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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

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