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7. DEPARTMENT OF TRANSPORTATION 
Sheth ata es COAST GUARD 
{ COAST GUARD OCEANOGRAPHIC UNIT —- 


Taut-Line Instrumented Arrays\ 
Used by 
the 


Coast Guard Oceanographic Unit | 
During 1970-1971 


\ 


‘Christopher L. Vais Thomas C. Wolford \ 
‘Alan D. Rosebrook Robert Erwin Ettle / 


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| Hee gh OCTOBER 1972 


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U.S. COAST GUARD TECHNICAL REPORT 


The reports in this series are given limited distribution within agencies, 
universities, and institutions engaging in cooperative projects with the U.S. 
Coast Guard. Therefore, citing of this report should be in accordance with 
the accepted bibliographic practice of following the reference with the phrase 
UNPUBLISHED MANUSCRIPT. Reproduction of this report in whole or 
in part is permitted for any purpose of the U.S. government. 


TAUT-LINE INSTRUMENTED ARRAYS USED BY THE 
COAST GUARD OCEANOGRAPHIC UNIT 
DURING 1970-1971 


BY 


Christopher L. Vais 

Alan D. Rosebrook 

Thomas C. Wolford 
Robert E. Ettle 


OCTOBER 1972 


U.S. COAST GUARD OCEANOGRAPHIC UNIT 
Washington, D.C. 


ABSTRACT 


The Coast Guard Oceanographic Unit (CGOU) used taut-line instru- 
mented arrays to investigate the current regime near the Grand Banks of 
Newfoundland. The instrumented arrays used were patterned after a design 
developed and used by Woods Hole Oceanographic Institution. G. B. Shick’s 
Circular Arc Approximation was used to compute the tension in the mooring 
line. The arrays were set and recovered by Coast Guard personnel under 
the supervision of CGOU field parties. 


Editor’s note: Reference to a product or comment with respect to it in 
this publication does not indicate, or permit any person to hold out by re- 
publication in whole, or in part or otherwise, that the product has been 
endorsed, authorized, or approved by the Coast Guard. 


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INTRODUCTION 


Since the early 1960’s, the International Ice 
Patrol Research Section (IIPRS) of the U.S. 
Coast Guard Oceanographic Unit has used taut- 
line instrumented arrays to collect current veloc- 
ity data near the Grand Banks of Newfoundland 
and the Labrador continental shelf. Only the 
1970-71 projects will be discussed in this report. 


The taut-line instrumented arrays used by the 
IIPRS (Figure 1) were patterned after a de- 
sign developed and used successfully by Woods 
Hole Oceanographic Institution (Berteaux, 1968; 
Berteaux and Walden, 1969). The arrays con- 
sisted of a surface float attached to a plaited 
nylon mooring line with current meters attached 
at various positions along its length. The com- 
plete mooring was secured to an anchor with a 
release device (acoustic or time) which freed 
the array from the anchor when triggered. 

The direct current observations collected are 
of interest to the Ice Patrol Research Section: 

© To determine the validity of the geostrophic 

approximation. 

© To collect direct current measurements which 

may be used for boundary conditions in a 
mathematical circulation model of the region. 


® To collect direct current measurements to be 
used in iceberg drift models. 


The 1970 arrays were set off the coast of 
Labrador north of the Strait of Belle Isle in 
positions 54°30’N, 54°32’W and 54°29’N, 54°- 
30’W. Both arrays were recovered successfully 
two weeks after they were set. In 1971, two 
arrays were set on the southeastern edge of the 
Grand Banks at positions 45°02’N, 48°55’W and 
46°40’N, 47°24’W . Two weeks later, one array 
was recovered; the other array was apparently 
struck by a fishing trawl which carried away the 
surface float, allowing the remaining section of the 
array to sink. When the CGC EVERGREEN 
was within about two miles of the location where 
the buoy had been set, the acoustic release device 
responded when interrogated. Extensive drag- 
ging operations failed to recover the release or 
any other part of the array. (Note in proof. 
Two of the current meters and assorted lengths 
of line from the southern array were found by a 
Newfoundland trawler and returned to CGOU 
in February 1973. The acoustic release was not 
recovered. ) 


FIXED BRIDLE 
SLING RING AND SHACKLES 


10 FEET %°" CHAIN 


iO 


FIXED BRIDLE 
SLING RING AND SHACKLES 


10 FEET %°" CHAIN 


@ 
© ——@ 
© (1) 9/16"* NYLON LINE a 

(2) 5/8°* NYLON LINE 

a ) SHACKLE mE 
(4) CURRENT METER a 
(GS) SHACKLES AND SLING RING 
(6) TIME RELEASE ® 


7) ACOUSTIC RELEASE 


ne) 
99 FEET %’’ AND 1%" CHAIN 
STIMSON ANCHOR 
(4000LBS IN AIR) 


FicurE 1. Single point taut-line instrumented arrays used in 1970-71. 


2 


BUOY ARRAY DESIGN 


All of the taut-line arrays set by the IIPRS 
in 1970 and 1971 used surface flotation which was 
on hand at CGOU. The floats used were Geodyne 
Model A-92 toroidal instrument buoys (Figure 
2). A Geodyne Model A-93 tripod tower on 
each buoy supported a pair of wire mesh, life- 
boat radar reflectors and a Geodyne Model 180 
Xenon light. A rigid tripod bridle, Geodyne 
Model B-301, attached to the bottom of the to- 
roid, supported the subsurface portion of the 
array. 


Surface buoy, Geodyne Model A-92. 


FIGURE 2. 


The use of surface flotation introduces major 
problems which can effect the survivability and 
reliability of taut-line arrays. 


® Surface floats are susceptible to collisions 
with ships, fishing trawlers and seiners, ice- 
bergs, and, in some locations, sea ice. 


© Surface floats with radar reflectors and 
lights are highly visible, and are, there- 
fore, subject to well-intentioned recovery or 
theft. 


© The use of surface floats requires a very 
accurate determination of water depth at the 
mooring site. 


If the water depth were not accurately known 
and the array were set in water exceeding the 
design depth, heavy seas, large tidal rises, or 
strong currents could cause the anchor to be lifted 
off the bottom since the reserve buoyancy of the 
surface float exceeded the weight of the anchor. 
If the anchor were carried into deep enough 
water, the entire array would be free to drift and 
could be lost. If however, the array were set in 
too shallow a depth of water, the mooring line 
could go slack and kink, or the current meters 
could be inclined in excess of 15° from the 
vertical by the current, making the readings 
unreliable. 

To determine water depth accurately at the 
mooring site, a Salinity/Temperature/Depth Sys- 
tem (STD) cast was taken and the sound velocity 
was computed at various depths. A weighted 
mean sound velocity, R, was then calculated. 
The depth at the mooring site, as indicated by the 
vessel’s fathometer, was noted. The time (T) 
required for the fathometer signal to reach bot- 
tom and return was determined from the re- 
lationship : 


RT 
Ba (1) 


where: Z=fathometer indicated depth, ft. 


R=4800 ft/sec (sound velocity for 
which the fathometer 
was calibrated ) 


T=time, sec 
A more accurate value of Z was then calculated by 
substituting the values of R and T into equation 


(i), 


Mooring Line Tension Calculations 


In 1971, the taut-line arrays were designed 
to satisfy the following requirements. 


® Mooring line tension must not exceed 15% 
of the breaking strength of the line. 


BUOY 


ur 
1, sin ay = 0, 


Forces at the Buoy 


ANCHOR 


Forces at the Anchor 


Figure 3. Circular Arc Approximation (Berteaux, 1968). 


® The arrays must be able to withstand at ® The maximum current will be 2.48 ft/sec 
least 30 feet of vertical movement to compen- and can be considered constant from sea sur- 
sate for tidal excursions and waves. face to bottom. 


® Current meters should not be allowed to in- 
cline more than 15° from the vertical. 


® Wind drag will be considered negligible. 


© All hardware used should have a safety fac- 
tor of 5:1. 


The total tension on the mooring line was cal- 
culated using the Cireular Are Approximation 
(G. B. Shick, 1964). The shape of the mooring 
line was assumed to be a circular arc (Figure 3). 
The only force considered was the form drag 
on the array. The form drag (F) acting on each 
component of the taut-line array was calculated 
from: 


F=0.5pv?LDC, (2) 
where: F=pressure drag, lbs 
p—density of seawater, slugs/ft* 
v—current velocity, ft/sec 
L=length of component, ft 
D=diameter of component, ft 
Ca=drag coefficient 


The uncertainties in determining the drag force 
arose from our lack of knowledge about the ac- 
tual current profile and the drag coefficient. 


The current velocity was assumed to be con- 
stant from the ocean surface to the bottom. 
This assumption was made to facilitate the cal- 
culation of F and to introduce a “worst case” 
situation. In 1970, a current velocity of 1.68 
ft/sec (0.51 m/sec) was used; in 1971 the value 
was increased to 2.48 ft/sec (0.76 m/sec). 

Selection of the drag coefficient (C,) was based 
on the Reynolds Number (Re) and the shape of 
the component. Reynolds Number, the ratio of 
inertial forces to viscous forces, is defined as: 


Vi t 
evs (3) 


Re=— = 
v B 
where: p=density of fluid, slugs/ft* 

V= velocity of flow, ft/sec 
w=coefficient of viscosity, lb-sec/ft? 
v=kinematic viscosity, ft?/sec 
«= characteristic length, ft 


A value of Re was calculated, using equation 38, 


for each component in the array. Values of Re 
ranged from 3 X 10? to5 10%. The calculated 
value of Re was used as the entering argument 
for determining C, from a graph of Re versus Cy 
(Bretschneider, 1966). The drag coefficient for a 
right circular cylinder ranged from 0.90 to 1.20. 


A Ca equal to 1.80 was used in the final calcula- 
tions for the current meters, release device, and 
the nylon line to allow an extra safety factor and 
to compensate for such factors as strumming of 
the mooring line. Strumming occurs when a 
cylinder is free to vibrate laterally under the 
effect of alternating lift forces generated by vor- 
tex shedding. Strumming increases turbulent 
flow behind the mooring line, resulting in in- 
creased drag. Since no graph of Re vs. Cy was 
available for chain, a Cy equal to 2.0 was selected 
based on a value used by Woods Hole Oceano- 
graphic Institution. 

The equivalent spring constant (IX) was cal- 
culated for each size nylon line considered for 
use in the array. K was calculated from the 
equation : 

K= T.7Ti (4) 
@,X— 1X 
where: K=spring constant, Ibs/ft 
T.&T,=tension, lbs 
e.&e, =percent elongation 
x=unstretched length, ft (x + per- 
cent initial elongation times x 
= water depth) 


The values of T and e were taken from first load- 
ing curves for line similar to that actually used 
in the construction of the arrays (Figure 4). 
The expected working range was between 5% 
and 15% of the average breaking strength of the 
nylon line. In 1971, the values of K calculated 
were 
® 90 lbs/ft for %6 inch line at the shallowest 
water depth (490 ft). 
@ 229 lbs/ft for 5¢ inch line at the shallowest 
water depth (490 ft). 
® 40 lbs/ft for 5% inch and %c inch line at the 
deepest water depth (870 ft). 


The total tension (T) in the mooring line was 
then computed using the Circular Are Approx- 
imation. A value of T was assumed and the 
angles a, and a, were computed: 


D, 

yD (5) 

where a,=surface angle of inclination 
D,=surface buoy drag, lbs 
T=assumed tension, Ibs 


a,=are sin 


and 


a= are sin 


1D? 
7 (6) 


% OF BREAKING STRENGTH 


TENSION (Pounds) 


2400 
PEAK LOAD 2000 
1600 
1200 
Expected 
Working 800 
400 
0 


0 5 10 Ge) Me a 9B 30 


TENSION (Pounds) 
3120 


2600 
5/8 INCH PLAITED NYLON: 


BREAKING STRENGTH 10,400 LBS 


PEAK LOAD 
© 9080 LBS 2080 


Expected 
Working 1040 


0 5 10 15° 20 °2 25 30 
% ELONGATION 


Ficure 4. First loading curve for % and % inch plaited nylon (Berteaux and Walden, 1969). 


6 


where a,=bottom angle of inclination 
D,=total subsurface drag, lbs 
T=assumed tension, lbs 


Next the are radius was computed : 


Zeal 
R= =, (7) 
R=are radius, ft 
Z=water depth, ft 
T=assumed tension, lbs 
D,=total subsurface drag, lbs 


D,=surface buoy drag, lbs 


After solving for R, the are length was 
calculated : 
S=R (a:—a;) (8) 
where S=arc length, ft 
R=are radius, ft 
a,—=bottom angle of inclination 
a,=surface angle of inclination 


Finally a value for T was calculated from: 
T=K(S—Z)+T> (9) 
where K=equivalent spring constant, lbs/ft 
S=arc length, ft 
Z=water depth, ft 
T,= initial tension, lbs 


The calculated value of T and the assumed 
value of T were compared, and if they were not 
in agreement, a new value of T was assumed and 
the calculation was repeated. The iterative proc- 


ess was continued until the assumed and calcu- 
lated values of T agreed within a predetermined 
limit. 

After the maximum tension in the mooring 
had been determined, the minimum underwater 
weight of the anchor was determined using the 
equation : 


W=T.+ (10) 


0.6 


where 0.6=assumed coefficient of friction of 
anchor on a mud bottom 


T,=vertical tension, T (cos a2), lbs 
Tp=horizontal tension, T (sin a,), lbs 
W=anchor weight, lbs 


The anchors used in 1970 were single concrete 
blocks (5400 Ibs) with 10 feet of 34 inch buoy 
chain attached above each block. In 1971, Stim- 
son anchors (4000 lbs) with 55 feet of 34 and 
14% inch chain were used. Portions of the chain 
could be lifted off the bottom when the array 
was subjected to severe storms or excessive tides, 
thereby increasing the length of the array and 
decreasing the maximum tension which would 
have resulted if simple anchors had been used. 
Thus, the possibility of failure of the array is 
decreased. 

A Dietzgen 7410-PA Programmable Calcu- 
lator was used for all computations. The pro- 
grams used are reproduced in Appendixes 1 
and 2. 


CONSTRUCTION AND TESTING 


Plaited nylon line was selected for use in the 
1970-71 arrays because of its great strength and 
elasticity, as well as for its ability to stretch 
and then return to its original length with no 
loss in strength (Figures 5-6). Asa result of its 
elasticity, nylon is able to absorb the large 
amounts of energy present during launching and 
during severe conditions such as storm waves or 
strong currents (Figure 7). Plaited nylon also 
resists twisting and kinking, thus eliminating the 
need for swivels in the mooring line. 

When placed under an initial load, new nylon 
will be permanently elongated by approximately 
10% (Figure 4); thus each section of nylon line 
in an array was cut shorter than its designed 
length. During launching, the new nylon line 
was placed under tension by the falling anchor 
and permanently elongated by approximately 
10%. 

Each piece of nylon line was terminated at 
both ends with a 3 or 4 tuck eye splice whipped 
with nylon line or black plastic tape (nylon 
whipping proved superior to the plastic tape). 
A steel thimble was used in each eye splice to 
prevent the nylon line from chafing. The nylon 
line and eye splices were tested by suspending 
the anchor from one section. 

Hardware items such as shackles and sling 
rings were selected so that the ultimate strength 
of any part was at least five times greater than 
the maximum tension the array was designed 
to withstand. Safety marine shackles, locked 
with cotter pins, were used to join sections to- 
gether. To reduce corrosion, the cotter pins were 
only slightly bent after insertion. 

In 1970, two Geodyne Model 102  photo- 
graphically recording current meters were tested 
by operating them in a darkroom with the pres- 
sure cases removed and a test strip of film in the 
magazine. After it was determined that the 
meters were functioning and sequencing prop- 
erly, the meters were reloaded with film and 
the pressure cases were replaced. 


Two Geodyne Model 850 magnetic tape re- 
cording current meters were also used in 1970. 
Four 850 current meters were used in 1971. A 
characteristic failure of these instruments is for 
the tape to wind around the capstan drive and 
stop the recorder. Each of our recorders was 
carefully tested to insure that the capstan drive 
functioned properly. Then the current meters 
were run in the lab for several days with test 
tapes in the recorders to determine if the tapes 
advanced properly. Magna-See fluid was used 
to insure that data were being recorded on the 
tape. A new piece of test equipment manufac- 
tured by Geodyne enabled the Instrument Sec- 
tion to give each current meter a comprehensive 
checkout before it left the lab in 1971. After 
testing, each meter had a new battery installed. 
Each battery was checked by placing it under a 
100 ohm load and measuring the voltage prior to 
installation. Before each tape cartridge was in- 
stalled, it was erased to clear it of any noise 
which might later interfere with computer proc- 
essing of the recorded data. Several desiccant 
bags were placed into each current meter before 
it was sealed . 

The “O” rings at the top and bottom of the 
case were removed and replaced with properly 
greased new ones before the pressure case was 
placed on the current meter. Care must be taken 
when placing the pressure case on the current 
meter to insure that the “O” rings are not pinched 
or improperly seated, or the meter will flood. 
Placement of the top “O” ring is especially 
critical. Once the pressure case was in place, 
the tie rods were torqued to 10 ft-lbs. The cur- 
rent meters were then pressure tested to 200 
meters by the National Oceanographic Instru- 
mentation Center. In 1970, the current meters 
were tested by suspending them in the Anacostia 
River just below the surface for about 3 hours. 
In 1971, one of the current meters flooded as a 
result of an improperly installed top “O” ring 
which had become pinched between the cap and 


the tube. The electronic components were ex- 
tensively damaged by the water-battery electro- 
lyte mixture and the pressure. After the current 
TIME 


9.0 
years 


1.8 
years 


130 
days 


POLYETHYLENE 
26 


days 


125 
hours 


25 
hours 


5.0 


hours 


1.0 
hours 


min. 


0 10 20 30 


meters passed the pressure test, a final check 
was made by activating the meters and listening 
for sequencing sounds with a stethoscope. 


POLYESTER 


MANILA 


40 50 60 70 


LOAD AS A PERCENT OF ULTIMATE TENSILE STRENGTH 


Figure 5. 


9 


Comparison of rope strength (Written communication from Columbian Rope Company). 


LOAD AS PERCENT OF AVERAGE BREAKING STRENGTH 


50 


40 


MANILA 


30 


20 


DACRON 


10 


10 


15 20 25 


PERCENT ELONGATION 


FIGURE 6. 


Typical elongation in various ropes after first loading to 50% of average breaking strength (Written 


communication from Columbian Rope Company). 


The Model A-393 and 855 Geodyne time re- 
leases used in 1970 were checked for proper opera- 
tion at room temperature in the laboratory on 
CGC EVERGREEN. They were then operated 
in the ship’s reefer to simulate expected water 
temperature (~0.0°C). One of the releases was 
test fired on deck. 

AMF Model 242 acoustic releases were used 
by IITPRS in 1971. Each release was completely 


10 


tested prior to use in accordance with the pro- 
cedures in the operation manual. Before use, 
both acoustic releases were given an air acoustic 
test at CGOU and again on the EVERGREEN 
immediately before deployment. 

The arrays were assembled on the buoy deck 
of EVERGREEN in accordance with a mooring 
order established prior to the cruise. The moor- 
ing order listed each component as it would ap- 


LOAD-PERCENT OF BREAKING STRENGTH 


MANILA 


DACRON 


POLYPROPYLENE 


Wote-line used in these tests was subjected to 
a load of 50% of tensile strength before testing. 


2000 4000 


6000 8000 10,000 


ABSORBING ENERGY OF VARIOUS TYPES OF LINE(FT-LB PER LB OF LINE?) 


FIGURE 7. 


Impact resistance or energy absorption properties of line (Written communication from 


Columbian Rope Company). 


pear in the actual array. A check-off list was 
completed for each instrument in the array to 
insure that it was ready to be set. A single 
inner tube was lashed to each instrument in the 
array to provide flotation while the array was 
being set and recovered. The lines used to secure 


11 


the flotation to the instrument were passed be- 
tween the tie rods and the pressure case to pre- 
vent the inner tube from slipping off as it was 
compressed by water pressure (Figure 8). After 
a final check to make sure that everything was 
assembled properly, the array was neatly laid 


Table 1. Comparison of taut-line array components, 1970 and 1971. 


BUOY #1 BUOY #2 BUOY #4 


54°30'N 54° 29'N 45°02'N 46°40'N 
54°32'W 54°30'W 48°55'W 47°24'W 


712 ft 712 ft 672 £t 
21 July 1970 | 21 July 1970 | 11 May 1971 12 May 1971 
i, Rae SO) A Avatee leno 25 May 1971 


Flotation Geodyne Model A-92 toroidal fiberglass buoy, 4300 lbs net 
Buoy buoyancy 
Tripod Tower Geodyne Model A-93 


Rigid Tripod Geodyne Model B-301 
Bridle 
Buoy Light Geodyne Model 180 Xenon 


Nylon Line Columbian Rope Company P1li-moot Columbian Rope Company Pli-moor 
9/16", breaking strength 5/8", breaking strength 10400 lts 
8000 lbs 

Sling Rings Crosby Laughlin Inc. Crosby Laughlin Inc. 


Pear shaped 5/8" Pear shaped 7/8" 
S.W.L. 4200 lbs S.W.L. 8300 1bs 

Safety Marine 

Shackle 


Position 


1/2" S.W.L. 2900 lbs 


Boston & Lockport Inc. 
5/8" S.W.L. 4400 lbs 
1" S.W.L. 10,000 lbs 


Boston & Lockport Inc. 
5/8" S.W.L.* 4200 lbs 


Geodyne 850 
Magnetic tape 
Recording 


Geodyne 850 
Magnetic tape 
Recording 


Geodyne 850 
Magnetic tape 
Recording 


Geodyne 102 
Photographic 
Recording 


Current Meters 


Releasing Geodyne A-393 | Geodyne 855 AMF 242 AMF 242 
Device Time release Time release Acoustic re- Acoustic release 
lease and and pinger 


pinger 


Chain | 3/4" Buoy 3/4" Buoy 3/4" Buoy 3/4" Buoy 
Proof load Proof load Proof load Proof load 
16000 lbs 16000 lbs 16000 lbs 16000 lbs 
1 1/4" Anchor }| 1 1/4" Anchor 
P.L. 45500 lbs} P.L. 45500 lbs 


Stimson 
4000 lbs 


Stimson 
4000 lbs 


Concrete block 
5400 lbs 


Concrete block 
5400 lbs 


ere 


* Safe Working Load 


12 


Ficure 8. Current meter with inner tube flotation 
eollar attached just prior to launching. 


out and secured on the buoy deck. The current 
meters were turned on, and the safety lanyards 
were removed from the release devices. 

Table 1 is a comparison of the components 
used on the 1970-71 arrays. 


Setting the Array 


Just prior to launching the array, the EVER- 
GREEN conducted a bathymetric survey of the 
mooring site. A suitable site was chosen and 
marked with a reference buoy. The two prime 
factors considered in site selection were water 
depth and a relatively flat bottom contour. The 
reference buoy was identical to the surface float 
used with parachute drogues deployed by IIPRS 


The 


Ficure 9. Surface buoy being swung over the side. 
instruments, line, and anchors are layed out on the 
buoy deck of the USCGC EVERGREEN. 


13 


(Wolford, 1966). They were moored with poly- 
propylene line and anchored with approximately 
50 pounds of chain. 


To set the array, the surface float was swung 
over the side and placed in the water (Figure 
9). Then as the EVERGREEN backed down 
slowly, the line and instruments were payed out 
by hand (Figure 10). A small amount of stern- 


Ficure 10. 


Instrument and line being payed over the 
side as the ship backs down. 


way on the ship kept the mooring line under 
enough tension to prevent kinking while the 
anchor was suspended in the port chain stopper. 
When the EVERGREEN was in position, the 
anchor was released from the chain stopper. 


When the anchor reached the bottom, the acous- 
tic release was interrogated to determine if it 
was still functioning properly. The surface float 
and the reference buoy were watched for about 
three hours to determine if there was any rela- 
tive motion between them which would have in- 
dicated that either the reference marker or the 
array was dragging anchor. During this time, 
the position of the mooring site was determined 
using the best methods available. In 1970, 
LORAN A and C were used, while in 1971 
NAVSAT fixes were also available. 


Recovering the Array 


In 1970, recovery operations had to be sched- 
uled when the time release was set to fire. This 
prevented rescheduling recovery if the weather 
was adverse or other operations (SAR) pre- 
vented being on station when the release fired. 
In 1971, the use of acoustic releases permitted 


Figure 11. Surface float lifted onto the buoy deck. 


recovery of the array when EVERGREEN was 
ready. During interrogation of the acoustic re- 
lease, it was necessary to turn off the ship’s 
fathometer (UQN-4) so that the fathometer 
signal would not be received by the release re- 
ceiver and mask the pinger signal. 

When the EVERGREEN was in position near 
the surface float, the acoustic release was fired, 
thereby freeing the array from the anchor. The 
surface float was then lifted onto the buoy deck 
with the whip, and the chain below the fixed 
bridle was secured in the chain stopper (Figure 
11). The chain below the bridle was then cut 
with an acetylene torch (Figure 12), and the buoy 
was secured on deck. The remaining chain was 
brought aboard with the boom, and the remainder 
of the array was pulled in by hand (Figure 
13). When the entire array was on deck, it was 
disassembled. The current meters were secured, 
and all instruments were rinsed in fresh water 
and stowed. 


14 


Kicure 12. Chain being cut from the rigid bridle. 


Figure 13. Line being pulled in by hand. 


DRAGGING OPERATIONS 


An attempt was made to recover the two cur- 
rent meters and the acoustic release which were 
lost in 1971 and thought to be lying in 108 
fathoms of water in the vicinity of 45°02’N and 
48°56’W. Dragging operations were conducted 
with a rig which consisted of 20 feet of 14 inch 
chain followed by 6 feet of % inch chain. Two 
15 pound heat treated marine grapnels and one 
10 pound galvanized marine grapnel were 
shackled to the chain as shown in Figure 14. 
The 15 pound grapnels are a standard Coast 
Guard supply item, and their performance was 
satisfactory during the dragging operations. The 
10 pound galvanized grapnels were purchased 
from the Atlantic Marine Exchange, Boston, 
Mass. They were too light for the type dragging 
being done and were not considered satisfactory. 
The rig was shackled to a 5 ton Miller D-5 
swivel which was then shackled to the end of 


15 


the STD cable. The STD cable was terminated 
with a Preformed Line Products Company eye 
grip clamped to the cable with three cable 
clamps for additional holding power. <A 38 foot 
length of 7% inch chain trailing the bottom grap- 
nel usually prevented the grapnels from fouling 
the chain when dragging downslope. 

A marker buoy was set and served as a refer- 
ence point for navigation during the operation. 
Dragging runs began by lowering the grapnels 
until they were just off the bottom. EVER- 
GREEN then got underway as more wire was 
let out (approximately 420 meters total). The 
vessel maintained a speed of 1-2 knots on a 
heading that set the ship away from the cable 
and kept it clear of the serews. <A total of 109 
dragging runs was made both parallel and 
perpendicular to the bottom contours; however, 
none of the missing equipment was recovered. 


1/4"" STD cable 


MILLER D-5 swivel 


1/2"’ chain 


151b marine grapnels 


7/8'’ chain 


101b marine grapnels 


Figure 14. Bottom drag rig used for dragging operations on the Grand Banks during June 1971. 


16 


RECOMMENDATIONS 


The following test procedures are recommended 
to minimize damage during pressure tests if a 
current meter should flood. 

® Limit the test to 30 meters instead of 200 

meters. 


© Suspend the test as soon as any pressure 
fluctuations in the test chamber are noted. 


® Have experienced personnel standing by to 
remove and disassemble the meter if there is 
any indication of flooding. 


® Keep the meter upright to prevent additional 
damage from water or battery electrolyte 
shorting energized circuits. 


The use of subsurface flotation is recommended. 
While subsurface flotation is generally more ex- 
pensive, an array using subsurface flotation is 

® As reliable as an array using surface flota- 

tion. 


® Less susceptible to theft or collision. 


® Easier to launch because lighter anchors can 
be used. 


© Not affected by sea level changes due to tides 
or waves, therefore, reducing dynamic 
loading. 


It is recommended that sufficient back-up flo- 
tation be used to insure recovery of any portion 
of the array remaining if part of the array 
should be damaged. Corning 16 inch glass 
spheres, which can be attached anywhere in the 
array, have been used successfully by Woods Hole 
as secondary flotation. Two releases attached in 
parallel would prevent the loss of an array if a 
single release failed to operate. A long tag line 
strong enough to lift the anchor would aid the 
recovery ship if the releases failed and dragging 
operations were required. 


REFERENCES 


Berteaux, H. O. (1968) Introduction to the statics of 
single point moored systems. Woods Hole Oceano- 
graphic Institution Technical Memorandum No. 
11-68, May 1968, (Unpublished manuscript), 52 pp. 

Berteaux, H. O. and R. G. Walden (1969) Analysis and 
experimental evaluation of single point moored buoy 
systems. Woods Hole Oceanographic Institution 
Reference No. 69-39, May 1969, (Unpublished manu- 
script), 79 pp. 

Bretschneider, C. L. (1966) Overwater wind and wind 
forces. In Handbook of Ocean and Underwater En- 


1 


rd 


gineering, J. J. Meyers, C. H. Holm, R. F. McAllister, 
editors. McGraw-Hill, 12.2-12.24. 

Shick, G@ B. (1964) The design of a deep moored oceano- 
graphic station. Buoy Technology Symposium, MTS, 
Washington, D. C., pp. 48-56. 

Wolford, T. C. (1966) Oceanography of the Grand Banks 
region and the Labrador Sea in 1966. U. S. Coast 
Guard Oceanographic Report No. 13, (CG-373-18), 
176 pp. 


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APPENDIX 1 


Program Title: Calculation of Mooring Line Tension 


CODE 
BR PT Step Instruction MIL Remarks 
0 000 Reset 024 
001 il 001 
002 Print x 026 
003 Halt 401 Enter Z, water depth, ft 
004 Print x 026 
005 St 1 440 
006 2 002 
007 Print x 026 
010 Halt 401 Enter D., subsurface drag, Ibs 
O11 Print x 026 
012 St 2 441 
018 3 008 
014 Print x 026 
015 Halt 401 Enter D,, surface buoy drag, lbs 
016 Print x 026 
017 St 3 442 
1 020 4 004 
021 Print x 026 
022 Halt 401 Enter T, assumed tension, Ibs 
023 Print x 026 
024 St 4 443, 
025 
026 
027 
030 
031 Rel 2 461 
082 = 062 
0383 Rel 3 462 
034 = 020 
035 St 6 445 T., initial tension, lbs 
036 o 007 
037 Print x 026 
2 040 Rel 1 460 
041 x 070 
042 Rel 4 463 
043 = 020 
044. = 072 
045 Rel 6 465, 


19 


CODE 


BR PT Step Instruction MIL Remarks 
046 = 020 
047 Print x 026 R, ARC Radius, ft 
050 St 0 457 
051 8 010 
052 Print x 026 
053 Rel 2 461 
054 + 072 
055 Rel 4 463 
056 -= 020 
O57 Sint 042 
3 060 R>O 046 
061 Print x 026 a, degrees 
062 St 5 444 
063 9 O11 
064 Print x 026 
065 Rel 3 462. 
066 = 072 
067 Rel 4 463 
070 = 020 
O71 Sin 042 
072 R-O 046 
073 Print x 026 a,, degrees 
O74. St 4 443 
075 1 OO1 
076 0 000 
O77 Print x 026 
4 100 Rel 5 464 
101 — 062 
102 Rel 4 463 
103 = 020 
104 Print x 026 
105 Sin 040 
106 Sint 042 
107 Print x 026 a.—a,, degrees 
110 ST 5 444 
ILL 1 OO1 
1H 1 OO1 
i118} eranbiex 026 
114 Rel 5 464. 
115 x O70 
116 Rel 0 ATT 
IALG = O20 
5 120 Print x 026 S, ARC Length, ft 
2, = 062 
122 Rel 1 460 
123 = 020 
124 Print x 026 S—Z, ft 


20 


CODE 


BR PT Step Instruction MIL Remarks 
125 ST 2 441 
126 5 005 
127 Print x 026 
130 Halt 401 Enter K, spring constant, lbs/ft 
131 Print x 026 
1382 ST 5 444 
133 6 006 
134 Print x 026 
135 y etalt 401 Enter T,, initial tension, lbs 
136 Print x 026 
137 ST 6 445 

6 140 1 001 
141 2 002 
142 Print x 026 
143 Rel 2 461 
144 x 070 
145 Rel 5 464 
146 = 020 
147 aP 060 
150 Rel 6 465 
151 = 020, 
152 Print x 026 'T, calculated tension, lbs 
153 To (0) 740 


Nore: This program was designed for use on a Dietzgen 7410-PA Programmable 
Calculator. 


21 


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APPENDIX 2 


Program Title: Normal Drag on Mooring 


CODE 
BR PT Step Instruction MIL Remarks 
0 000 Reset 024 
001 1 001 
002 Print x 026 
003 Halt 401 Enter V, velocity, ft/sec 
004 Print x 026 
005 ax O74: 
006 2 002 
007 = 020 
010 Sut i 440 V? 
011 2, 002 
012 Print x 026 
013 Halt 401 Enter Ca, drag coefficient 
014 Print x 026 
015 ST 2 441 
016 
017 Halt 401 
1 020 3 0038 
021 PE 026 
022 Halt 401 Enter d, diameter, ft 
023 Print x 026 
024 ST 3 449 
025 4 004 
026 Print x 026 
027 Halt 401 Enter :, length, ft 
030 Print x 026 
O31 ST 4 443 
0382 5 005 
033 Print x 026 
034 
035 
036 
037 
2 040 Rel 1 460 
041 x 070 
042 Rel 2 461 
043 x O70 
044 Rel 3 462 


23 


BR PT 


Step 


Instruction 


045 
046 
047 
050 
O51 
052 
053 
054 
055 
056 
057 


Rel 4 


Print x 
Halt 

SFS ON 
SKFS 
JMP to 00 
JMP to 16 


CODE 
MIL 


070 
463 
020 
026 
401 
523 
540 
600 
616 


Remarks 


F, drag force, lbs 


060 
061 
062 
063 
064 
065 
066 
067 
070 
071 
072 
073 
O74. 
075 
076 
O77 


Note: This program was designed for use on a Dietzgen 7410-PA Programmable 


Calculator. 


24. 


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