload Development Lab (PDL) II – POIF US Lab Mockup  Power, nitrogen, water available  International Procedures Viewer (IPV)  Flight-like use of procedures on an EXPRESS Laptop  Available in all training facilities, but must be requested  APEX-Cambium will use IPV  Tools  Station tools and support equipment available

12 MOL The Mission Operations Laboratory Page 12 NASA MSFC Engineering Directorate Huntsville, Alabama On-Board Training (OBT)  OBT Products can be in the form of crew procedures, video conference with certified instructor, On-board Computer-Based Trainer (OCBT) or other approved training materials.  May be used as a supplement to or in place of ground-based training.  Reasons for OBT: proficiency, optional refresher, just-in-time training due to lack of available hardware or training time prior to launch.  Duration for lessons is taken from Payload’s on-board operation allotment and requirements are input into the Planning Data set (URC).  OCBTs must follow a template required by the On-Board Training Working Group.  All courseware used for training must have been through a payload training dry run and is configuration-controlled by the JSC On-Board Support System (COSS) integration group.

13 MOL The Mission Operations Laboratory Page 13 NASA MSFC Engineering Directorate Huntsville, Alabama On-Board Training Development Process  TST makes the decision to use OBT for a payload.  PD fills out a preliminary OBT Description Form and provides it to the Ops Lead.  Product information incl. type of product, title, version #, file size  Product compliance information  Synopsis of what is in the product  Supporting hardware the product requires  COSS Product Integration services required  Launch and return flights of the product  ~L-12 months: Lesson Concept Meeting between PD and Ops Lead to finalize training objectives, lesson synopses and planned OBT media.  User develops the OBT product and holds iterative evaluations.  Physical media and OCBT (electronic uplink) both require a PTDR (L-4 to 2 months) before final delivery.

14 MOL The Mission Operations Laboratory Page 14 NASA MSFC Engineering Directorate Huntsville, Alabama Payload Instructor Selection and Certification Requirements  Who will be the instructor?  Dave Reed for ABRS Facility and TAGES Science  Melanie Mailloux for Cambium Science  Will there be a backup instructor?  Dave and Melanie will certify as backups for one another.  Are multiple instructors needed?  No, but Subject Matter Experts could be called upon: PIs and April Spinale.  Payload Instructor(s) are certified by successfully performing a Payload Training Dry Run for each lesson.

15 MOL The Mission Operations Laboratory Page 15 NASA MSFC Engineering Directorate Huntsville, Alabama Payload Training Data Set  What is the training data set?  Payload Training Requirements  Curriculum Requirements  How to access it?  PDs Need POIF Account (Ops Lead will provide access info)  PDs Need URL of Training & Crew Ops Web site  Who populates it?  Ops Lead (PD will verify information)  When and how to baseline?  1 ECR for PTU Requirements Post-TST (as soon as we all agree; in schedule on next page, it is the first item, ”Dataset Baseline”)  1 ECR for Curriculum Requirements Post-PTDR* * PDs should plan to attend the Payload Training Dry Run (PTDR) to support as Subject Matter Experts (SMEs)

16 MOL The Mission Operations Laboratory Page 16 NASA MSFC Engineering Directorate Huntsville, Alabama Training Development Milestones Based on implementation after 2J/A:  Dataset Baseline – Identify Training HardwareJanuary 08  Draft Procedure Delivery to Ops LeadFebruary 08  Tabletop Procedure ReviewFebruary 08  Procedure Validation March 08  Usability TestMarch/April 08  Payload Simulator (Training Hardware) Test ProcedureMay/June 08  Simulator Pre-Ship TestMay/June 08  Simulator DeliveryJune 08  Simulator Post Ship TestJune 08  Lesson Plan/Courseware DeliveryJune 08  Payload Training Dry Run (PTDR) July 08  Dataset Baseline – Class Curriculum/Duration July 08  Ready for TrainingJuly 08  Baseline ProceduresAugust 08  Launch of 2J/AMarch 09

17 MOL The Mission Operations Laboratory MOL The Mission Operations Laboratory NASA MSFC Engineering Directorate Huntsville, Alabama Backup Charts

18 MOL The Mission Operations Laboratory Page 18 NASA MSFC Engineering Directorate Huntsville, Alabama Acronyms ABRSAdvanced Biological Research System APEXAdvanced Plant EXperiments on orbit BPSBiomass Production System CDRCritical Design Review CTCCrew Training Coordinator ECREngineering Change Request ERCEnvironmental Research Chamber GUSBeta-Glucuronidase JSCJohnson Space Center IPVInternational Procedures Viewer ISSInternational Space Station IVAIntravehicular Activity KFTKSC Fixation Tube LANLocal Area Network LEDLight Emitting Diode MELFIMinus Eighty Degree Freezer for ISS MITPMission Integrated Training Plan MSFCMarshall Space Flight Center MWAMaintenance Work Area NPOCBNASA Payload Operations Control Board OBTOn Board Training PDPayload Developer PDRPreliminary Design Review PDRTPayload Displays Review Team POIFPayload Operations Integration Function PSAT Post Shipping Assessment Test PTDR Payload Training Dry Run PTCPayload Training Complex PTUPayload Training Utilization RBARack Build-up Area SMESubject Matter Expert SOCShuttle Operations Coordinator TRRTest Readiness Review TSTTraining Strategy Team

19 MOL The Mission Operations Laboratory Page 19 NASA MSFC Engineering Directorate Huntsville, Alabama PTU Classes/Component Fidelities  Component Fidelities  Total Fidelity (T): All functional and physical characteristics representative of the flight design  Functional Fidelity (F): All functional characteristics representative of the flight design; physical characteristics are not represented  Physical Fidelity (P): All physical characteristics representative of flight design; functional characteristics are not required  Envelope Fidelity (E): Mockup with exterior shape and color representative of flight design  Visual Fidelity (V): No operational/functional capabilities; front panels representative of flight design


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