1 International Space Station Program Mission Integration & Operations Increment 19_20 Overview POIWG 22 July 2008 OC/Increment Engineer Karen Alfaro

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 2 The Increment 19 & 20 Team –Benjamin Pawlik – Increment Manager – x47089 –4S/4305D – Blackberry: –Karen Alfaro – Increment Engineer – x47568 –David Bach – Increment Engineer - x46748 –Donald McBride – Increment Engineer – x40927 –Martha Trammell – Schedules – x40204 –Nancy Monsees – IDRD Book Manager – x42336 –Carol Lott – Meeting Coordinator – x46889 NASA Launch Package Managers –Steve Huning – 2J/A - x48043 –Bernestine Dickey – 17A – x47933 –Mike Hoy – Russian Vehicles – x48168 –Quan Le – HTV-1 – x47151 OC/Increment 19&20 Management Team

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 3 Expedition 19 & 20 Crew CDR Gennady Padalka CDR  18S/  18S FE-1 Mike Barratt FE-1  18S/  18S 15A FE-2 Koichi Wakata 15A FE-2 Koichi Wakata  15A/  2J/A 2J/A FE-2 Tim Kopra 2J/A FE-2 Tim Kopra  2J/A/  17A 17A FE-2 Nicole Stott 17A FE-2 Nicole Stott  17A/  19S FE-3 Frank DeWinne FE-3  19S/  19S  19S/  ULF3  19S/  19S FE-5 Roman Romanenko FE-5 FE-4 Bob Thirsk FE-4

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 4 Increment Overview – Increments 19 & 20 Soyuz Relocation Shuttle EVA RS Stage EVA

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 5 Increment 20 Crew of 6 19S Docking (during 2J/A) begins crew of 6 operations and Increment 20 Crew of 6 for Increment 20 (4USOS/2 RS) –Generic plan is to have 3 USOS and 3 RS (Incr 23) –Segmented operations >Activities on RS side completed by RS crewmembers >Activities on USOS side completed by USOS crewmembers Direct and Indirect Crew Rotations –Direct- Soyuz Flights overlap (Space Flight Participants) Not the nominal plan –Indirect- Crewmembers arrive after the previous Soyuz has already left >Will be a period of time with only 3 crew onboard (16 days) IDRD Crew Time Allocations –Calculated using segmented ops concept. Some activities are considered integrated such as medical operations, routine ops, onboard emergency training –With 4 USOS crewmembers there is abundant time during Increment 20 allocated to payloads Training –Not all crews will be trained on all activities –Assuming upmass for payloads is resolved can the payload training template accommodate the increased payload activities?

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 6 Affecting Payloads 6 Crew Hardware Readiness –Operations and performance go/no-go for 6-crew requires 90 days ops Food and Supplies –6-crew supply, reserve, and CSCS capabilities impact other upmass requirements. Review of consumable rates currently in work. Crew Time for Utilization –Preliminary assessment shows under subscription of available crew time for Utilization, with potential for additional time if the HTV launch slips. MPLM Return –Program is assessing impacts of leaving the 17A MPLM berthed to ISS, and replacement with a permanently attached PLM (Permanent Logistics Module) on 19A. Payload upmass will be affected on 19A. RS Utilization –Preliminary assessment very little crew time available for Russian payloads due to crew complement (4:2) and segmented operations Joint RS/USOS Utilization –Potential deferral of Inc 18 RS/USOS IP tasks Utilization Cargo –Cargo priorities and launch delays affect Utilization capabilities, with additional threats Sharing Comm assets for Crew of 6 –6 crew sharing same amount of s/g assets as 3 crew. Will have to coordinate usage Known Issues and Uncertainties

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 7 Other SARJ Operations and Limitations –Repair and maintenance planning, hardware pre-positioning, effects on ISS power management and assembly operations T2 Transfer and Activation –T2 delay to 17A requires interim ISS installation during docked ops, with final installation during stage 17A. Exercise and Scheduling –Delivery of T2 late in Increment 20 results in scheduling constraints and potentially increased maintenance on other exercise hardware Safety –Need to maintain Safety focus and awareness Software Updates –Accelerated software development and deliveries required MRM2 Prep –Work associated with 5R launch and MRM2 docking Known Issues and Uncertainties

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 8 Other (Cont) Russian Stage EVAs –3 EVAs associated with MRM2 arrival prep, and MRM2 configuration to support 20S docking USOS Resources on RS EVA –Potential Partner agreements may be required regarding USOS crewmember on Stage EVAs Crew Quarter and Interim Crew Quarter –Interim sleep area prior to arrival of CQ on 17A 2J/A Deferred EVA Tasks –Lower priority tasks may be deferred COTS Readiness –Testing and readiness to support COTS visiting vehicles (CUCU checkout) HTV Prep –Delivery and checkout of supporting systems for HTV arrival –HTV rendezvous demonstration testing Joint Shuttle/Soyuz Ops –Shuttle and ISS Program assessing capability to perform Soyuz vehicle dockings during Shuttle/ISS operations Known Issues and Uncertainties

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 9 I IDRD Crew Time Allocations (based on GGR&C times) Increment 19 (3 Crew Operations) –Traffic Ops include: 19S and 2J/A joint operations, 32P undock and 33P dock, 18S relocation, New crew fam and departure preps –Nominal GGR&C allocations hrs/week for medical ops, OBT, Payloads, Routine ops, PAO –Maintenance: Historical averages for US/RS (assumed 1/3 of total time) –Assembly: Assumed 1/3 of total Increment allocation during I19 –Approximately 0 hours available Increment 20 (6 Crew Operations: 4 NASA/2 RS) –Total available crew time is split 2/3 for NASA and 1/3 for RS –Integrated Ops times are split 50/50 allocation between NASA and RS and include: Medical ops, routine ops, Emergency OBT –First time to use segmented operations. Allocations are either NASA or RS and include: traffic ops (Shuttle, HTV, Progress, Soyuz), PAO, Maintenance, Assembly (MRM2), EVAs (3 RS EVAs scheduled to prep and outfit MRM2) –A US crewmember is performing 3 RS EVAs (185 hrs). This time will be compensated from RS to NASA but will most likely not be crew time since RS does not have available crew time to trade –Approximately 1000 hours available for NASA payloads –If HTV dock slips to Increment 21, USOS potential additional 166 hrs available for payloads –If the 17A MPLM is left on USOS potential additional 55 hrs available for payloads

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 10 I Utilization Allocations in Baselined IDRD

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 11 I Utilization Crew Time Challenge and Forward Work Increment 20 (6 Crew Operations) –Identify additional Utilization for the crew to perform that does not require significant upmass –OZ currently in the process of identifying requirements to fill the 1000 hrs for Increment 20 –This challenge will likely extend into Increment 21 & 22 –Need to work an integrated plan between OC and OZ to coordinate manifesting the utilization cargo for Increment –Develop a reasonable training template for the A-line and B-line crews (19S and 20S)

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 12 Back Up Information

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 13 Launch Date: May 15, 2009 Vehicle: OV-105 Payload Bay Manifest: –JEM EF, JEM ES –ICC VLD with 6 P6 batteries, PM, LDU, SGANT –DRAGONSAT, ANDE-2 (deployed post undocking) Duration: days EVA’s: 5 +1 Crew Size: 7 up/7 down, 1 crew rotation Cryo Tank sets: 5 GN2 Tanks: 6 2J/A Overview

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 14 Perform 1-person crew rotation Deliver, install and activate JEM-EF to JEM-PM (EVA) Deliver and Install ELM-ES to JEM-EF (EVA) Remove and replace six P6 batteries (EVA) Transfer PM-2, LDU and SGANT to ESP-3 (EVA) Return ICC-VLD (with six P6 batteries) to PLB Install JAXA EF Payloads and ICS to JEM-EF (EVA) Return ELM-ES to PLB 2J/A Major Objectives

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 15 FD1 Launch FD2 SRMS Checkout; Cargo Visual Inspection with SRMS; OBSS Survey; EMU Checkout; EVA Tool Config FD3RPM, Rendezvous w/ Station & dock to PMA2 (on Node 2 forward port); Ingress Station; IELK installation; Middeck transfer FD4EVA 1 – JEM-EF installation, ICC-VLD installation, IEA battery preparation and EF Fwd Camera install FD5 MT Translation, ELM-ES installation FD6 EVA 2 – Battery R&R (4 batteries) FD7 No EVA or EVR activities FD8 EVA 3 – Battery R&R (2 batteries) and ES payload prep FD9 MT Translation, JEM RMS transfers ICS and MAXI and SSRMS puts SPDM down FD10 EVA 4 – Old battery torque operations and ORU transfers, FD11JEM RMS transfers SEDA-AP and SSRMS return ES FD12 EVA 5 – SSRMS return ICC-VLD and EF Aft Camera Install FD13 No EVA or EVR activities FD14 Undock from ISS; Late TPS Inspection FD15 Cabin Stow, Entry Prep FD16 Deorbit Prep, Landing 2J/A Timeline Review

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 16 ISS-17A (STS-128) Overview 17A Manifest: MPLM, LMC (ATA, 1 PFRAMs), 2 SWCs (MISSE-6 FSE) –Mission Parameter >Launch Date – 7/30/2009 >OV Atlantis >Mission Duration Days >Crew 7 / 1 crewmember rotation >2 EVAs (protecting for 3 ) >5 Cryo Tanks FULL >5 Nitrogen Tanks FULL >Ballast Box Only

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 17 One Expedition crewmember will be rotated on 17A (last crew rotation on Shuttle). MPLM w/16 Racks. 6 racks are transferred to ISS. Remaining racks are RSP (qty.6), RSR (qty. 4), and ZSR (qty. 2, attached to RSR) oCrew Quarters Rack oTreadmill-2 rack completes ISS 6-crew habitation requirements oNode 3 Air Revitalization System (N3 ARS) rack oThree International Standard Payload Rack (ISPR) for utilization: - Materials Science Research Rack (MSRR) - Minus Eighty Laboratory Freezer for ISS-2 (MELFI-2) - Fluids Integration Rack (FIR) LMC launch configuration: Direct-Mounted Ammonia Tank Assembly (ATA) and an empty Passive Flight Releasable Mechanism (PFRAM). LMC landing configuration: Empty ATA and European Technology Exposure Facility (EuTEF). If required, a Return On Need (RON) ORU will return on PFRAM instead of EuTEF. 17A Major Tasks/Objectives

OC/B, Pawlik/K. Alfaro 7/22/08 Pg EVAs: Remove/Replace P1 ATA Transfer EuTEF from Columbus Exposed Payload Facility (EPF) to LMC Transfer MISSE 6a and 6b from Columbus EPF to Bay 4 & 5 Port Sidewalls. Remove/Replace S0 Rate Gyro Assembly Middeck Powered Payloads: General Laboratory Active Cryogenic on ISS Experiment Refrigeration (GLACIER) Mice Drawer System (MDS) TriDAR DTO-701A: Evaluation of TriDAR Automated Rendezvous and Docking Sensor during Shuttle docking, while docked and flyaround. Payload of Opportunities: Maui Analysis of Upper Atmosphere Injections (MAUI) Shuttle Exhaust Ion Turbulence Experiment (SEITE) 17A Major Tasks/Objectives

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 19 COTS = Commercial Orbital Transportation System, i.e. new providers of launch services to ISS to fulfill NASA demand post Shuttle retirement Dragon = Spacecraft under development by SpaceX (through Space Act Agreement) to demonstrate capability to rendezvous and attach to ISS CUCU (COTS UHF Communication Unit) = Proximity Communications box for UHF communication between Dragon & ISS CCP = Crew Command Panel for ISS crew to send commands to Dragon Figure Courtesy of SpaceX CUCU Checkout (Post 17A)

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 20 Main Purpose of MRM2 Purpose To provide an additional port for manned and cargo vehicles To perform airlock ops in MRM2 and crewmember spacewalk egress from the egress hatch during EVA (after DC1 stops functioning as a mated element of the ISS RS); To provide workstations for science hardware. Main Specifications Launch mass3670±50 kg Maximum hull diameter2550 mm Hull length along docking assembly planes 4049 mm Gas volume~ 12.5 m 3 Number of egress hatches (open inward) 2 Egress hatch diameter1000 mm

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 21 MRM2 design is based on the docking compartment DC1 (see document “International Space Station. Integrated Russian Segment. Space Hardware. Description of the Docking Compartment (DC1) (Article 240ГК)”). MRM2 differs from the DC1 base article in the following ways: MRM2 docks to the SM zenith port, which requires additional work on the ISS RS to accommodate MRM2; MRM2 provides a payload system designed to integrate science hardware on MRM2; MRM2 provides a docking tracking target for visual monitoring of Soyuz vehicle automatic docking to MRM2; Design changes have been made due to the need to integrate science hardware on MRM2; Instruments that are components of the onboard equipment control system (СУБА) have been upgraded; The way caution and warning alarms on MRM2 are issued has been modified. Modifications stem from upgrading СУБА instruments; MRM2 onboard measurement system has been configured based on the mini data telemetry system (МБИТС); Atmosphere revitalization system hardware has been upgraded due to the need to integrate science hardware on MRM2. MRM2 Basic Information

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 22 ISS RS after MRM2 Integration DC1 МRМ2 SМSМ FGB Soyuz ТМA Progress М Soyuz ТМА Progress М

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 23 MRM2 Interdependencies The following work must be carried out on the ISS RS in preparation for the arrival of MRM2: 1.Install a conical cover on the SM zenith docking assembly during EVA from the SM transfer compartment (ПхО). Connect cables to the conical cover after it is transferred (IVA). 2.Manufacture and deliver to the ISS RS, on Progress no later than April 2009, the docking target unit, Kurs-P antenna units, and external and internal cable inserts to connect the antenna feeder unit to the SM Kurs-P container. 3.EVA to install the docking target unit, and to install and connect the MRM2 Kurs-P antenna units to the SM Kurs- P container. 4.During IVA, install cable inserts connecting the MRM2 Kurs-P antenna units to SM Kurs-P hardware and with the DC1 Kurs-P antenna feeder unit set. 5.Remove and temporarily secure nearby the onboard neutron telescope (БТН-М1) science hardware on the SМ (to prevent the possibility of MRM2 colliding with БТН-М1 during oscillation), restore the БТН-1М configuration after MRM2 docking. 6.Manufacture, deliver, and install (during IVA) SM flight data telemetry system (БИТС 2-12) ROM to receive telemetry from MRM2 systems and cable inserts for receiving telemetry from vehicles docked to MRM2. 7.Manufacture, deliver, and install (during IVA) components of the SM onboard equipment control system (СУБА) (docking system command processing unit (БОК СС and cable inserts) to support EVA from MRM2 and to recharge the storage batteries of transport vehicles docked to MRM2. 8.Before MRM2 arrival, develop and install the SM onboard computer system software version supporting the ISS RS configuration including MRM2.

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 24 RS EVA No. in Flight Program Operation 2Installation of reciprocal measurement equipment on the SM. Adjustments (if necessary). 2323Cone transfer from the SM nadir port to the zenith port. 2424Installation of the Kurs antenna feeder unit (АФУ) and target on МИМ2. Connection of cables to the SM. EVA for МИМ2 Integration

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 25 HTV SUMMARY –JAXA develops, unmanned, performs automated rendezvous to capture box, captures by SSRMS and attaches to Node 2 Nadir CBM –16.5MT vehicle launched on H-IIB from Tanegashima, Japan –ISS re-supply (6MT) >Pressurized cargo (experiment payloads, consumables, potable water, etc,.) >Unpressurized cargo (ORUs, experiment payloads, ISS batteries) … >Departs with solid/ liquid waste –Docked duration- up to 30 days –Controlled destructive re-entry –Major milestones >PQR kick-off in May 2008 >PROX communication equipment launch on 1J/A >First flight in NLT September 2009 –Useful link: H-IIB Launch Vehicle HTV

OC/B, Pawlik/K. Alfaro 7/22/08 Pg. 26 HTV Elements Logistics Carrier - Pressurized Section (Pressurized Cargo) Logistics Carrier - Unpressurized Section (Unpressurized Cargo) Avionics Module Propulsion Module Exposed Pallet (EP) EP Payload (Unpressurized Cargo) Propellant Tank Main Thruster Hatch Forward RCS Thruster Earth Sensor Li-ion Non-rechargeable Battery Avionics Navigation Light Solar Cells Length: 9.2 m Diameter: 4.4 m Weight: 16.5 tons (at launch) Payloads: 6 tons (mix) Rendezvous Target Orbit: Altitude km; Inclination 51.6 deg. HTV Cargo Research Materials (experiment units, samples, etc.) Daily commodities (water, food, clothing) Resupply Items (ORUs, batteries, etc.) HTV Cargo Research Materials (experiment units, samples, etc.) Daily commodities (water, food, clothing) Resupply Items (ORUs, batteries, etc.)