| ISS Facilities and Inserts |
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Acceleration Measurement and
Environment Characterization |
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Space Acceleration Measurement System
(SAMS) and Microgravity Acceleration Measurement System (MAMS) provide
continuous measurement of the ISS vibratory and quasi-steady acceleration
environment, respectively. SAMS
measurement capability extends to all three laboratories, while MAMS
data can be mathematically mapped to any arbitrary location using
rigid-body assumptions.
SAMS and MAMS support NASA’s Physical Sciences Research Program. These
systems along with PIMS analysis serve a critical, ongoing role in
support of vehicle/loads monitoring. These instruments
along with the Principal Investigator Microgravity Services (PIMS)
project serve a critical, ongoing role in support of vehicle loads
and dynamics monitoring, assist technology developers and principal
investigators in various disciplines. The goal is to characterize
and understand the acceleration environment as related to a wide array
of disturbances and events that routinely or uniquely take place on
the ISS. |
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| Figure 5.1-1. SAMS control unit and tri-axial sensor head. |
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Figure 5.1-2. Spectral analysis of SAMS data as shown in
the spectrogram above reveals structure & boundaries in time
and frequency to help qualify microgravity events. |
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Microgravity Acceleration Measurement
System (MAMS) |
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Principal Investigator Microgravity
Services (PIMS) |
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Space Acceleration Measurements System
II (SAMS-II) |
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Cumbustion Integrated Rack (CIR) |
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The Combustion Integrated Rack (CIR) was designed
to test experiments that focus on fire prevention, detection and suppression
of fires in space. The hardware was delivered on STS-126 (November
2008) to the ISS and installed in the US LAB. The CIR provides
a 100-liter chamber with eight optical windows with easily reconfigurable
diagnostics, digital cameras and lighting with large data storage
capability, gas distribution/cleanup, passive vibration isolation,
and vacuum resources to support a wide range of gravity-dependent
gaseous, liquid and solid combustion experiments. |
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Fluids Integrated Rack (FIR) |
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The Fluids Integrated Rack (FIR) was designed to
test and understand critical technologies needed for advanced life
support and future spacecraft thermal control, research in complex
fluids (colloids) and life science experiments. The hardware
was delivered on STS-128 (August 2009) to the ISS and installed in
the US LAB. The FIR provides the largest, contiguous volume
for experimental hardware of any ISS facility, easily reconfigurable
diagnostics, customizable software, active rack-level vibration isolation,
and other subsystems that are required to support a wide range of
gravity-dependent fluid physics and life science investigations. |
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Electro-Magnetic
Levitator (EML) |
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Five of the current US materials
science investigations are to be performed in the Electro-Magnetic
Levitation (EML) facility. The facility utilizes electromagnetic
induction to position and heat samples and high speed video and optical
pyrometry to observe the samples. A sample’s viscosity,
surface tension, thermal expansion, and nucleation behavior can be
determined over a wide range of temperatures. This facility
was built as a cooperative effort between ESA and DLR. NASA
investigators use the EML through a barter arrangement with ESA. The
EML is to be delivered to ISS on ATV-4. Experiments are in planning
for the following six years. A new set of EML samples is to
be delivered to ISS each year once the facility is on orbit. |
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Expedite
the Processing of Experiments to Space Station (EXPRESS) Racks |
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The eight EXpedite the PRocessing
of Experiments to Space Station (EXPRESS) racks are multi-use facilities
which provide standard interfaces and resources for Middeck Locker
(MDL) and International Subrack Interface Standard (ISIS) Payloads. Payloads
using single, double, or quad locker configurations can be accommodated
by these racks. The racks provide a number of services for payloads
including Nitrogen, Vacuum, RS422, ethernet, video, air and water-cooling. |
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| Figure
5.7-1. Front view of an EXPRESS rack |
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Microgravity Science Glovebox (MSG) |
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The
Microgravity Science Glovebox (MSG) is a rack facility aboard the
International Space Station (ISS) in which fundamental and applied
scientific research is conducted. The MSG has been operating on the
ISS since July 2002 and is located in the US Laboratory. The unique
design of the facility allows it to accommodate science and technology
investigations in a “workbench” type environment. The
facility has an enclosed working volume that is held at a negative
pressure with respect to the crew living area. This allows the facility
to provide two levels of containment for small parts, particulates,
fluids, and gases. This containment approach protects the crew from
possible hazardous operations that take place inside the MSG work
volume. Research investigations operating inside the MSG are provided
a large 255 liter enclosed work space, 1000 watts of dc power via
a versatile supply interface (120, 28, + 12, and 5 Vdc), 1000 watts
of cooling capability, video and data recording and real time downlink,
ground commanding capabilities, access to ISS Vacuum Exhaust and Vacuum
Resource Systems, and gaseous nitrogen supply. These capabilities
make the MSG one of the most utilized science facilities on ISS. In
fact, the MSG has been used for over 10,000 hours of scientific payload
operations. MSG investigations involve research in cryogenic fluid
management, fluid physics, spacecraft fire safety, materials science,
combustion, plant growth, human health, and life support technologies.
The MSG facility is ideal for advancing our understanding of the role
of gravity upon science investigations and research and to utilize
the ISS as a technology platform for space exploration.
Microgravity
Science Glovebox (MSG) Quad Chart
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Materials Science Research Rack (MSRR) |
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The
MSRR is designed to study a variety of materials including metals,
ceramics, semiconductor crystals, and glasses for developing improved
materials. The MSRR was launched on STS-128 in August 2009 and is
installed in the USLAB. Eight current NASA investigator lead projects
are to be conducted in Materials Science Research Rack (MSRR) furnace
inserts. An additional three NASA funded projects provide modeling
support to international science teams utilizing the MSRR. The rack
is a NASA development and contains the ESA developed Materials Science
Laboratory (MSL). Two furnace inserts that interface to the MSL are
also supplied by ESA. NASA and ESA utilize the rack and its inserts
in a shared arrangement. MSRR is a highly automated facility in which
sample cartridges can be processed up to temperatures of 1400 °C.
The experiments can be run by automatic command or via telemetry commands
from the ground. The initial US MSRR investigations are to be performed
between 2013 and 2017. Additional MSRR investigations are to be selected
in the 2015-2016 timeframe.
Materials
Science Research Rack (MSRR) Quad Chart
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