On-site personnel:
The AGO team consisted of Kevin Killilea (Field personnel/Groomer)
and Tom Barfield and Joe Kujawski (AGO technical service team).
Station:
The station was cold upon arrival. The AGO lost function due
to a blockage on the air exhaust. Part of the failure caused
ice formation in the exhaust manifold.
The technical service team successfully started the thermo-electric generator and raised the station temperature to 17-22 C. That temperature was maintained throughout the service call.
The CAGOSYS upgrade was completed. Additionally, a 100 lb propane cylinder located outside the AGO shelter was plumbed for cooking. The 100 gallon cylinder that was isolated last year (because it was leaking) was relocated to the auxilary tank position.
AGO-1 was not targeted to be raised this year and will not need to be
raised for several years.
TEG:
The TEG was upgraded to add a forced combustion air delivery system,
called the Turbo, and to make it compatible with the new station
configuration. Additional noise suppresion (capacitors and
inductors) were added to the Turbo electronics to reduce EMI to an
acceptable level.
Batteries for the electronic shutoff valve were changed. Manifold
propane pressure was set to 3.5 psi. The maximum burner temperatures
that could be achieved are:
#1: 210 C, #2: 240 C, #3: 220 C, #4:
230 C, #5: 240 C, #6: 230 C.
Data Control Unit (DCU):
CAGODCU Rev. 1 was installed. Also installed were two Storage
computers (Rev 2, SN: 004 and 019).
The optical disks containing data gathered during the past year were retreived and will be sent to Augsburg for processing.
Power Supply Controller (PSC):
CAGOPSC Rev. 2 was installed without any problems.
See AGO1.AGO for experiment power settings, priorities, and other station
information.
Data Acquisition Unit (DAU):
All functions were normal when the unit was turned on.
Non-volatile random access memory was replaced.
The DAU was upgraded per CAGODAUM Rev 0. See AGO1.AGO for DAU
settings.
Global Positioning System Receiver (GPS):
The GPS was functional when the AGO electronics were turned on.
Bell Labs Fluxgate Magnetometer:
Data was examined to verify the operation and leveling of the magnetometer.
By examining this data, the service team determined that there was no need
to change the magnetometer settings.
Settings for the magnetometer are:
Sensitivity : 1000 nT
H Offset : +
00 07 220
D Offset : OFF 00 00 000
Z Offset : -
02 08 940
The electronics were checked out per the servicing documentation. The results of the checkout were as follows:
Axis Meter Out
DAU Save File
Reading
Reading Name
H: -10.000 V
015 H P199_FLH.GIF
+10.000 V
FEC H
D: -10.000 V
004 H P199_FLD.GIF
+10.000 V
FE9 H
Z: -10.000 V
00C H P199_FLZ.GIF
+10.000 V*
FFA H
* Scale adjusted to 10^3
The secondary ground on the experiment was connected to chassis.
Tohuku ULF Search Coil:
Tohuku was upgraded per CAGOULFM. Sample data was recorded to
disk.
Stanford VLF Receiver:
The Stanford experiment was not calibrated since the calibrator went
to AGO-3. Data was collected and examined for possible problems.
Settings for the experiment are as follows:
8-16 KHz 20
16-32 KHz 20
0.5 - 1KHz 20
4-8 KHz
20
24.0 KHz NAA RF-20 IF-15
1-2 KHz NS 10
2-4 KHz
10
30-40 KHz 10
1-2 KHz EW 10
Line Receiver NS 30
Line Receiver EW 35
University of Maryland Riometer:
The signal attenuators provided by the University of Maryland were
installed. After installation, data was observed and found
to be very noisy in both channels. The service team could do
nothing to improve the noise and left the attenuators in place.
See P199_RI1.GIF and P199_RI2.GIFfor
collected data.
Anubis Seismic:
Both seismometers were tested and one was found to be non-functional.
The working seismometer was installed in a vault upwind of the station.
After the
vault was dug and the seismometer was installed it was discovered that
both of the Reftek units were non-functional. The service team tried
to make a functional unit from the non-functional ones by trading
PC boards between the units. Unltimately, the RefTek could
not be made to work.
The vault electronics were left at the site and both RefTeks were retro'ed.
Power to the experiment was turned OFF.
Dartmouth LF/HF Receiver:
Data was collected and examined on the Dartmouth experiment.
Sample data can be seen in P199_LFH.GIF.
Allsky Camera:
The battery was replaced. The allsky camera was upgraded to CAGOALLM
Rev. 1. The calibration flashlight was used to collect sample data.
One image is present in P199_ALL.GIF
Due to the late arrival of the calibration flashlight, the service
team did not find out that the batteries for the instrument were not
included until AFTER the team arrived at the AGO. The team had to
use two very old 'D' cell batteries found at the site and two new batteries
which had been brought for other purposes.
NASA LIDAR:
The service team had planned to remove the Lidar from the site this
year. However, neither the shipping containers nor the instructions
for removal had made it to McMurdo in time for the service visit.
As a result, the insturment was disconnected and kept at the AGO site.
Miscellaneous:
GPS position: S 83 52' E 129 37'. Elevation: 2813
m.
Notes for the future:
1) Experimenters that provide cable for outside use should provide cables
that are cold-friendly and are flexible at -40 C.
2) Experiments that provide junction boxes and connection points outside
the AGO should allow for the fact that these connections will be made by
people
with gloves and should have adequate spacing between the
connectors.