1. MOL The Mission Operations Laboratory MOL The Mission Operations Laboratory NASA MSFC Engineering Directorate Huntsville, Alabama Training Strategy Team IntraVenous fluids GENeration and mixing (IVGEN) March 4, 2008 Carol Reynolds EO20 256-961-0205 carol.reynolds@nasa.gov

2. MOL The Mission Operations Laboratory Page 2 NASA MSFC Engineering Directorate Huntsville, Alabama Objective The TST is a structured planning and decision-making group who determine the payload training requirements for each payload or complement of payloads or experiments. Payload training requirements, and what will be needed to fulfill those requirements for crewmembers, are discussed, defined, and agreed upon during this process.

3. MOL The Mission Operations Laboratory Page 3 NASA MSFC Engineering Directorate Huntsville, Alabama Agenda  Crew Training Template  TST Products  Payload Hardware and Operations Description  Crew Training Curriculum and Hours  Proposed Payload Training Hardware (PD-Provided)  Proposed Payload Training Support Hardware (NASA-Provided)  On-Board Training Requirements  Payload Instructor Certification  Payload Training Data Set  Schedule

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 * * Based on ULF3 launch date of September 09

5. MOL The Mission Operations Laboratory Page 5 NASA MSFC Engineering Directorate Huntsville, Alabama Crew Training Template From Payload Training and Implementation Plan (PTIP), June 2006

6. MOL The Mission Operations Laboratory Page 6 NASA MSFC Engineering Directorate Huntsville, Alabama TST Products  Training Objectives  Training Curriculum  Training Time  Trainer Type and Fidelity  Training Tools and Development Schedule  Instructor Selection and Certification  Overall Schedule (Level 4)

7. MOL The Mission Operations Laboratory Page 7 NASA MSFC Engineering Directorate Huntsville, Alabama Other Training Products  Lesson Plans (PL Instructor)  Courseware (PL Instructor)  Completion of Training Tool Development  Procedures & agreement on how they are validated  Displays  Usability Test/Trial  Training Equipment  PL Simulator Test Procedures  Training Data Set ECRs to NPOCB

8. MOL The Mission Operations Laboratory Page 8 NASA MSFC Engineering Directorate Huntsville, Alabama IVGEN Overview  With NASA’s desire to return to the Moon and to extend manned exploration missions to Mars, there is an increased likelihood of a mishap and/or medical emergency. With a focus on minimizing up-mass for exploration missions, it is desirable to have a system onboard that will produce intravenous (IV) solutions as needed rather than flying large quantities of pre-made IV solutions that have a limited shelf life.  IVGEN’s objective is to design a compact water purification system to reliably produce Sterile Water for Injection (SWI) and provide a pharmaceutical mixing capability in a reduced gravity environment with minimal dependency on spacecraft power resources.  A prototype of IVGEN is to be tested on ISS in 2010.

9. MOL The Mission Operations Laboratory Page 9 NASA MSFC Engineering Directorate Huntsville, Alabama IVGEN Breadboard Concept Bubble Removal Membranes Rolling PTFE diaphragm accumulator pump Gas side Water side Accumulator Assembly Purification Assembly with Diagnostics Collection Bag with Mixing Apparatus (not shown) Liquid flow meter Deionization Module Pressure Transducers Conductivity Sensors IVGEN Hardware Description

10. MOL The Mission Operations Laboratory Page 10 NASA MSFC Engineering Directorate Huntsville, Alabama Simplified IVGEN on-orbit operations  Hardware Setup Accumulator Fill Experiment Initiation Experiment Shutdown Hardware Stow Hardware Setup Crew installs IVGEN hardware in MSG. Experiment Initiation IVGEN system is started and MSG nitrogen slowly pushes water (1 Liter per hour) through purification system into a water collection bag (IV bag). Mixing apparatus is activated to mix sodium chloride crystals with purified water resulting in normal saline solution. Accumulator Fill Crew disconnects and removes accumulator from MSG and transports to either the Water Processing Assembly (if available), or to a Contingency Water Container (CWC). Crew fills liquid side of accumulator with drinking quality water from one of the two locations above. Crew re-installs accumulator in MSG and connects MSG nitrogen to gas side of accumulator Run 1-5 Run 6 Experiment Shutdown Crew member squeezes filled IV bag to transfer contents through a tube into an empty IV bag. During this process, a conductivity sensor verifies uniform mixing has taken place. Crew transports filled IV bags to refrigerated location for stowage Repeat process for desired number of samples Hardware Stow Crew removes IVGEN hardware from MSG.

11. MOL The Mission Operations Laboratory Page 11 NASA MSFC Engineering Directorate Huntsville, Alabama Proposed Crew Training Curriculum and Hours  Prerequisite  MSG Facility Overview  MSG Video Setup  SAMS Overview (possible)  Lesson 1: IVGEN Experiment Overview, 40 minutes, I-8 to I-3  Objectives  Understand the science objectives of the IVGEN experiment (5 minutes)  Describe the IVGEN hardware (15 minutes)  Describe the basic operations of the IVGEN experiment (10 minutes)  Understand payload constraints (5 minutes)  Describe safety hazards and controls (5 minutes)  Training Methodology  Columbus Module  Training Tools  Powerpoint presentation handout  Training Hardware

12. MOL The Mission Operations Laboratory Page 12 NASA MSFC Engineering Directorate Huntsville, Alabama Proposed Crew Training Curriculum and Hours  Lesson 2: IVGEN Operations, 2 hours 15 mintues, I-8 to I-3  Objectives  Setup and install IVGEN and SAMS hardware into MSG (45 minutes)  Setup MSG video equipment (15 minutes) (might delete this b/c its taught in MSG class)  Perform nominal operations (1 hour)  Accumulator Fill  Experiment Initiation  Experiment Monitoring  Experiment Shutdown  Understand off-nominal and maintenance ops (periodic leak checks and cleanup) (10 minutes)  Summarize Safety hazards (5 minutes)  Obtain Specialist qualification  Training Methodology  Hands-on training using IVGEN Flight-Like Hardware and the MSG TU  Training Tools  IVGEN hardware♦ MSG TU  iPV- crew procedures♦ MLC –IVGEN displays  MSG video cameras, mounting arm  SAMS hardware♦ Water source (CWC)

13. MOL The Mission Operations Laboratory Page 13 NASA MSFC Engineering Directorate Huntsville, Alabama PTU Proposal – PD Supplied Equipment TrainerFidelityQuantity Accumulator Assembly Functional1 Water Purification Assembly Physical1 Fill Hose Assembly Physical1 Water Collection Assembly Functional1 Mixing Module Functional1 Avionics Assembly Functional or Physical?1

14. MOL The Mission Operations Laboratory Page 14 NASA MSFC Engineering Directorate Huntsville, Alabama PTU Proposal – JSC Supplied Equipment  Payload Training Complex (PTC) (bldg 5)  Columbus Module  Presentation Handout  MSG Rack Simulator  Cameras  recorders  Cables  MLC  SAMS  iPV  Chairs  Rolling cart  Support Utilities  Power  Water

15. MOL The Mission Operations Laboratory Page 15 NASA MSFC Engineering Directorate Huntsville, Alabama On-Board Training  Just-in-Time or Proficiency training that will be required prior to on-board payload operations.  Time for lessons is taken from Payload’s on-board operation allotment and requirements are input into the Planning Data set (URC).  CBTs must meet the template requirements of 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.

16. MOL The Mission Operations Laboratory Page 16 NASA MSFC Engineering Directorate Huntsville, Alabama Payload Instructor Selection and Certification Requirements  Crew Training Instructors  Dan Brown  Kimesha Calaway  Karen Barlow  Payload Instructor(s) and courseware are certified by successfully performing a Payload Training Dry Run for each lesson at I-9.  The Ops Lead and a Crew Representative will certify the instructor.

17. MOL The Mission Operations Laboratory Page 17 NASA MSFC Engineering Directorate Huntsville, Alabama Payload Training Data Set  What is the training data set?  PTU Requirements  Curriculum Requirements  How to access it?  POIF account ( john.jupin@nasa.gov)john.jupin@nasa.gov  url of Training & Crew Ops website https://payloads1.msfc.nasa.gov/station/EO20/Index.asp https://payloads1.msfc.nasa.gov/station/EO20/Index.asp  Need write privileges  Who populates it?  Ops Lead  When and how to baseline?  1 ECR for PTU requirements post-TST  1 ECR for curriculum requirements post-PTDR

18. MOL The Mission Operations Laboratory Page 18 NASA MSFC Engineering Directorate Huntsville, Alabama Training Development Milestones Template Date  Dataset Baseline – Simulator HardwareI-20  Procedure Delivery & Chosen AuthorI-14  Tabletop Procedure ReviewI-12  Procedure Validation I-12  Usability TestI-11  Payload Simulator Test ProcedureI-13  Simulator Pre-Ship TestI-12  Simulator DeliveryI-11  Simulator Post Ship TestI-11  Lesson Plan/Courseware DeliveryI-10  PTDRI-9  Dataset Baseline – Curriculum/HoursI-8  Ready for TrainingI-8

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

20. MOL The Mission Operations Laboratory Page 20 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