#mlt2

[hghrules]

Commissions are open!

I WON’T‌ draw:

-gore

-nsfw

-nudity

-animals, but this can be negotiated

I will draw: pretty much anything else! I specialize in DnD‌ characters, but I’ll do anything. If something doesn’t work for me, I reserve the right to tell you so before you finish placing an order.

Message me here on tumblr or at hbxplain@gmail.com to place an order or negotiate if cash is tight! Image transcription below the cut.

Image Transcription, for handwriting’s sake:

Icons: 3 USD, +1 for solid color background, +2 per extra character AND/OR +2 per extra icon (bundle)

Bobbles: (lineless) 8 USD + 2 for solid color background

Sigils: (e.g. “I am alive,” “I will recall”)  2 USD

Detailed Backgrounds: +5 USD

Lineart: Bust–10 USD, Torso–12‌ USD, 3/4–15 USD

Flat Color: Bust–15 USD, Torso–18 USD, 3/4–20 USD

Limited Shading: Bust–20 USD, Torso–23 USD, 3/4–25 USD

Full Shading: Bust–25 USD, Torso–30 USD, 3/4–35 USD

Lineless: Bust–35 USD, Torso–45 USD

Transparency Background: +5 USD

Group Pictures: 1 character: Lineart–20 USD, Flat Color–25 USD, Full Shading–30 USD. Extra character (each): Lineart–6 USD, Flat Color–8 USD, Full Shading–10 USD

[rajenbara]

so many memories etched in one place... #LT1 #LT2 #LT3 #MLT2 #MLT3 #lecturetheatre #lecturehall #iimv #iimvisakhapatnam (at IIM Visakhapatnam) https://www.instagram.com/p/B_4tWf1gwM-/?igshid=1py0x9tadf775

[cupomonline]

Lâmpada mata mosquito BlitzWolf® BW-MLT2 - De: R$234,24 - Por: R$99,52 #cupons #cupom #desconto #ofertas #promoções #promoção #cupomdedesconto #cupomonline #cuponsdedesconto

[fortheeastculture]

DAEN MARTIAN DROPPED A WHOLE NEW BODY OF WORK TITLED "MLT2". CHECK IT OUT EXCLUSIVELY ON THE LINK BELOW.

#issaeastting

https://daevmartian.bandcamp.com/album/mlt2

[superdescontostop]

BlitzWolf BW-MLT2 Mosquito Killer RGB Light

BlitzWolf BW-MLT2 Mosquito Killer RGB Light

Característica: -UV luz atrai. -1200-1600V Grid. -Luz da atmosfera. Bateria de -2200mAh. -Modelagem de socket. -Portátil e compacto. -Dois em um. A encantadora luz RGB combinada com a luz ultravioleta torna a sua noite muito divertida. -Mosquito Killer Lamp. RGB Atmosphere Light Modo 1: luz branca Modo 2: 7 cores únicas Modo 3: RGB dinâmico -Eficaz e poderoso.A luz ultravioleta pode atrair…

[robster2001]

If I were to get only one souvenir of @cszrichmond Sweet T Tourney, this is the one I'd want. Pic courtesy a friendly CapAle server. :) #latergram #mlt2 https://ift.tt/2OpBTsZ

[livefreeshop]

MagVector: The crew completed setup activities and began the 7-day MagVector #14 experiment run. The European Space Agency (ESA) MagVector investigation studies how Earth’s magnetic field interacts with an electrical conductor. Using extremely sensitive magnetic sensors placed around and above a conductor, researchers can gain insight into ways that the magnetic field influences how conductors work. This research not only helps improve future International Space Station experiments and electrical experiments, but it could offer insights into how magnetic fields influence electrical conductors in general, the backbone of our technology. At Home in Space Questionnaire and Photo:  The crew took photos to document ISS culture in support of the At Home in Space investigation. This Canadian Space Agency experiment assesses culture, values, and psychosocial adaptation of astronauts to a space environment shared by multinational crews on long-duration missions. It is hypothesized that astronauts develop a shared space culture that is an adaptive strategy for handling cultural differences and they deal with the isolated confined environment of the spacecraft by creating a home in space. At Home in Space uses a questionnaire to investigate individual and culturally related differences, family functioning, values, coping with stress, and post-experience growth. Circadian Rhythms: The 51S crewmember removed and stowed the Double Sensors and Thermolab Unit equipment that was used to complete a 36 hour Circadian Rhythms session that began on Tuesday. Circadian Rhythms investigates the role of synchronized circadian rhythms, or the “biological clock,” and how it changes during long-duration spaceflight. Researchers hypothesize that a non-24-hour cycle of light and dark affects crewmembers’ circadian clocks. The investigation also addresses the effects of reduced physical activity, microgravity and an artificially controlled environment. Changes in body composition and body temperature, which also occur in microgravity, can affect crewmembers’ circadian rhythms as well. Understanding how these phenomena affect the biological clock will improve performance and health for future crewmembers. Two Phase Flow:  The crew setup the Two Phase Flow laptop in the Multi-Purpose Small Payload Rack (MSPR).  The Two Phase Flow investigation seeks to build a database on the heat transfer efficiency of liquids in space that can be used in the design of high-performance thermal management systems for future space platforms.  Japanese Experiment Module (JEM) Camera Robot: Following yesterday’s checkout activities, today the crew conducted a cable swap to allow the ground team to perform a software update. This device is a free-flying camera robot that provides real time video downlink and photographs. It is expected to reduce the crew time requirements to support video recording of activities, especially at the blind spot of existing JEM internal cameras.   Meteor Hard Disk Drive and Antivirus Update: The crew removed and replaced the hard drive in the Meteor laptop located in the Window Observational Research Facility (WORF) and transfered an updated Antivirus file to the laptop.  The Meteor payload is a visible spectroscopy instrument with the primary purpose of observing meteors in Earth orbit. Meteor uses image analysis to provide information on the physical and chemical properties of the meteoroid dust, such as size, density, and chemical composition. Since the parent comets or asteroids for most of the meteor showers are identified, the study of the meteoroid dust on orbit provides information about the parent comets and asteroids.   Device for the study of Critical Liquids and Crystallization) DECLIC Hose Relocation: The DECLIC supply and return hoses from the Upper Control Panel (UCP) to the Lower Control Panel (LCP) were relocated to continue troubleshooting the moderate temperature loop (MTL) flow issues to the DECLIC directional solidification insert (DSL). DECLIC is a multi-user facility utilized to study transparent media and their phase transitions in microgravity onboard the International Space Station (ISS). The DSI portion of the DECLIC multi-user facility experiment will study a series of benchmark experiments on transparent alloys that freeze like metals under microgravity onboard the International Space Station (ISS) using SCN (succinonitrile-a transparent organic substance in the liquid state that is used to study the phenomena related to solidification processes) based alloys. The DSI insert will be installed for the second run of the three series of DECLIC experiments. Space Linear Acceleration Mass Measurement Device (SLAMMD) Hardware Setup and Control Run: The crew performed a SLAMMD control run by setting up the calibration arm and attaching the calibration mass, prior to setting the software to implement a control run and payload body mass measurement. SLAMMD follows Newton’s Second Law of Motion by having two springs generate a known force against a crewmember mounted on an extension arm, the resulting acceleration being used to calculate the subject’s mass. The device is accurate to 0.5 pounds over a range from 90 pounds to 240 pounds. Extra Vehicular Activity (EVA) preparations:  Today the crew configured EVA tools, inspected the EVA Mobility Unit (EMU) Sublimators, performed an EMU loop scrub, filled the Liquid Cooled Ventilation Garment (LCVG), recharged the EMU water, and performed a conductivity test on that water in preparation for the upcoming trio of EVAs in October.  The goals of the EVAs include Remove and Replace (R&R) of a Space Station Remote Manipulator System (SSRMS) Latching End Effector (LEE), lubrication of the LEEs, and R&R of two external cameras.  Today’s Planned Activities All activities were completed unless otherwise noted. Extravehicular Activity (EVA) Reminder for On-Orbit Fitcheck Verification (OFV) RELAXATSIYA. Charging battery for Relaksatstiya experiment (initiate) At Home In Space Culture Photo Extravehicular Mobility Unit (EMU) Cooling Loop Maintenance Scrub iPad Air 2 Install Part 1 Rechecking basic sets of Quick Release Screw Clamps (ЗВБ) in MRM1 and DC1. Video recording and downlink via OCA.  Tagup with specialists as necessary European Modular Cultivation System Gas Valve Close Equipment Lock (E-LK) Preparation JEM Camera Robot Cable Swap Replacement of Pretreat Container (E-K) and hose, Replacement of Pretreat and Water Dispenser (ДкиВ) in [АСУ]. [АСУ] Activation after Replacement Max Cycle Ergometer w/Vibration Isolation & Stabilization (CEVIS) Portable PFS Subject Preparing For Upcoming MagVector Science Run Circadian Rhythms Deinstrumentation Two Phase Flow(TPF) Experiment Laptop Terminal 2(ELT2) Relocation Two Phase Flow(TPF) MMA Laptop Terminal 2(MLT2) […] September 28, 2017 at 10:00AM from NASA https://go.nasa.gov/2fXjnsl via IFTTT

[hrhprince]

ISS Daily Summary Report – 9/28/2017

MagVector: The crew completed setup activities and began the 7-day MagVector #14 experiment run. The European Space Agency (ESA) MagVector investigation studies how Earth’s magnetic field interacts with an electrical conductor. Using extremely sensitive magnetic sensors placed around and above a conductor, researchers can gain insight into ways that the magnetic field influences how conductors work. This research not only helps improve future International Space Station experiments and electrical experiments, but it could offer insights into how magnetic fields influence electrical conductors in general, the backbone of our technology. At Home in Space Questionnaire and Photo:  The crew took photos to document ISS culture in support of the At Home in Space investigation. This Canadian Space Agency experiment assesses culture, values, and psychosocial adaptation of astronauts to a space environment shared by multinational crews on long-duration missions. It is hypothesized that astronauts develop a shared space culture that is an adaptive strategy for handling cultural differences and they deal with the isolated confined environment of the spacecraft by creating a home in space. At Home in Space uses a questionnaire to investigate individual and culturally related differences, family functioning, values, coping with stress, and post-experience growth. Circadian Rhythms: The 51S crewmember removed and stowed the Double Sensors and Thermolab Unit equipment that was used to complete a 36 hour Circadian Rhythms session that began on Tuesday. Circadian Rhythms investigates the role of synchronized circadian rhythms, or the “biological clock,” and how it changes during long-duration spaceflight. Researchers hypothesize that a non-24-hour cycle of light and dark affects crewmembers’ circadian clocks. The investigation also addresses the effects of reduced physical activity, microgravity and an artificially controlled environment. Changes in body composition and body temperature, which also occur in microgravity, can affect crewmembers’ circadian rhythms as well. Understanding how these phenomena affect the biological clock will improve performance and health for future crewmembers. Two Phase Flow:  The crew setup the Two Phase Flow laptop in the Multi-Purpose Small Payload Rack (MSPR).  The Two Phase Flow investigation seeks to build a database on the heat transfer efficiency of liquids in space that can be used in the design of high-performance thermal management systems for future space platforms.  Japanese Experiment Module (JEM) Camera Robot: Following yesterday’s checkout activities, today the crew conducted a cable swap to allow the ground team to perform a software update. This device is a free-flying camera robot that provides real time video downlink and photographs. It is expected to reduce the crew time requirements to support video recording of activities, especially at the blind spot of existing JEM internal cameras.   Meteor Hard Disk Drive and Antivirus Update: The crew removed and replaced the hard drive in the Meteor laptop located in the Window Observational Research Facility (WORF) and transfered an updated Antivirus file to the laptop.  The Meteor payload is a visible spectroscopy instrument with the primary purpose of observing meteors in Earth orbit. Meteor uses image analysis to provide information on the physical and chemical properties of the meteoroid dust, such as size, density, and chemical composition. Since the parent comets or asteroids for most of the meteor showers are identified, the study of the meteoroid dust on orbit provides information about the parent comets and asteroids.   Device for the study of Critical Liquids and Crystallization) DECLIC Hose Relocation: The DECLIC supply and return hoses from the Upper Control Panel (UCP) to the Lower Control Panel (LCP) were relocated to continue troubleshooting the moderate temperature loop (MTL) flow issues to the DECLIC directional solidification insert (DSL). DECLIC is a multi-user facility utilized to study transparent media and their phase transitions in microgravity onboard the International Space Station (ISS). The DSI portion of the DECLIC multi-user facility experiment will study a series of benchmark experiments on transparent alloys that freeze like metals under microgravity onboard the International Space Station (ISS) using SCN (succinonitrile-a transparent organic substance in the liquid state that is used to study the phenomena related to solidification processes) based alloys. The DSI insert will be installed for the second run of the three series of DECLIC experiments. Space Linear Acceleration Mass Measurement Device (SLAMMD) Hardware Setup and Control Run: The crew performed a SLAMMD control run by setting up the calibration arm and attaching the calibration mass, prior to setting the software to implement a control run and payload body mass measurement. SLAMMD follows Newton’s Second Law of Motion by having two springs generate a known force against a crewmember mounted on an extension arm, the resulting acceleration being used to calculate the subject’s mass. The device is accurate to 0.5 pounds over a range from 90 pounds to 240 pounds. Extra Vehicular Activity (EVA) preparations:  Today the crew configured EVA tools, inspected the EVA Mobility Unit (EMU) Sublimators, performed an EMU loop scrub, filled the Liquid Cooled Ventilation Garment (LCVG), recharged the EMU water, and performed a conductivity test on that water in preparation for the upcoming trio of EVAs in October.  The goals of the EVAs include Remove and Replace (R&R) of a Space Station Remote Manipulator System (SSRMS) Latching End Effector (LEE), lubrication of the LEEs, and R&R of two external cameras.  Today’s Planned Activities All activities were completed unless otherwise noted. Extravehicular Activity (EVA) Reminder for On-Orbit Fitcheck Verification (OFV) RELAXATSIYA. Charging battery for Relaksatstiya experiment (initiate) At Home In Space Culture Photo Extravehicular Mobility Unit (EMU) Cooling Loop Maintenance Scrub iPad Air 2 Install Part 1 Rechecking basic sets of Quick Release Screw Clamps (ЗВБ) in MRM1 and DC1. Video recording and downlink via OCA.  Tagup with specialists as necessary European Modular Cultivation System Gas Valve Close Equipment Lock (E-LK) Preparation JEM Camera Robot Cable Swap Replacement of Pretreat Container (E-K) and hose, Replacement of Pretreat and Water Dispenser (ДкиВ) in [АСУ]. [АСУ] Activation after Replacement Max Cycle Ergometer w/Vibration Isolation & Stabilization (CEVIS) Portable PFS Subject Preparing For Upcoming MagVector Science Run Circadian Rhythms Deinstrumentation Two Phase Flow(TPF) Experiment Laptop Terminal 2(ELT2) Relocation Two Phase Flow(TPF) MMA Laptop Terminal 2(MLT2) […] from NASA http://ift.tt/2xDDLsH via IFTTT

[achmad2-blog]

ISS Daily Summary Report – 2/08/2017

Galley Rack Outfitting: Today the crew relocated the Node 1 16-Port Ethernet Switch from Node 1 Port-Deck location to the Galley Rack. All pre-existing cables remained mated to the switch during relocation, and the switch power feed will remain the same. Later today they will connect the two Microgravity Experiment Research Locker/Incubator (MERLIN) Ethernet connections to the newly relocated switch followed by the crew relocating the MERLIN-2 unit currently located in EXPRESS Rack 6 Locker-2 to the Galley Rack in Node 1.  JEM ORU Transfer Interface (JOTI) Retrieval from PMA2: Earlier today the crew ingressed the Pressurized Mating Adapter-2 (PMA2) and retrieved the JOTI hardware.  After the crew retrieved the JOTI the crew egressed PMA2. JOTI will be used tomorrow, Friday 10-February, to install the Robotics External Leak Locator (RELL) on Japanese Experiment Module (JEM) Airlock (A/L) Slide Table.  RELL operations are planned this weekend to perform surveys, focused around Radiator Beam Valve Module (RBVM) P1-3-2, to assist in an investigation into a possible External Active Thermal Control System (EATCS) Loop B leak.   Synchronized Position Hold, Engage, Reorient, Experimental Satellites (SPHERES) Universal Docking Port (UDP): The crew reconfigured the SPHERES satellites assembling the Docking Port hardware. They then loaded the test software and performed the session with ground support staff direction.  The objectives of the UDP session are to demonstrate a reliably successful docking through running multiple, repeatable docking maneuvers using both global metrology and docking port cameras; perform joint maneuvers of docked satellites using the thrusters from two satellites to demonstrate controllability; and test an algorithm for docking to a satellite which is tumbling in a slow, known manner. The addition of the Docking Ports is a critical upgrade to the SPHERES facility aboard the ISS. With the new ability to dock and undock, SPHERES provides a test bed to address many of the challenges of combining autonomous spacecraft. Mated spacecraft can assemble complex systems in orbit or combine sensors and actuators for satellite servicing and repurposing missions. The SPHERES-UDP enables testing of complex tasks through optimal and adaptive control, autonomous decision-making processes, and real-time image processing.  Cool Flames Investigation: The crew performed a gas bottle change out in the Combustion Integration Rack’s (CIR’s) Fluids and Combustion Facility (FCF) upper rack.  The Cool Flames Investigation will provide new insight into the phenomenon where some types of fuels initially burn very hot, then appear to go out — but they continue burning at a much lower temperature, with no visible flames (cool flames). Understanding cool flame combustion helps scientists develop new engines and fuels that are more efficient and less harmful to the environment. Story Time From Space Buoy Demo: The crew narrated and recorded a video demonstrating how buoyancy and sedimentation occur in microgravity just as it does on Earth. Story Time From Space combines science literacy outreach with simple demonstrations recorded aboard the ISS. Crew members read five science, technology, engineering and mathematics-related children’s books in orbit, and complete simple science concept experiments. Crew members videotape themselves reading the books and completing demonstrations. Video and data collected during the demonstrations are downlinked to the ground and posted in a video library with accompanying educational materials. The narrated demonstration based on the children’s book Max Goes to Space Station. Mobile Servicing System (MSS) Operations:  In preparation for the RELL RBVM scans this weekend, ground controllers walked off Space Station Remote Manipulator System (SSRMS) to Mobile Base System (MBS) Power and Data Grapple Fixture (PDGF) 1, unstowed Special Purpose Dexterous Manipulator (SPDM), and translated the Mobile Transporter (MT) to Worksite (WS)7.  Japanese Experiment Module Remote Manipulator System (JEMRMS) Operations:  Ground controllers at Japan’s Space Station Integration and Promotion Center (SSIPC) will maneuvered JEMRMS to stow Small Fine Arm (SFA) onto SFA Storage Equipment (SSE) and then moved to JEM AL cleared position for the next RELL transfer operation.  Treadmill 2 (T2) Belt Issue: Today the nominal, weekly T2 power cycle was not able to complete. Teams reattempted a ground powercycle via the nominal process with no joy. Crew confirmed the Graphical User Interface (GUI) was closed and the Command Logic Unit (CLU) was still showing as connected. All data LEDs indicated T2 was nominal so T2 was still considered GO for exercise. Later, however, when the crew attempted to exercise, the treadbelt would not spin. Ground teams are meeting today to determine a recovery plan. Today’s Planned Activities All activities were completed unless otherwise noted. SM and DC1 [СТТС] Tagup RELAKSATSIYA. Hardware Setup. DC1 S/G2 Comm Config Fine Motor Skills Experiment Test – Subject MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 2 Hardware setup for Orlan No.4 and Orlan No.6 checkout RELAKSATSIYA. Parameter Settings Adjustment JEM Airlock Press Orlan No. 4 Activation Water Recovery System Waste Water Tank Drain Termination RELAKSATSIYA. Observation Orlan No.4 and Orlan Interface Unit (БСС) checkout from ПКО-М panel Node 2 Endcone Cleanout RELAKSATSIYA. Closeout Ops and Hardware Removal AstroPi IR health check JEM Airlock Leak Check DAN. Experiment Ops. PMA2 Ingress Galley Ethernet Switch Relocation and Install Galley Closeout Panel JOTI Retrieval from PMA2 Orlan No.4 and БСС storage mode operation PMA2 Egress Orlan No. 6 Activation Node2 Endcone Stowage Replace Dose Tracker Data Entry Subject Orlan No.6 and Orlan Interface Unit (БСС) checkout from ПКО-М panel MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 3 Long Duration Sorbent Testbed Camera Return Story Time from Space Exploring Buoyancy Demonstration TIMER. Battery Charge Story Time From Space Historical Photo 4K Encoder Disconnect ISS HAM Radio Program MELFI 1 Electronic Unit Remove Multi-purpose Small Payload Rack (MSPR) /Group Combustion Module (GCM) Component Deactivation Comm reconfig for nominal ops SPHERES Crew Conference SPHERES Test Session Setup ESA Weekly crew conference Combustion Integrated Rack Crew Conference Orlan No.6 and БСС storage mode operation Combustion Integrated Rack Inspection Hardware Gather SPHERES Docking Port Test Run Equipment stowage after Orlan No.4 and Orlan No.6 checkout VEG-03 Plant Photo TIMER. Experiment setup and initiation of video recording Combustion Integrated Rack Bottle Replacement 1 Checkout of SM-AGAT-U42 Monitor Connection VIZIR. […] from NASA http://go.nasa.gov/2ktURPM via IFTTT | Java Wisata

[livefreeshop]

MagVector: The crew completed setup activities and began the 7-day MagVector #14 experiment run. The European Space Agency (ESA) MagVector investigation studies how Earth’s magnetic field interacts with an electrical conductor. Using extremely sensitive magnetic sensors placed around and above a conductor, researchers can gain insight into ways that the magnetic field influences how conductors work. This research not only helps improve future International Space Station experiments and electrical experiments, but it could offer insights into how magnetic fields influence electrical conductors in general, the backbone of our technology. At Home in Space Questionnaire and Photo:  The crew took photos to document ISS culture in support of the At Home in Space investigation. This Canadian Space Agency experiment assesses culture, values, and psychosocial adaptation of astronauts to a space environment shared by multinational crews on long-duration missions. It is hypothesized that astronauts develop a shared space culture that is an adaptive strategy for handling cultural differences and they deal with the isolated confined environment of the spacecraft by creating a home in space. At Home in Space uses a questionnaire to investigate individual and culturally related differences, family functioning, values, coping with stress, and post-experience growth. Circadian Rhythms: The 51S crewmember removed and stowed the Double Sensors and Thermolab Unit equipment that was used to complete a 36 hour Circadian Rhythms session that began on Tuesday. Circadian Rhythms investigates the role of synchronized circadian rhythms, or the “biological clock,” and how it changes during long-duration spaceflight. Researchers hypothesize that a non-24-hour cycle of light and dark affects crewmembers’ circadian clocks. The investigation also addresses the effects of reduced physical activity, microgravity and an artificially controlled environment. Changes in body composition and body temperature, which also occur in microgravity, can affect crewmembers’ circadian rhythms as well. Understanding how these phenomena affect the biological clock will improve performance and health for future crewmembers. Two Phase Flow:  The crew setup the Two Phase Flow laptop in the Multi-Purpose Small Payload Rack (MSPR).  The Two Phase Flow investigation seeks to build a database on the heat transfer efficiency of liquids in space that can be used in the design of high-performance thermal management systems for future space platforms.  Japanese Experiment Module (JEM) Camera Robot: Following yesterday’s checkout activities, today the crew conducted a cable swap to allow the ground team to perform a software update. This device is a free-flying camera robot that provides real time video downlink and photographs. It is expected to reduce the crew time requirements to support video recording of activities, especially at the blind spot of existing JEM internal cameras.   Meteor Hard Disk Drive and Antivirus Update: The crew removed and replaced the hard drive in the Meteor laptop located in the Window Observational Research Facility (WORF) and transfered an updated Antivirus file to the laptop.  The Meteor payload is a visible spectroscopy instrument with the primary purpose of observing meteors in Earth orbit. Meteor uses image analysis to provide information on the physical and chemical properties of the meteoroid dust, such as size, density, and chemical composition. Since the parent comets or asteroids for most of the meteor showers are identified, the study of the meteoroid dust on orbit provides information about the parent comets and asteroids.   Device for the study of Critical Liquids and Crystallization) DECLIC Hose Relocation: The DECLIC supply and return hoses from the Upper Control Panel (UCP) to the Lower Control Panel (LCP) were relocated to continue troubleshooting the moderate temperature loop (MTL) flow issues to the DECLIC directional solidification insert (DSL). DECLIC is a multi-user facility utilized to study transparent media and their phase transitions in microgravity onboard the International Space Station (ISS). The DSI portion of the DECLIC multi-user facility experiment will study a series of benchmark experiments on transparent alloys that freeze like metals under microgravity onboard the International Space Station (ISS) using SCN (succinonitrile-a transparent organic substance in the liquid state that is used to study the phenomena related to solidification processes) based alloys. The DSI insert will be installed for the second run of the three series of DECLIC experiments. Space Linear Acceleration Mass Measurement Device (SLAMMD) Hardware Setup and Control Run: The crew performed a SLAMMD control run by setting up the calibration arm and attaching the calibration mass, prior to setting the software to implement a control run and payload body mass measurement. SLAMMD follows Newton’s Second Law of Motion by having two springs generate a known force against a crewmember mounted on an extension arm, the resulting acceleration being used to calculate the subject’s mass. The device is accurate to 0.5 pounds over a range from 90 pounds to 240 pounds. Extra Vehicular Activity (EVA) preparations:  Today the crew configured EVA tools, inspected the EVA Mobility Unit (EMU) Sublimators, performed an EMU loop scrub, filled the Liquid Cooled Ventilation Garment (LCVG), recharged the EMU water, and performed a conductivity test on that water in preparation for the upcoming trio of EVAs in October.  The goals of the EVAs include Remove and Replace (R&R) of a Space Station Remote Manipulator System (SSRMS) Latching End Effector (LEE), lubrication of the LEEs, and R&R of two external cameras.  Today’s Planned Activities All activities were completed unless otherwise noted. Extravehicular Activity (EVA) Reminder for On-Orbit Fitcheck Verification (OFV) RELAXATSIYA. Charging battery for Relaksatstiya experiment (initiate) At Home In Space Culture Photo Extravehicular Mobility Unit (EMU) Cooling Loop Maintenance Scrub iPad Air 2 Install Part 1 Rechecking basic sets of Quick Release Screw Clamps (ЗВБ) in MRM1 and DC1. Video recording and downlink via OCA.  Tagup with specialists as necessary European Modular Cultivation System Gas Valve Close Equipment Lock (E-LK) Preparation JEM Camera Robot Cable Swap Replacement of Pretreat Container (E-K) and hose, Replacement of Pretreat and Water Dispenser (ДкиВ) in [АСУ]. [АСУ] Activation after Replacement Max Cycle Ergometer w/Vibration Isolation & Stabilization (CEVIS) Portable PFS Subject Preparing For Upcoming MagVector Science Run Circadian Rhythms Deinstrumentation Two Phase Flow(TPF) Experiment Laptop Terminal 2(ELT2) Relocation Two Phase Flow(TPF) MMA Laptop Terminal 2(MLT2) […] from ISS On-Orbit Status Report https://go.nasa.gov/2fXjnsl

[livefreeshop]

Galley Rack Outfitting: Today the crew relocated the Node 1 16-Port Ethernet Switch from Node 1 Port-Deck location to the Galley Rack. All pre-existing cables remained mated to the switch during relocation, and the switch power feed will remain the same. Later today they will connect the two Microgravity Experiment Research Locker/Incubator (MERLIN) Ethernet connections to the newly relocated switch followed by the crew relocating the MERLIN-2 unit currently located in EXPRESS Rack 6 Locker-2 to the Galley Rack in Node 1.  JEM ORU Transfer Interface (JOTI) Retrieval from PMA2: Earlier today the crew ingressed the Pressurized Mating Adapter-2 (PMA2) and retrieved the JOTI hardware.  After the crew retrieved the JOTI the crew egressed PMA2. JOTI will be used tomorrow, Friday 10-February, to install the Robotics External Leak Locator (RELL) on Japanese Experiment Module (JEM) Airlock (A/L) Slide Table.  RELL operations are planned this weekend to perform surveys, focused around Radiator Beam Valve Module (RBVM) P1-3-2, to assist in an investigation into a possible External Active Thermal Control System (EATCS) Loop B leak.   Synchronized Position Hold, Engage, Reorient, Experimental Satellites (SPHERES) Universal Docking Port (UDP): The crew reconfigured the SPHERES satellites assembling the Docking Port hardware. They then loaded the test software and performed the session with ground support staff direction.  The objectives of the UDP session are to demonstrate a reliably successful docking through running multiple, repeatable docking maneuvers using both global metrology and docking port cameras; perform joint maneuvers of docked satellites using the thrusters from two satellites to demonstrate controllability; and test an algorithm for docking to a satellite which is tumbling in a slow, known manner. The addition of the Docking Ports is a critical upgrade to the SPHERES facility aboard the ISS. With the new ability to dock and undock, SPHERES provides a test bed to address many of the challenges of combining autonomous spacecraft. Mated spacecraft can assemble complex systems in orbit or combine sensors and actuators for satellite servicing and repurposing missions. The SPHERES-UDP enables testing of complex tasks through optimal and adaptive control, autonomous decision-making processes, and real-time image processing.  Cool Flames Investigation: The crew performed a gas bottle change out in the Combustion Integration Rack’s (CIR’s) Fluids and Combustion Facility (FCF) upper rack.  The Cool Flames Investigation will provide new insight into the phenomenon where some types of fuels initially burn very hot, then appear to go out — but they continue burning at a much lower temperature, with no visible flames (cool flames). Understanding cool flame combustion helps scientists develop new engines and fuels that are more efficient and less harmful to the environment. Story Time From Space Buoy Demo: The crew narrated and recorded a video demonstrating how buoyancy and sedimentation occur in microgravity just as it does on Earth. Story Time From Space combines science literacy outreach with simple demonstrations recorded aboard the ISS. Crew members read five science, technology, engineering and mathematics-related children’s books in orbit, and complete simple science concept experiments. Crew members videotape themselves reading the books and completing demonstrations. Video and data collected during the demonstrations are downlinked to the ground and posted in a video library with accompanying educational materials. The narrated demonstration based on the children’s book Max Goes to Space Station. Mobile Servicing System (MSS) Operations:  In preparation for the RELL RBVM scans this weekend, ground controllers walked off Space Station Remote Manipulator System (SSRMS) to Mobile Base System (MBS) Power and Data Grapple Fixture (PDGF) 1, unstowed Special Purpose Dexterous Manipulator (SPDM), and translated the Mobile Transporter (MT) to Worksite (WS)7.  Japanese Experiment Module Remote Manipulator System (JEMRMS) Operations:  Ground controllers at Japan’s Space Station Integration and Promotion Center (SSIPC) will maneuvered JEMRMS to stow Small Fine Arm (SFA) onto SFA Storage Equipment (SSE) and then moved to JEM AL cleared position for the next RELL transfer operation.  Treadmill 2 (T2) Belt Issue: Today the nominal, weekly T2 power cycle was not able to complete. Teams reattempted a ground powercycle via the nominal process with no joy. Crew confirmed the Graphical User Interface (GUI) was closed and the Command Logic Unit (CLU) was still showing as connected. All data LEDs indicated T2 was nominal so T2 was still considered GO for exercise. Later, however, when the crew attempted to exercise, the treadbelt would not spin. Ground teams are meeting today to determine a recovery plan. Today’s Planned Activities All activities were completed unless otherwise noted. SM and DC1 [СТТС] Tagup RELAKSATSIYA. Hardware Setup. DC1 S/G2 Comm Config Fine Motor Skills Experiment Test – Subject MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 2 Hardware setup for Orlan No.4 and Orlan No.6 checkout RELAKSATSIYA. Parameter Settings Adjustment JEM Airlock Press Orlan No. 4 Activation Water Recovery System Waste Water Tank Drain Termination RELAKSATSIYA. Observation Orlan No.4 and Orlan Interface Unit (БСС) checkout from ПКО-М panel Node 2 Endcone Cleanout RELAKSATSIYA. Closeout Ops and Hardware Removal AstroPi IR health check JEM Airlock Leak Check DAN. Experiment Ops. PMA2 Ingress Galley Ethernet Switch Relocation and Install Galley Closeout Panel JOTI Retrieval from PMA2 Orlan No.4 and БСС storage mode operation PMA2 Egress Orlan No. 6 Activation Node2 Endcone Stowage Replace Dose Tracker Data Entry Subject Orlan No.6 and Orlan Interface Unit (БСС) checkout from ПКО-М panel MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 3 Long Duration Sorbent Testbed Camera Return Story Time from Space Exploring Buoyancy Demonstration TIMER. Battery Charge Story Time From Space Historical Photo 4K Encoder Disconnect ISS HAM Radio Program MELFI 1 Electronic Unit Remove Multi-purpose Small Payload Rack (MSPR) /Group Combustion Module (GCM) Component Deactivation Comm reconfig for nominal ops SPHERES Crew Conference SPHERES Test Session Setup ESA Weekly crew conference Combustion Integrated Rack Crew Conference Orlan No.6 and БСС storage mode operation Combustion Integrated Rack Inspection Hardware Gather SPHERES Docking Port Test Run Equipment stowage after Orlan No.4 and Orlan No.6 checkout VEG-03 Plant Photo TIMER. Experiment setup and initiation of video recording Combustion Integrated Rack Bottle Replacement 1 Checkout of SM-AGAT-U42 Monitor Connection VIZIR. […] February 09, 2017 at 10:00AM from NASA http://go.nasa.gov/2kA8aAx via IFTTT

[livefreeshop]

Galley Rack Outfitting: Today the crew relocated the Node 1 16-Port Ethernet Switch from Node 1 Port-Deck location to the Galley Rack. All pre-existing cables remained mated to the switch during relocation, and the switch power feed will remain the same. Later today they will connect the two Microgravity Experiment Research Locker/Incubator (MERLIN) Ethernet connections to the newly relocated switch followed by the crew relocating the MERLIN-2 unit currently located in EXPRESS Rack 6 Locker-2 to the Galley Rack in Node 1.  JEM ORU Transfer Interface (JOTI) Retrieval from PMA2: Earlier today the crew ingressed the Pressurized Mating Adapter-2 (PMA2) and retrieved the JOTI hardware.  After the crew retrieved the JOTI the crew egressed PMA2. JOTI will be used tomorrow, Friday 10-February, to install the Robotics External Leak Locator (RELL) on Japanese Experiment Module (JEM) Airlock (A/L) Slide Table.  RELL operations are planned this weekend to perform surveys, focused around Radiator Beam Valve Module (RBVM) P1-3-2, to assist in an investigation into a possible External Active Thermal Control System (EATCS) Loop B leak.   Synchronized Position Hold, Engage, Reorient, Experimental Satellites (SPHERES) Universal Docking Port (UDP): The crew reconfigured the SPHERES satellites assembling the Docking Port hardware. They then loaded the test software and performed the session with ground support staff direction.  The objectives of the UDP session are to demonstrate a reliably successful docking through running multiple, repeatable docking maneuvers using both global metrology and docking port cameras; perform joint maneuvers of docked satellites using the thrusters from two satellites to demonstrate controllability; and test an algorithm for docking to a satellite which is tumbling in a slow, known manner. The addition of the Docking Ports is a critical upgrade to the SPHERES facility aboard the ISS. With the new ability to dock and undock, SPHERES provides a test bed to address many of the challenges of combining autonomous spacecraft. Mated spacecraft can assemble complex systems in orbit or combine sensors and actuators for satellite servicing and repurposing missions. The SPHERES-UDP enables testing of complex tasks through optimal and adaptive control, autonomous decision-making processes, and real-time image processing.  Cool Flames Investigation: The crew performed a gas bottle change out in the Combustion Integration Rack’s (CIR’s) Fluids and Combustion Facility (FCF) upper rack.  The Cool Flames Investigation will provide new insight into the phenomenon where some types of fuels initially burn very hot, then appear to go out — but they continue burning at a much lower temperature, with no visible flames (cool flames). Understanding cool flame combustion helps scientists develop new engines and fuels that are more efficient and less harmful to the environment. Story Time From Space Buoy Demo: The crew narrated and recorded a video demonstrating how buoyancy and sedimentation occur in microgravity just as it does on Earth. Story Time From Space combines science literacy outreach with simple demonstrations recorded aboard the ISS. Crew members read five science, technology, engineering and mathematics-related children’s books in orbit, and complete simple science concept experiments. Crew members videotape themselves reading the books and completing demonstrations. Video and data collected during the demonstrations are downlinked to the ground and posted in a video library with accompanying educational materials. The narrated demonstration based on the children’s book Max Goes to Space Station. Mobile Servicing System (MSS) Operations:  In preparation for the RELL RBVM scans this weekend, ground controllers walked off Space Station Remote Manipulator System (SSRMS) to Mobile Base System (MBS) Power and Data Grapple Fixture (PDGF) 1, unstowed Special Purpose Dexterous Manipulator (SPDM), and translated the Mobile Transporter (MT) to Worksite (WS)7.  Japanese Experiment Module Remote Manipulator System (JEMRMS) Operations:  Ground controllers at Japan’s Space Station Integration and Promotion Center (SSIPC) will maneuvered JEMRMS to stow Small Fine Arm (SFA) onto SFA Storage Equipment (SSE) and then moved to JEM AL cleared position for the next RELL transfer operation.  Treadmill 2 (T2) Belt Issue: Today the nominal, weekly T2 power cycle was not able to complete. Teams reattempted a ground powercycle via the nominal process with no joy. Crew confirmed the Graphical User Interface (GUI) was closed and the Command Logic Unit (CLU) was still showing as connected. All data LEDs indicated T2 was nominal so T2 was still considered GO for exercise. Later, however, when the crew attempted to exercise, the treadbelt would not spin. Ground teams are meeting today to determine a recovery plan. Today’s Planned Activities All activities were completed unless otherwise noted. SM and DC1 [СТТС] Tagup RELAKSATSIYA. Hardware Setup. DC1 S/G2 Comm Config Fine Motor Skills Experiment Test – Subject MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 2 Hardware setup for Orlan No.4 and Orlan No.6 checkout RELAKSATSIYA. Parameter Settings Adjustment JEM Airlock Press Orlan No. 4 Activation Water Recovery System Waste Water Tank Drain Termination RELAKSATSIYA. Observation Orlan No.4 and Orlan Interface Unit (БСС) checkout from ПКО-М panel Node 2 Endcone Cleanout RELAKSATSIYA. Closeout Ops and Hardware Removal AstroPi IR health check JEM Airlock Leak Check DAN. Experiment Ops. PMA2 Ingress Galley Ethernet Switch Relocation and Install Galley Closeout Panel JOTI Retrieval from PMA2 Orlan No.4 and БСС storage mode operation PMA2 Egress Orlan No. 6 Activation Node2 Endcone Stowage Replace Dose Tracker Data Entry Subject Orlan No.6 and Orlan Interface Unit (БСС) checkout from ПКО-М panel MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 3 Long Duration Sorbent Testbed Camera Return Story Time from Space Exploring Buoyancy Demonstration TIMER. Battery Charge Story Time From Space Historical Photo 4K Encoder Disconnect ISS HAM Radio Program MELFI 1 Electronic Unit Remove Multi-purpose Small Payload Rack (MSPR) /Group Combustion Module (GCM) Component Deactivation Comm reconfig for nominal ops SPHERES Crew Conference SPHERES Test Session Setup ESA Weekly crew conference Combustion Integrated Rack Crew Conference Orlan No.6 and БСС storage mode operation Combustion Integrated Rack Inspection Hardware Gather SPHERES Docking Port Test Run Equipment stowage after Orlan No.4 and Orlan No.6 checkout VEG-03 Plant Photo TIMER. Experiment setup and initiation of video recording Combustion Integrated Rack Bottle Replacement 1 Checkout of SM-AGAT-U42 Monitor Connection VIZIR. […] from ISS On-Orbit Status Report http://go.nasa.gov/2kA8aAx

[hrhprince]

ISS Daily Summary Report – 2/08/2017

Galley Rack Outfitting: Today the crew relocated the Node 1 16-Port Ethernet Switch from Node 1 Port-Deck location to the Galley Rack. All pre-existing cables remained mated to the switch during relocation, and the switch power feed will remain the same. Later today they will connect the two Microgravity Experiment Research Locker/Incubator (MERLIN) Ethernet connections to the newly relocated switch followed by the crew relocating the MERLIN-2 unit currently located in EXPRESS Rack 6 Locker-2 to the Galley Rack in Node 1.  JEM ORU Transfer Interface (JOTI) Retrieval from PMA2: Earlier today the crew ingressed the Pressurized Mating Adapter-2 (PMA2) and retrieved the JOTI hardware.  After the crew retrieved the JOTI the crew egressed PMA2. JOTI will be used tomorrow, Friday 10-February, to install the Robotics External Leak Locator (RELL) on Japanese Experiment Module (JEM) Airlock (A/L) Slide Table.  RELL operations are planned this weekend to perform surveys, focused around Radiator Beam Valve Module (RBVM) P1-3-2, to assist in an investigation into a possible External Active Thermal Control System (EATCS) Loop B leak.   Synchronized Position Hold, Engage, Reorient, Experimental Satellites (SPHERES) Universal Docking Port (UDP): The crew reconfigured the SPHERES satellites assembling the Docking Port hardware. They then loaded the test software and performed the session with ground support staff direction.  The objectives of the UDP session are to demonstrate a reliably successful docking through running multiple, repeatable docking maneuvers using both global metrology and docking port cameras; perform joint maneuvers of docked satellites using the thrusters from two satellites to demonstrate controllability; and test an algorithm for docking to a satellite which is tumbling in a slow, known manner. The addition of the Docking Ports is a critical upgrade to the SPHERES facility aboard the ISS. With the new ability to dock and undock, SPHERES provides a test bed to address many of the challenges of combining autonomous spacecraft. Mated spacecraft can assemble complex systems in orbit or combine sensors and actuators for satellite servicing and repurposing missions. The SPHERES-UDP enables testing of complex tasks through optimal and adaptive control, autonomous decision-making processes, and real-time image processing.  Cool Flames Investigation: The crew performed a gas bottle change out in the Combustion Integration Rack’s (CIR’s) Fluids and Combustion Facility (FCF) upper rack.  The Cool Flames Investigation will provide new insight into the phenomenon where some types of fuels initially burn very hot, then appear to go out — but they continue burning at a much lower temperature, with no visible flames (cool flames). Understanding cool flame combustion helps scientists develop new engines and fuels that are more efficient and less harmful to the environment. Story Time From Space Buoy Demo: The crew narrated and recorded a video demonstrating how buoyancy and sedimentation occur in microgravity just as it does on Earth. Story Time From Space combines science literacy outreach with simple demonstrations recorded aboard the ISS. Crew members read five science, technology, engineering and mathematics-related children’s books in orbit, and complete simple science concept experiments. Crew members videotape themselves reading the books and completing demonstrations. Video and data collected during the demonstrations are downlinked to the ground and posted in a video library with accompanying educational materials. The narrated demonstration based on the children’s book Max Goes to Space Station. Mobile Servicing System (MSS) Operations:  In preparation for the RELL RBVM scans this weekend, ground controllers walked off Space Station Remote Manipulator System (SSRMS) to Mobile Base System (MBS) Power and Data Grapple Fixture (PDGF) 1, unstowed Special Purpose Dexterous Manipulator (SPDM), and translated the Mobile Transporter (MT) to Worksite (WS)7.  Japanese Experiment Module Remote Manipulator System (JEMRMS) Operations:  Ground controllers at Japan’s Space Station Integration and Promotion Center (SSIPC) will maneuvered JEMRMS to stow Small Fine Arm (SFA) onto SFA Storage Equipment (SSE) and then moved to JEM AL cleared position for the next RELL transfer operation.  Treadmill 2 (T2) Belt Issue: Today the nominal, weekly T2 power cycle was not able to complete. Teams reattempted a ground powercycle via the nominal process with no joy. Crew confirmed the Graphical User Interface (GUI) was closed and the Command Logic Unit (CLU) was still showing as connected. All data LEDs indicated T2 was nominal so T2 was still considered GO for exercise. Later, however, when the crew attempted to exercise, the treadbelt would not spin. Ground teams are meeting today to determine a recovery plan. Today’s Planned Activities All activities were completed unless otherwise noted. SM and DC1 [СТТС] Tagup RELAKSATSIYA. Hardware Setup. DC1 S/G2 Comm Config Fine Motor Skills Experiment Test – Subject MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 2 Hardware setup for Orlan No.4 and Orlan No.6 checkout RELAKSATSIYA. Parameter Settings Adjustment JEM Airlock Press Orlan No. 4 Activation Water Recovery System Waste Water Tank Drain Termination RELAKSATSIYA. Observation Orlan No.4 and Orlan Interface Unit (БСС) checkout from ПКО-М panel Node 2 Endcone Cleanout RELAKSATSIYA. Closeout Ops and Hardware Removal AstroPi IR health check JEM Airlock Leak Check DAN. Experiment Ops. PMA2 Ingress Galley Ethernet Switch Relocation and Install Galley Closeout Panel JOTI Retrieval from PMA2 Orlan No.4 and БСС storage mode operation PMA2 Egress Orlan No. 6 Activation Node2 Endcone Stowage Replace Dose Tracker Data Entry Subject Orlan No.6 and Orlan Interface Unit (БСС) checkout from ПКО-М panel MLT2 Setup for EFU Adapter Wireless Access Point Checkout Part 3 Long Duration Sorbent Testbed Camera Return Story Time from Space Exploring Buoyancy Demonstration TIMER. Battery Charge Story Time From Space Historical Photo 4K Encoder Disconnect ISS HAM Radio Program MELFI 1 Electronic Unit Remove Multi-purpose Small Payload Rack (MSPR) /Group Combustion Module (GCM) Component Deactivation Comm reconfig for nominal ops SPHERES Crew Conference SPHERES Test Session Setup ESA Weekly crew conference Combustion Integrated Rack Crew Conference Orlan No.6 and БСС storage mode operation Combustion Integrated Rack Inspection Hardware Gather SPHERES Docking Port Test Run Equipment stowage after Orlan No.4 and Orlan No.6 checkout VEG-03 Plant Photo TIMER. Experiment setup and initiation of video recording Combustion Integrated Rack Bottle Replacement 1 Checkout of SM-AGAT-U42 Monitor Connection VIZIR. […] from NASA http://ift.tt/2kX3vd7 via IFTTT