AIDJEX Bulletin #40 - Polar Science Center - University of Washington
AIDJEX Bulletin #40 - Polar Science Center - University of Washington
AIDJEX Bulletin #40 - Polar Science Center - University of Washington
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AIR DROPPABLE RAMS (ADRAMS) BUOY<br />
W. P. Brown<br />
<strong>Polar</strong> Research Laboratory, Inc.<br />
123 Santa Barbara Street<br />
Santa Barbara, California 93101<br />
E. C. Kerut<br />
NOAA Data Buoy Office<br />
Mississippi Test Facility<br />
Bay St. Louis, Mississippi 39520<br />
Abstract<br />
The ADRAMS buoy was developed to provide<br />
remote tracking <strong>of</strong> drifting sea ice near the<br />
Arctic coast. The air droppable feature was<br />
employed to reduce the high cost <strong>of</strong> deployment<br />
inherent to manual installation and to provide<br />
access to, deployment areas and seasons <strong>of</strong> the<br />
year not previously suitable. ADRAMS contains<br />
a 401.2 MHz transmitter and suitable digital<br />
encoding to allow it to be received by the<br />
NIMBUS-6 satellite. This satellite contains a<br />
random access measurement system (RAMS) package.<br />
The RAMS system determines the position<br />
<strong>of</strong> the ADRAMS buoys to an accuracy <strong>of</strong> better<br />
than 5 €31 thru doppler measurements <strong>of</strong> the<br />
received signal. The buoy is deployed via its<br />
own parachute and is designed to survive and<br />
properly orient its antenna on any type <strong>of</strong><br />
terrain. The 80 pound package contains enough<br />
batteries for 7 to 8 months operation at surface<br />
temperatures as low as -5OOC. Although<br />
the original ADRAMS was designed for tracking<br />
only, it has been modified to incorporate a<br />
capability for sensor data telemetry. The RAMS<br />
system in the NIMBUS-6 satellite accepts 32 bits<br />
<strong>of</strong> data from each transmission. Nineteen ADRAMS<br />
buoys have been deployed thus far; 17 in the<br />
Arctic and 2 in the Antarctic. The air drops<br />
have been 100% successful.<br />
1. Introduction<br />
The Bureau <strong>of</strong> Land Management, in conjunction<br />
with the Arctic Ice Dynamics Joint Experiment<br />
(<strong>AIDJEX</strong>) program, developed an urgent need for a<br />
device to allow remote tracking <strong>of</strong> the Arctic<br />
ice pack drifting near shore. This need resulted<br />
from the expansion <strong>of</strong> oil activities on the<br />
northern coast <strong>of</strong> Alaska and from problems encountered<br />
during 1975 in attempting to ship<br />
large amounts <strong>of</strong> material to the oil-rich Prudhoe<br />
Bay area.<br />
Because <strong>of</strong> the urgent nature <strong>of</strong> the program,<br />
it was probable that the buoys would have to be<br />
deployed,during the all-dark period <strong>of</strong> winter<br />
in the Arctic and under adverse weather conditions.<br />
Previously-developed Arctic data buoys<br />
(~,2) were not suitable because their installation<br />
required a crew to land on the ice, an<br />
operation too hazardous for the dark <strong>of</strong> winter.<br />
21<br />
Therefore, the concept was evolved for a small<br />
buoy which could be deployed from an aircraft via<br />
parachute. With the constraint <strong>of</strong> small size,<br />
the obvious choke <strong>of</strong> a tracking scheme was the<br />
NIMBUS-6 satellite Random Access Measurement<br />
System (RAMS). This system is being used succese<br />
fully in other buoy programs. The buoy was given<br />
the acronym ADRAMS (Air Droppable RAMS). The<br />
NOAA Data Buoy Office was selected to spearhead<br />
this program because <strong>of</strong> its wide experience in<br />
developing data buoys for the open ocean as well<br />
as the Arctic.<br />
A contractor, <strong>Polar</strong> Research Laboratory, <strong>of</strong><br />
Santa Barbara, California was selected to perform<br />
the ADRAMS design, development, and fabrication.<br />
2. Design Considerations<br />
The following factors provided the major constraints<br />
on the overall system design.<br />
1.<br />
2.<br />
3.<br />
4.<br />
5.<br />
6.<br />
7.<br />
8.<br />
The fabrication <strong>of</strong> the first group <strong>of</strong><br />
buoys had to be complete within six months<br />
<strong>of</strong> the program start to allow deployment<br />
for the critical winter season. This<br />
factor constrained the use <strong>of</strong> electronic<br />
components, materials and energy sources<br />
to those that were readily available.<br />
The size <strong>of</strong> the buoy could not Cxceed the<br />
dimensions <strong>of</strong> the parachute door on available<br />
deployment aircraft.<br />
The electronic subsystems and mechanical<br />
structure had to withstand the landing<br />
impact <strong>of</strong> a parachute landing on smooth<br />
and rough ice.<br />
The parachute had to be disconnected from<br />
the buoy after landing to prevent the buoy<br />
from being dragged across the ice by high<br />
winds.<br />
The rate <strong>of</strong> change <strong>of</strong> oscillator frequency<br />
with temperature had to be minimized, wittr<br />
out using power, to optimize tracking<br />
accuracy.<br />
The system was to have a minimum life <strong>of</strong><br />
six months.<br />
The system was to withstand the<br />
surface temperature extremes <strong>of</strong><br />
-5OOC.<br />
ice pack<br />
t10 to<br />
The buoy hull had to be water t ght in the