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SHERE Status
The SHERE experiment has completed all 25 test
runs during Increment 18 operation and all 20 test runs plus eight
repeat test run during Increment 17 operations. Both sets of SHERE
fluid modules have been returned to Earth in preparation for SHERE
II operations in 2010.
- Dec 2008-Jan 2009: Successful completion
of 25 Test Runs by Mike Fincke.
- Dec 27, 2008: A Dry Run Test was
completed by astronaut Mike Fincke and allowed Mike a chance to
go through the procedures and practice using tools needed specifically
to install, deploy and remove a fluid module during science testing.
- Nov 14, 2008: Twenty-six additional
Fluid Modules (consisting of 25 filled Fluid Modules and one "dry" Fluid
Module) were launched on the STS 126/Endeavour (Flight ULF-2).
- Aug 2 - Sept 30, 2008: Succesful completion
of 20 Test Runs plus eight repeat test runs by Greg Chamitoff.
- July 26, 2008: A Dry Run Test was completed
by astronaut Greg
Chamitoff. This test is used to perform a functional test of the
SHERE
hardware using a "dry" fluid module. It also allowed Greg
a chance to
go through the procedures and practice using tools needed specifically
to install, deploy and remove a fluid module during science testing.
- July 20, 2008: Check-out of several
hardware components, such as the
force transducer, laser micrometer and SHERE camera, on the flight
hardware was successfully performed by astronaut Greg Chamitoff.
- June 29, 2008: The SHERE Hardware
(Interface Box, Rheometer, Camera Arm, Keyboard, Toolbox and cable
assemblies) was successfully set-up in the Microgravity Science
Glovebox by astronaut Greg Chamitoff. SHERE Software Load was
also performed.
- March 11, 2008: The
Fluid Modules (consisting of 20 filled Fluid Modules and one "dry" Fluid
Module) were launched on the STS 123/Endeavour (Flight 1J/A).
- October 23, 2007: The
Main Hardware (Rheometer, Interface Box, Toolbox, Keyboard, Camera
Arm and cable assemblies) was launched inside the Harmony Module
on the STS-120/Discovery.
Background
The resistance of a fluid to an imposed flow is termed ‘viscosity’,
and it is a fundamental material parameter by which manufacturers
and end-users characterize a material. Normally, researchers place
a material in a commercial instrument that imposes a simple rotational
shearing flow and obtains a rate-dependent shear viscosity. While
this level of characterization is sufficient for some processes, in
typical industrial polymer processing operations the material experiences
a complex flow history with both shear and extensional characteristics.
For example, in fiber spinning, the fluid experiences a complex rotational
shear flow as it flows through the spinneret head before entering
a region of dominant axial elongation in the spinline.
Polymer behavior under these conditions is process-dependent and stems
from their long chain structure. Polymers are typically hydrocarbon-based
molecules composed of repeated molecular units and can contain hundreds
to tens of thousands of these repeat units. The resulting long molecular
chain is usually very flexible, allowing the polymer to coil, extend,
and entangle with neighboring polymer chains. In its rest state, a
typical polymer chain will assume a random coiled configuration. When
exposed to a rotational shearing flow, this coil will align 45o to
the flow direction and flip over and over again to coil the polymer
chain. When exposed to an extensional flow, the coil extends axially
and can be pulled taut if the flow is strong enough. Because polymers
act like springs, more stress is required to stretch them to higher
strains. This relationship between stress and extensional deformation
rate (i.e., strain rate) is expressed as an extensional viscosity
and is a fundamental material parameter independent of shear viscosity.
Science Overview
Due to the coiling effect of rotational shear flow on the
polymer chains, shearing on the fluid immediately before extension
will have an effect on the extensional behavior of the fluid. Therefore,
the main objective of SHERE is to study the effect of rotational
preshear on the extensional behavior of the fluid. Of specific interest
is the transient evolution of the microstructure and viscoelastic
tensile stresses that are present during the extension of the fluid.
The combination of both shearing and extensional flows is common in
many polymer-processing operations such as extrusion, blow-molding
and fiber spinning. Therefore, knowledge of the complete rheological
properties of the polymer fluid is required in order to accurately
predict and account for its flow behavior. In addition, if numerical
simulations are to serve as a priori design tools for optimizing
polymer processing operations, then it is critical to have an accurate
knowledge of the extensional viscosity and its variation with temperature,
concentration, molecular weight, and strain rate.
Unlike common Newtonian fluids, complex fluids such as polymers cannot
be characterized by a single material parameter such as the Newtonian
(shear) viscosity. Instead, they exhibit nonlinear responses to imposed
deformations. The extensional function of non-Newtonian fluids is
not constant but depends on both the rate of deformation and the total
strain experienced by a fluid element.
A class of dilute polymer solutions, collectively referred to as ‘Boger
fluids,’ has become a popular choice for rheological studies
of non-Newtonian fluids and will be used in this experiment. These
ideal elastic fluids exhibit a nearly constant shear viscosity, which
allows a direct comparison of Boger fluids with Newtonian fluids having
similar viscosities. The high viscosity of the suspending solvent
results in long relaxation times and substantial normal stresses,
and the low concentration of high molecular weight polymers facilitates
modeling analysis.
Experiment Operations
SHERE is designed to fly in the Microgravity Science Glovebox
(MSG) on the International Space Station (ISS). The main SHERE hardware
consists of the interface box, rheometer, camera arm, cabling,
keyboard, and tool box as shown in Figure 1. In addition, there
are 25 fluid modules in a stowage tray (not shown). The interface
box contains all power distribution, controllers, and data acquisition
and storage. It also contains the video system that combines the
camera view and data display onto one video signal for recording
and downlink. The rheometer (see Figure 2) contains the rotational
preshear motor, translation slider, sensitive force transducer,
electroluminescent backlight panel, laser micrometer, and thermistors.
During testing it will also contain one of the 25 fluid modules.
The camera arm attaches to rheometer for video recording of the
stretched fluid’s shape. The tool box contains miscellaneous
tools used during setup and operation of the experiment. The keyboard
is used to control the experiment with the help of the MSG video
monitor. The 25 fluid modules contain the fluid that will be sheared
and stretched during the course of the experiment. Each fluid module
contains prepackaged Boger fluid, and all samples are identical.
The fluid modules are stored at 20ºC at least 24 hours prior
to testing. After the hardware is installed in the MSG, the experiment
goes through a set of initial check-out and calibration procedures.
Once these procedures are complete, one fluid module is installed
in the rheometer, the outside shells of the fluid module are removed
and the inner shroud is slid back to expose the Boger fluid. The preshear
motor is then rotated at a slow 100 rpm, and a stable fluid column
is verified. Horizontal and vertical position controls are available
as necessary to achieve a stable column. A test point is then selected
(preshear and strain rates), and the experiment automatically executes.
The fluid is presheared and stretched according to a preprogrammed
exponential velocity profile. The stretch is stopped abruptly at 194
mm in length, and the fluid is allowed to relax. Each experiment lasts
approximately five minutes, most of which is spent waiting for the
fluid column to drain to the end plates and break in the middle. See
Figure 2 – SHERE Rheometer
Afterwards, the translation slider is repositioned to the starting
position, and the fluid column is recombined. If it is reusable due
to criteria based on temperature, bubble contamination, and previous
strain encountered, then another test can be performed with the same
fluid module. Otherwise, it is removed, and the next one is installed
for the next test.
Measurements
During each experiment, a smooth, bubble-free cylindrical liquid bridge
is generated between two flat endplates. The liquid bridge will initially
be 5 mm long and 10 mm in diameter. A rotational shear rate will be
imposed on the fluid by rotating one endplate from 0 to 500 rpm for
a predetermined time while holding the other endplate stationary.
As soon as the rotation has stopped, an elongational deformation will
be imposed by axially translating one of the endplates in an exponential
manner in order to generate constant strain rates from 0.1 to 5.0
s-1. The tensile force and filament shape will be monitored during
the elongation, and the elongation will stop at a length of approximately
194 mm. The position of the moving plate is recorded to verify the
imposed velocity profile. By backlighting the test fluid with an electroluminescent
panel and viewing the fluid column from above with a video camera,
half of the fluid column’s shape can be recorded for use in
later analyses and simulations. Additionally, the fluid diameter is
recorded via a laser micrometer at the column’s midpoint. Fluid
and air temperatures are digitally recorded from thermistors. Once
the elongated bridge has been allowed to stabilize, the experiment
will monitor subsequent evolution of the midpoint radius, filament
shape, and tensile force in the column. Eventually, the filament necks
down and breaks under the combined action of elastic and viscous capillary
stresses. From measurements of force and radius during the stretch
and relaxation of the fluid, we can compute the extensional viscosity
as a function of strain rate and a function of the amount of preshearing. |
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Figure 1.
SHERE Flight Hardware |
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Figure 2.
SHERE Rheometer |
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