Algor Software Used on International Space Station
Project
FEA Software Utilized in Training
Module and Flight Hardware Designs
The International Space Station (ISS) is the largest scientific
cooperative program in history, drawing on the resources and expertise
of 16 countries. Using Algor software, Bergaila Engineering Services
in Houston, Texas, working with Johnson Engineering Corporation
under NASA’s Mentor Prot間?program, is designing and analyzing
components both for the space station and its testing module.
Construction of many of the space station’s components is already
under way. ISS assembly in orbit is scheduled to begin in June
1998* and continue for five years. The ISS will
serve to foster advances in science and technology and produce
direct and indirect economic benefits worth twice the cost of
investment. In addition, the program will forge international
partnerships and inspire the next generation of scientists, engineers
and entrepreneurs.

Computer-generated drawing of the International Space
Station, a cooperative scientific program supported by 16 countries
to further scientific and technological research in space. The
inset shows a close-up of the 7-A airlock. A replica of this component
was designed for training purposes using mechanical engineering
software from Algor, Inc. Digital artist's concept courtesy
of NASA.
Neutral Buoyancy Lab Training Module
Components

The 7-A airlock of the Neutral Buoyancy Laboratory training
module will be used by space station trainees to exit the module
for underwater exercises. An analysis was performed to determine
the best placement of lift points for hoisting the airlock in
and out of water. Based on the initial analysis results (shown
left), the lift points were moved to decrease high stress levels
and associated deflection in the final design (shown right). Models
courtesy of Bergaila Engineering Services.
In January 1999*, an international crew of three will begin
living aboard the ISS. When complete, the station will provide
living space for up to seven astronauts and scientists. To train
these people for maneuvers in space, a module is being constructed
for the Neutral Buoyancy Laboratory in Clear Lake, Texas.
The Neutral Buoyancy Lab is a large pool 102 feet wide, 202 feet
long and 40 feet deep. Modules are lifted into the pool, and astronauts
practice maneuvers which will take place outside the space station.
These drills, which may include attaching hoses and installing
and removing fuel tanks, are used both to train the astronauts
and to aid in logistical planning.
The training module replicates the dimensional and functional
parameters of the ISS; however, adaptations need to be made to
account for its underwater use. The module components must be
strong enough to withstand the stress of support systems both
in and out of the pool, the lifting system and buoyancy. In addition,
stainless steel is used for the training components rather than
the aluminum alloys employed in the space station.
Mark Gray, an engineer at Bergaila Engineering Services, worked
on several components for the training module including the 7-A
airlock, from which trainees emerge into the water. Mr. Gray and
fellow Bergaila engineer Kim Wong built a 37,000 plate/shell element
model of the airlock based on the ISS design using Algor's precision
finite element model-building tool, Superdraw III.
“The latest version of Algor's Superdraw III has made the process
of building models faster and easier,” remarked Mr. Gray. A stress
analysis was executed to determine whether the airlock would endure
use in the Neutral Buoyancy Laboratory.
Mr. Gray appreciates how Algor’s graphical and engineering capabilities
complement each other. “The capabilities that enable me to realistically
model systems and see how structures react and interact have reduced
the need to make assumptions and design unnecessarily conservatively,”
said Mr. Gray.
Based on analysis results, engineers at Bergaila Engineering
Services and Johnson Engineering determined that the lift configuration
used to move the module in and out of the pool should be changed
to lower stress levels and associated deflection. In addition,
engineers agreed that many of the space station's bolted connections
could be welded for the stainless steel training module.
Mechanical fastening methods, such as bolting, are favored for
space station flight hardware because the aluminum alloys used
weaken when welded. Since stainless steel is used in the training
module, welding was a better joining option.
These final modifications were made to Mr. Gray’s model in January
1998. The training module’s construction will be complete by June
1998*, when training will begin.
Flight Hardware for the International
Space Station

Ross Bozeman designed this stowage platform, which will be installed
in the ISS. This stress contour simulates a 500 lb. payload with
translational and rotational acceleration loads in the X, Y and
Z directions.
Ross Bozeman, engineering manager at Bergaila Engineering Services,
used Algor to design and analyze a flight hardware component for
the space station. The aluminum re-supply stowage platform (RSP)
needed to weigh less than 150 lb. and be able to support up to
500 lb. of equipment. In addition, the structure’s natural frequencies
had to fall within a defined window.
Mr. Bozeman designed a combined beam and plate/shell model of
the RSP in Superdraw III according to NASA’s specifications.
“The updates to Superdraw III over the past year strike me as
very intuitive, especially to new users,” said Mr. Bozeman.
For each design, Mr. Bozeman conducted a series of 20 linear
stress and vibration analyses. He was able to automate the process
using batch files. Dozens of design variations were analyzed to
determine the best 3 or 4 designs. For those few designs, Mr.
Bozeman used Merlin Meshing Technology and Supergen to refine
the mesh of the models before running a series of final analyses.
In addition, he conducted linear dynamic response analyses on
other existing flight hardware components. The results of these
analyses help engineers at Johnson Engineering to determine the
net effects of launch- and crew-induced vibrations.
“The graphical representation of results in Algor has always
been superior,” said Mr. Bozeman. “The wide variety of display
types Algor offers has always impressed me.”
* Editor's Note: The ISS
construction and assembly schedule is subject to change. Check
NASA's web site (www.nasa.gov) for more
information.
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