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UPDATE # 33 - January 10, 1998

PART 1: Get involved in Space Team Online
PART 2: Chemistry helps improve KSC's environment
PART 3: Measuring one tenth of one billionth of one degree
PART 4: Status of Columbia's processing
PART 5: Subscribing/unsubscribing: how to do it


GET INVOLVED IN SPACE TEAM ONLINE

Happy New Year from Space Team Online!

If you are a teacher and haven't yet gotten your students involved
in Space Team Online projects, we hope this is the year you will
start. Below are two activities that won't require too much
planning or time.

First, consider joining a web chat. For one hour, NASA experts are
available to talk about their jobs and how they wound up working for
NASA. A different person joins us almost every week. Please visit this
page for details: http://quest.arc.nasa.gov/space/events/interact.html

This Wednesday at 10AM Pacific, Tracy Gill will be in the chat room.
Tracy works to prepare experiments to fly on the shuttle. He has
provided a biography and a bunch of Field Journals and now will be
your chance to ask him questions. For more about Tracy, please read
his biography at http://quest.arc.nasa.gov/space/team/gill.html

* * * * * * * * * * * * * * * * * * * * * * * * *

Another activity is called Student Stumper will work on the
communication skills of students while challenging them to
think creatively.

The basic idea is this: kids make riddles for other kids to solve.
Students will create a question about the shuttle or space station
that they think will be difficult but fun to answer. Pose that question
(we'll put it online in the Kids' Corner of the Web), and others will 
email their responses directly back. The question creator gets to decide
if the respondent is right. Then, we'd love to see the results if you'd
like to share.

An example question might be: What are some reasons that the Shuttle's
external tank is ejected and not carried for the entire mission.

That question isn't too tough; we know you can do better than that!

We expect the result to be a bunch of kid-kid email exchanges which
heat up the Internet. Send your original Student Stumpers to Oran at
oran@quest.arc.nasa.gov. Also, visit the web at
http://quest.arc.nasa.gov/space/kids/stumpers.html


[Editor's note: Dale is a chemist at the Kennedy Space Center. His group manages over thirty projects involving ground support for the shuttle, space station and expendable vehicle processing and preparation for launch.]

CHEMISTRY HELPS IMPROVE KSC'S ENVIRONMENT

Dale Lueck
http://quest.arc.nasa.gov/space/team/lueck.html

January 8, 1998
It has been a long journey, but we have arrived at phase
five of the Nitrogen Oxide (NOx) Scrubber to Fertilizer
project. This project has been a three-year team effort to
find a way to minimize the Nitrogen Oxide emissions that
occur when refueling the space shuttle and Titan rockets. It
is interesting to note that the Titan rocket carries a much
larger fuel load than the space shuttle!

Here is how it works: during refueling operations, it is normal
that nitrogen oxide fumes are produced, because the oxidizer
(which is called nitrogen tetroxide) is near it's boiling point at
room temperature. As the fuel tanks are cooled, more fumes are
emitted. The oxidizer fumes (nitrogen oxide) must be contained
and filtered so that they don't enter the atmosphere. Filtering
these fumes is called scrubbing. The oxidizer scrubber is the
equipment that is used to do this. In the current scrubber, as
the nitrogen oxide is contained and scrubbed, sodium nitrate
and nitric oxide are produced. These are called the liquor. We
discovered that using hydrogen peroxide instead of sodium
hydroxide in the scrubber produced a byproduct of potassium
nitrate - a directly usable fertilizer! To learn more about the
chemical process and how the control mechanism works, go to:
http://technology.ksc.nasa.gov/WWWaccess/Opport/scrubber.html

There are many benefits to this project. The first benefit is
to the environment. The old system produced
approximately 250,000 pounds per year of highly caustic
hazardous waste. Companies had to be contracted to
remove the spent liquor and it had to go through a
neutralization process, both of which are very expensive.
The byproduct of the new scrubbing process is potassium
nitrate. Potassium nitrate is a common fertilizer sold in
garden care stores throughout the world.

The second benefit is that the new scrubber process is
approximately five (5) times more efficient in terms of
scrubbing the NOx emissions.

The third benefit is to the workers safety. Because the
liquor is no longer caustic, the workers can handle the
waste (potassium nitrate) in a much safer manner, using far
less protective gear.

The fourth benefit is cost. This process is cost effective
because companies will no longer have to be contracted for
the removal of the liquor. This saves approximately
$65,000 per year. It also reduces the cost of ground
maintenance for Kennedy Space Center because the
potassium nitrate can be used directly on the grounds at
Kennedy Space Center as fertilizer. This saves
approximately $18,000 per year. Kennedy Space Center
saves a total of $83,000 per year!

How did we get here? The project was broken down into
five phases:

    Phase I - Our research was laboratory tested to prove
    that the concept was valid.

    Phase II - The process was applied to a full-scale
    oxidizer scrubber at the "Oxidizer Storage Farm" at
    launch pad 39A.

    Phase III - This phase redesigned the process control
    system and tested the ability of the scrubber to
    produce potassium nitrate during an operation.

    Phase IV - This phase is the final field testing of the
    equipment. Because of the high concentrations
    involved in the Titan qualification testing, favorable
    wind conditions are required.

    Phase V - This is the installation phase of the project.
    Both the United States Air Force and NASA need the
    phase IV data to decide if the installation costs are
    worth the benefits.

It is the hope of NASA that this application will be used by
industry and will contribute to a safer, less costly and
environmentally friendlier world!


[Editor's note: Stephanie is an experiment integration engineer. She interprets electrical schematics and writes test procedures to test all the experiment power cables to make sure that they were built correctly. In this series, Stephanie is sharing her experience with CHeX, an experiment that flew recently in space. CHeX involves studying Helium at very specific temperatures. Last time, the Shuttle had just taken off and an early problem with CHeX was fixed by turning the experiment off and back on.]

Stephanie Stilson
http://quest.arc.nasa.gov/space/team/stilson.html


MEASURING ONE TENTH OF ONE BILLIONTH OF ONE DEGREE

November 20, 1997 (Flight Day 2)
It is 7:30 p.m. and time for work. During my shift, CHeX
completed the High Resolution Thermometer (HRT)
calibration. A portion of this calibration included
performing Flight Objective-2 (FO-2) which involves
injecting a bubble into the helium to help give more
accurate temperature data. The biggest excitement so far is
that by completing the HRT calibration, we have been able
to achieve the highest resolution temperature measurements
ever attempted in space, one tenth of one billionth of one
degree. This is equivalent to the ability to measure the
distance between Los Angeles and New York to the width
of a single strand of hair!

Calibration efforts are continuing. We are about nine hours
behind schedule due to being too warm when the mission
started. The Payload Experiment Developers (PEDs) assure
me that there was nothing we could have done on the
ground that would have prevented this situation. Being
behind schedule does not pose any impact at this time.

November 21, 1997 (Flight Day 3)
During my off-shift, the team ran into a slight problem.
When one of the valves was commanded open to assist with
the cryostat cooling process, there didn't seem to be any
change in the rate of temperature drop. The valve open
command was reissued with the hopes that although the
telemetry reported it open on the initial attempt maybe the
mechanical action did not occur. This troubleshooting did
not have any affect. The cryogenics team believes that there
may be some blockage in one of the cooling loops and is
now analyzing data to see if they can figure out exactly
where the blockage is located. This problem will not deter
us from achieving our science goals, but is will increase the
amount of time it takes to get into position to start gathering
this data.

The bigger hurtle for us right now has to do with the
SPARTAN satellite problems. With the plan to grapple
SPARTAN in the near future, JSC is requiring the orbiter
to use the primary thrusters more often than planned
(possibly the remainder of the mission) in order to save
fuel. If these thrusters are fired when CHeX is at the
lambda point, the cryostat heats up and we slip away from
lambda. It would then take us approximately eight hours to
recover and we would not be able to achieve the minimum
science requirements. Negotiations with JSC are currently
underway to come up with a plan that will be acceptable to
both CHeX and SPARTAN. Keep your fingers crossed!

November 22, 1997 (Flight Day 4)
CHeX completed the calibration of the calorimeter heaters
and has begun the general scan in preparation for high
resolution measurements later in the mission.

When the general scans were complete, CHeX began high
resolution data collection. The wide range heat capacity
measurements were successfully performed and included
the first scan above the lambda point. This produced the
first observations of the confinement effect in the helium
sample. A total of nine high resolution sweeps were
completed.

CHeX's achievement of today's science objectives was in
part due to JSC's minimal use of the orbiter's primary
thrusters. We hope that our luck continues.


STATUS OF COLUMBIA PROCESSING

Below, we'll provide some details about the post flight work
being done after STS-87 and the subsequent processing of Columbia
as it prepares to fly again as STS-90. These reports will contain
jargon and unfamiliar terms; our intent is not to confuse you, but to
provide a glimpse at all the steps involved. Detailed daily reports
about Columbia's processing can be found at the NASA Shuttle Status
web site at http://www-pao.ksc.nasa.gov/kscpao/status/status.htm

Since the last updates-sto message, opened Shuttle Columbia's
payload bay doors were opened following an extended down period
during the holidays.

Ku band antenna testing took place and the orbiterUs nose and main
landing gear tires were also installed. The orbiter windows were
polished and post-flight window inspections were completed.

Technicians replaced fuel cells No.1 and No. 3 and functional tests
were begun. Also started were operations to remove the remote
manipulator system robotic arm, functional tests of the orbiter
maneuvering system, and auxiliary power unit leak and functional
checks.

STS-90 SCHEDULED OPERATIONAL MILESTONES (dates are target only):
- Fuel cell voltage tests complete (Jan. 13)





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