JMU Notice : This technical data is furnished on the condition that it will be used by and disclosed to the receiving Cooperating agency and its contractors and sub contractors only for the purposes of fulfilling the cooperating agency’s responsibilities under the Space Station Intergovernmental Agreement (IGA) and Memorandum of Understanding (MOU). It shall not be used for any other purpose, nor disclosed or retransferred to any other entity or government without prior written permission of the Japan Aerospace Exploration Agency (JAXA). Increment 33 and 34 JAXA Utilization Overview POIWG #31 Jan 24-26, 2012 Takefumi Sakaguchi / JEM PAYLOADS Yuji Abiru / JEM PAYLOADS Tooru Mori / JPOC

JMU Objectives  Provide big picture for the JAXA utilization.  State the overview of each experiments and activities.  State the operational key points.

JMU Increment 33 and 34 JAXA utilization New

JMU Increment 33 and 34 JAXA utilization

JMU Increment 33 and 34 JAXA utilization

JMU Increment 33 and 34 JAXA utilization New

JMU Dynamic Surf / Marangoni UVP Crew activities: Cell installation to FPEF, removal/exchange of specimen cell # of crew: 1 Facility/Interfaces: Ryutai Rack, FPEF, IPU, Ar, Vacuum, MMA, MWA Liquid Bridge will be sensitive to g-disturbances. Will be performed during crew sleeping time and quiet periods of the gravitational environment. The setup/maintenance activities of the experiment cell need MWA. #activities 1Experiment execution(30days) 2VRU-HDD exchange [Crew task] 3Maintenance, Assembly and Installation of Experiment Cell, MMA Setup [Crew task] 4Experiment execution(30days) 5VRU-HDD exchange [Crew task] 6Maintenance, Assembly and Installation of Experiment Cell, MMA Setup [Crew task] Inc 33/34 13 Dynamic Surf Marangoni UVP MIDM: Microscopic Imaging Displacement MeterUVP: Ultrasonic Velocity Profiler

JMU In-situ observation of growth mechanisms of protein crystals and their perfection under microgravity Nano Step Interferometer image Nano Step Cell (mockup) Crew activities: Cell installation to SCOF, removal/exchange of specimen cell Facility/Interfaces: SCOF, IPU, G1, MMA Experiment should be done within a few months. Crystal quality will be sensitive to g-disturbances. Experiments require quiet period concerning gravitational environments. (Avoid docking time period. The critical phase of crystal growth is about 48 hours, so we would like the critical experiment to be scheduled when the g-environment is good.) #activities 1MMA setup 2Nano Step Cell launch lock removal and Nano Step Cell installation to SCOF 35 experiment runs (specimen cell 1) (35 days TBD) 4Remove Nano Step Cell from SCOF, exchange specimen cell, and re-install Nano Step Cell to SCOF 55 experiment runs (specimen cell 2) (35 days TBD) 6Remove Nano Step Cell from SCOF, exchange specimen cell, and re-install Nano Step Cell to SCOF 75 experiment runs (specimen cell 2) (35 days TBD) 8Nano Step Cell removal HTV Inc 33/34Inc31/

JMU Crystal growth mechanisms associated with the macromolecules adsorbed at a growing interface - Microgravity effect for self-oscillatory growth - Ice Crystal 2 Ice Cell 2 (mockup). Phase-contrast (upper) and interference (lower) image. Inc 33/34 Crew activities: Cell installation to SCOF, removal will be done in Inc 33. Facility/Interfaces: SCOF, IPU, MMA Experiment lasts a few months. Crystal quality will be sensitive to g-disturbances. Experiment will be performed at GMT night time frame from ground. (Avoid docking time period or when there is a g-disturbing crew event in KIBO. ) #activities 1Ice Cell 2 installation to SCOF 2100 experiment runs (40 days) 12

JMU High Quality Protein Crystal Growth Experiment JAXA PCG High Quality Protein Crystal Growth Experiment Canister Protein Crystallization Resaerch Facility (PCRF) Crew activities: PCG install, removal # of crew: 1 Facility/Interfaces: PCRF #activities 1Cell setup and Experiment Activation 2Experiment Execution (2-4 months) 3Experiment Deactivation and Stow 12 Inc 33 48P31S 3

JMU Stem Cells Crew activities: MELFI ins. Facility/Interfaces: MELFI (-95 deg. C) After about one month, six months, 12 months, 24 months, 36 months, the case will be retrieved to the ground. #activities 1Transfer from SpX-2 to MELFI, keep frozen (Five Sample Cases and One PADLES) 2Transfer from MELFI to SpX-2, keep frozen (One Sample Case) SpX-2 12 MELFI Stem Cells Sample Case A “Stem Cells Sample Case” in a mock up of MELFI 1/2 box module Cryo tubes in the Case New Inc 34 SpX-2

JMU Alloy Semiconductor / HICARI GHF/ Kobairo Rack in JEM Alloy Semiconductor Sample Cartridge BossSupportCartridge Crystal quality will be sensitive to g-disturbances. Facility/Interfaces: GHF, MMA, IPU, N2, Vacuum, MPC, G1 Max. power: 4.2 kW Inc 33/34

JMU Aquarium C/O MEDAKA OSTEOCLAST Aquatic Habitat (EM). medaka (Oryzias latipes). Aquarium. Crew activities: AQH C/O, experiment start, fish fixation, water quality check, water exchange. Facility/Interfaces: MSPR, MELFI(+2/-95 deg. C), CCD camera (HRDL: 10 M * 3 / day) Medaka will be sampled from the Aquatic Habitat Aquariums and chemically fixed for the retrieval after approx. 2 weeks, 1 month, and 2 months from the experiment start. The Aquatic Habitat maintenance operations, such as water sampling, water quality check, water exchange, and ORU exchanges are planned. #activities 1Aquatic Habitat Checkout 2Transfer Fish to ISS 3Aquatic Habitat Experiment Start 4AQH Initila Fish Fixation (RNAlater) 5-24Aquatic Habitat Water Quality Check #1-# AQH Fish Fixation (PFA) #1-# AQH Water Exchange #1-# AQH Gas Exchanger Exchange #1-# AQH Waste Filter Exchange #1-#2 35 AQH Fish Fixation (RNAlater) 36AQH Disassmbly and Stow 37-38Transfer Sample from ISS MELFI to SpX-2 SpX-2 Inc 33/ New S32S

JMU Biomedical analyses of human hair exposed to a long–term space flight HAIR Hair Sampling with Tweezers. Crew activities: Sample collection, MELFI insertion Facility/Interfaces: MELFI (-80 deg. C) Must be performed in L+20~37 days and R-25~7 days. Samples must be inserted into MELFI within 30 minutes after sample collection. Pre, In, and Post-flight data collections are required. #activities 1Preparation 2Sample collection 3MELFI (-80 ˚C) insertion 4Stow Inc 33/34 Hair Sampling Holder SpX-2

JMU The effect of long-term microgravity exposure on cardiac autonomic function by analyzing 48-hours electrocardiogram Biological Rhythms 48hrs Crew activities: ECG recording, data transfer 48-hour electrocardiogram data recording 96-hour Actiwatch data recording In-flight data collection timings. 23 +/- 7 days after launch 16 +/- 7 days before return Pre, In, and Post-flight data collections are required. #activities 1Preparation Actiwatch (setup and don) 2Collect Actiwatch data 3Don digital Holter ECG 4Collect digital Holter ECG data and Actiwatch data 5Exchange digital Holter ECG 6Collect digital Holter ECG data and Actiwatch data 7Doff Actiwatch and digital Holter ECG 8Transfer/Dump data from space to MCC Inc 33/34 Digital Holter ECG. Actiwatch

JMU Evaluation of Onboard Diagnostic Kit 2 Execution timings. FD23+/-7and FD75+/-7 #activities 1Transfer from vehicle to ISS 2Initial checkout 3Medical Equipment #1 (FD21+/-7and FD75+/-7) Stethoscope. Medical Laptop. Digital Holter. Pulse Oximeter. USB Camera. Electroencephalogram. Inc 34Inc 33 Sphygmomanometer Myodynamometer Thermometer Day 1Day 2Day 3 Data DL

JMU Area Passive Dosimeter for Lifescience Experiments in Space 9 Area PADLES 9 The location of Area Dosimeters in KIBO. Area Dosimeter package. Crew activities: Area dosimeters installation, removal Total planned duration: 5 months Must be installed for duration above 90 % or more in total flight duration over launch to landing. #activities 1Install Area dosimeters on JPM and JLP wall. 2Radiation Measurement 3Remove Area dosimeters and stow in zip bag. Inc 33/34 32S

JMU JAXA EPO9/10 5 activities are planned for Inc 33/34. JAXA Try ZERO G JAXA Educational Contest JAXA REPORT JAXA VIDEO Educational Activity1 #activities 1-1Educational Activity1 1-2Educational Activity1 2 to 5JAXA Try ZERO G JAXA Educational Contest JAXA REPORT JAXA VIDEO Inc Inc 34

JMU Temperature data logger DS1922L. (mm) Transport environment monitor TEM for Orb-1 TEM package. Inc 33/34 Automatic measurement and recording of temperature during transportation to the ISS.

JMU Multi-mission Consolidated Equipment MCE MCE is an experimental equipment consists of 5 individual devices. IMAP (Ionosphere, Mesosphere, upper Atmosphere, and Plasma sphere mapping) GLIMS (Global Lightning and Sprite Measurement Mission) SIMPLE (Space Inflatable Membranes Pioneering Long-term Experiments) REXJ (Robot Experiment on JEM) COTS HDTV-EF MCE “Airglow” and “plasma resonance scattering light” at upper atmosphere. Sprite, elves, and blue jet. Inflatable Membranes. Robot arm with extension arm work function. COTS HDTV-EF. Inc 33/34 #activities 1MCE Experiments &Observation 1

JMU SEDA-AP RESEARCH OBJECTIVES SEDA-AP will measure space environment (neutrons, plasma, heavy ions, high-energy light particles, atomic oxygen, and cosmic dust) in ISS orbit and environmental effects on materials and electronic devices to investigate the interaction with and from the space environment at the JEM exposed facility (JEM EF). At the same time, it is also expected to conduct on-orbit verification of APBUS (Attached Payload BUS) technology, which furnishes necessary functions when mounted on the JEM EF. PLAM HIT ＳＤＯＭ

JMU MAXI ATCS Electronics Grapple Fixture PIU (KIBO-EF Interface) Carrier Interface Optical Star Sensor Ring Laser Gyro Gas Slit Cameras (GSC) Solid-state Slit Cameras (SSC) Radiator for X-ray CCDs RESEARCH OBJECTIVES The Monitor of All-sky X-ray Image (MAXI) is an X-ray camera with a wide field of view designed to monitor active astronomical objects and the universe. It will monitor the variations of the X- ray intensity of various sources in the entire sky, at the highest sensitivity so far achieved with such an instrument.

JMU SMILES RESEARCH OBJECTIVES Superconduction Submillimeter-wave Limb- emission Sounder (SMILES), is aimed at global mappings of stratospheric trace gases by means of the most senseitive submillimeter receiver. Such sensitivity is ascribed to a Superconductor- Insulator-Superconductor (SIS) mixer, which is operated at 4.5 K in a dedicated cryostat combined with a mechanical cooler.