l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican...

59
•.: ' ,, ' . {t "',., lo 1, .. ? '" .... ),. ·'··".;. , , I NA'JAI.. OCEANOGRAPHIC OFfiCt: REFERENCE PUBUCATION 2'i 1978 Approved for P'·'b.lic distribution unlimited. DEPARTM!r.NT OF THE NAVY NS'!L STATION BAY ST. 39522 ,. .. t ' E

Transcript of l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican...

Page 1: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

•.: ' ,,

' . {t

"',.,

~~ lo 1, i.~ ~:\'"' .. ?

~ '" .... ),. ~ ·'··".;.

, , I

NA'JAI.. OCEANOGRAPHIC OFfiCt: REFERENCE PUBUCATION 2'i

l3~EC[IROIN6 MALFUNCTION~~

s~UGUST 1978

Approved for P'·'b.lic reltfO$~>; distribution unlimited.

DEPARTM!r.NT OF THE NAVY

NS'!L STATION

BAY ST. LOUI~,MS. 39522 ,. ~~ r~~

.. t '

E

Page 2: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

ABSTRACT

:)·1 u:n '~X'3T system is a re11ab1e method of measuring temperatures ' r

:, .P~ ,,,,. .,-,,v hundred meters of the ocean while underway. The system !

( .

i"'D? ti Jn on 1 ocal temperature distribution and sonic conditions

·· ,e 1t;vy in tactical decision making.

r··:~r'·:' hr<· been p:repared to aid the system operator in discerning

~ta. It describes erroneous SXBT traces and simple

.. ::; ~· " , )y;::d for rr~ct'ifying the more comnon problE:ms which may

t.,,;::sT AVAILABLE COPY

Page 3: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

/4) NOO..RP-21

GUIDE TO £OMMONHIPBOA RDEXPENDA BL E BA TH YTHERMOGRA PH (SXB T)

RECORDING MA L FUNCTIONS

/I Stephen M.A(ronerBarry P./Blumenthal

//: AUG 078 ,.- /

Approved for public release; distribution unlimited.

NAVAL OCEANOGRAPHIC OFFICE

NSTL STATION

BAY ST. LOUIS, MS. 39522 , . I

Page 4: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

FOREWORD

Accurate and synoptic shipboard expendable bathythermograph(SXBT) data are necessary as input to environmental/acoustic pre-dictions which are provided to fleet units. Since tactical decisionsare based on these predictions, erroneous SXBT data may result inmisleading acoustic predictions.

This report will aid the system operator in discerning gooddata from bad data. It describes erroneous SXBT data and simplemethods to be employed for rectifying defective SXBT recordingequipment.

i .McDONNELLCiTIN, USN

COMMlANDER

Accession ForNTIS GRA&IDTIC TABUnannounced ElJustification

ByDistribution/Availability Codes

Avail and/orDist Special

M7 -z

- ..----- -*-.--A---

Page 5: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

ACKNOWLEDGEMENTS

The authors would like to thank the Sippican Corporation for

assistance in identifying probable causes of SXBT system recording

malfunctions presented in this publication. We also wish to thank

Mr. Alfred Lewando for his many helpful suggestions and Messrs.

Robert Cheney and Alvan Fisher who critically reviewed the manuscript.

Kay Collins and Jo Ann Lyons provided secretarial assistance.

II

Page 6: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

ICONTENTS

Page

INTRODUCTION ........ .. ........................... 1SYSTEM DESCRIPTION ........ .. ........................ 1OPERATION PROCEDURES ......... ....................... 3SXBT SYSTEM ERRORS ........ .. ....................... 6

Category 1 - Check mode calibration mark other than 16.70 C (620F). 8Category 2 - Recorder gain set incorrectly ............ .I.I.. 11Category 3 - Noise> 0 .20C (o.40F)............. . .... 14Category 4 - Wire break ...... ..................... ... 18Category 5 - Insulation penetration ...... ................ 21Category 6 - Wire stretch. ... ..................... 25Category 7 - Improper ground or leakage at launcher. ........ 29Category 8 - Doubtful features ....... .................. 32Probe hits bottom ...... ......................... ... 35Frontal regions ...... .......................... .... 38REFERENCES ................................. 41APPENDIX A - RECORDER CALIBRATION PROCEDURES. ........... 42APPENDIX B - GAIN AND OVERSHOOT ADJUSTMENT .............. .... 45

FIGURES

Figure I - Expendable bathythermograph system ..... ........... 2Figure 2 - Calibration check trace.... 4Figure 3 - Check mode calibration mark other than'16.7°C ..... 9Figure 4 - Check mode calibration mark other than 16.70 C ..... .... 10Figure 5 - Recorder gain set incorrectly - stylus slew response

slow ...... .......................... .... 12Figure 6 - Recorder gain set too high ................ 13Figure 7 - Noise greater than 0.20C external interference ..... 15Figure 8 - Electrical noise. . .................... 16Figure 9 - Servo potentiometer "flat" spot at 16.7C....... . 17Figure 10 - Fouling followed by wire break at launcher ... ...... 19Figure 11 - Wire break from probe spool. . .............. 20Figure 12 - Wire insulation penetration with attempt at recovery. 22Figure 13 - Wire insulation penetration followed by continuous

leakage ..... .. .. ....................... 23Figure 14 - Wire leakage ........ ..................... 24Figure 15 - Wire stretch ... ..................... 26Figure 16 - Wire stretch in mixed layer .............. 27Figure 17 - Wire stretch at bottom of trace resulting in false

temperature increase .... ................. .... 28

1..v

OMU PAGE E.AMa-h~r FIjjMW

Page 7: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

CONTENTS (CONT.)

Page

Figure 18 - Improper launcher ground - erratic excursions tohigh tenperature end ...... ................ 30

Figure 19 - Launcher leakage ....................... 31Figure 20 - Doubtful feature within the mixed layer. . . 33Figure 21 - Doubtful feature within the permanent thermocine 34Figure 22 - Shallow drop - bottom spike followed by isothermal

reading as probe lies on bottom...... . .... 36Figure 23 - Shallow drop - bottom spike followed by wire

leakage. .................... 37Figure 24 - Frontal region with real 7°C temperature inversion * 39Figure 25 - Frontal region with real 30C temperature inversion . 40Figure A-1 - Recorder subassemblies, right side .... ......... 44Figure B-1 - Reccrder subassemblies, rear view .......... .... 46

TABLE

Table I - SXBT Recording Malfunctions ...... .............. 7

vi

Page 8: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

INTRODUCTION

The U. S. Navy uses the Sippican shipboard expendable bathythermograph

(SXBT) system on board its vessels to collect temperature profiles while

underway. Accurate SXBT data are required to prepare effective environmental/

acoustic predictions for fleet units which rely on these predictions for

sensor placement and tactical decisions. Accurate data are also necessary

for mapping thermal variability of' the oceans and for building and maintain-

ing scientifically accurate historical data files.

This publication is designed to assist the SXBT operator in collecting

acceptable SXBT data; it is not an exhaustive study of the SXBT system itself.

Recording problems are documented to demonstrate common system malfunctions

and the adjustment procedures required to correct the system.

SYSTEM DESCRIPTION

The SXBT system consists of a shipboard recorder, a launcher, and an

expendable probe (figure 1). The recorder has a completely automatic cycle

initiated by loading the launcher with an SXBT probe. Closing of the launcher

breech completes a circuit between the probe and recorder, triggering the

recorder into the Check/Run Mode. The calibration temperature (16.70C/62°F)

is recorded on the recorder chart paper for approximately 2 seconds after

which the recorder is in Launch Mode (green light illuminates on the lower

left front of the recorder).

When the probe is launched and contacts the water, the Measure Mode

begins and the chart drive operates for 88 seconds for T-4 probes or 178

seconds for T-7 probes. A continuous trace of temperature versus depth is

-'4 ',', i . i , ' . . .. ..

Page 9: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Canister Loading Breech

G d Canister Wire Spool

Launcher/ Record-er Cable (4-wire

shielded) LAUNCHER

AdjustableAC Power Cable Stanchion,(3-wire)

Optional]Equipment

Depth/TJemp.

Terminal VChartBoardfKH

* GroundStrap Connection

RECORDER

Wire

Spool

i. Thermistor -4"

Figure I - Expendable bathythermograph PROBE (9T)system (after Sippican, 1974)

2

Page 10: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

recorded on the chart until the probe wire is exhausted. The cycle is now

complete with the recorder in Reload Mode (red light illuminates on the lower

right front of the recorder).

The probe, containing the thermistor, functions by a dual-spooling

technique. Wire is unreeled from the probe as it drops vertically through

the water column; simultaneously, wire is unreeled from a canister in the

launcher aboard ship. Changes in electrical resistance of the thermistor

due to temperature changes in the water are transmitted to the recorder.

The probe descends at a known rate while the recorder chart drive

advances at a constant speed. In order to compensate for the probe's

decrease in speed as it loses weight (wire), the vertical divisions of the

chart paper are expanded towards the bottom of the chart. Hence, depth can

be read directly from the vertical axis of the chart.

Overall system accuracy is +0.20C (+O.40 F) for temperature and the

greater of 2 percent or 4.6 m (15 ft) for depth. Temperature measurement

error is due to servometer response in the recorder, accuracy of the chart

paper, and to a lesser degree to uncertainties in thermistor calibration

and wire resistance balance. Depth error is due to launch conditions

(launcher distance from sea surface and wave height) and the descent rate

of the probe (Dugan and Schuetz, 1977).

OPERATION PROCEDURES

Before launching the initial probe, the system should be calibrated

according to the procedures outlined in appendixes A and B. Calibration

should be checked daily, whenever the chart roll is renewed, or after

3

-- -- ,>.-

Page 11: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

C, 25 4C,0f-20

Ir -pU ISE--

TIM-1)A/MO//Y

-. -t.1 + ~*3*~CRUSEr.- NO.

CALIBRATION MARK( AT 67

- -~ 0 C I DEP rH (METEP5)A

Figure 2-Calibration check trace

Page 12: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

minor repairs. The calibration trace shown in figure 2 indicates the -

correct high (34.40C/940F) and low (-l.lOCI3OoF) values and the central

check mark at 16.70C (620F).

The recorder's chart alignment (depth axis) should also be checked;

the stylus should be positioned at the "SURFACE" line. Should the stylus

overshoot this line, advance the roll to the next chart. Never reverse

the chart drive.

During operation, the chart roll may tend to either slip or pull out

of the drive sprocket teeth. In such cases, the plastic chart spool ends

should be checked to assure that they are properly fitted into both the

feed and rewind rolls. If the condition persists, determine the direction

of misalignment in relation to the drive sprocket and adjust the set screws

on the spool ends either in or out to properly align the chart roll. Should

a malfunction occur during operation, adjustments can be made prior to

launch of the next probe. However, the expended canister should not be

replaced until shortly before the next drop to protect the launcher contact

pins from corrosion.

Specific information, including platform name, cruise number, position,

time (GMT), date, consecutive observation number, surface reference tempera-

ture, and bottom depth, must be recorded on each trace and in appropriate

SXBT logs. Calibration tests must also be dated and timed to assure that,

if separated, all traces can later be placed in chronological order by the

processing agency for a final data quality check.

5

Page 13: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

SXBT SYSTEM ERRORS

Table 1 lists the most commnon errors that occur in recording SXBT

data. Each error category contains 1) sample SXBT traces, 2) probable

cause(s) of the error, and 3) a possible method for correction prior to

the next launch. In addition to traces representative of each error

category, examples are given of SXBTs taken in shallow water and within

oceanic frontal regions.

Obvious malfunctions (wire leaks or breaks, launcher leakage,

recorder problems) normally occur in less than 10 percent of launches.

However, improper handling of the SXBT probe before launch can lead to

a greater number of failures than normal because of wire insulation

damage or tangled wire. These failures can be reduced by storing the

probes away from extremes of temperature and humidity. Probes should

always be maintained in a vertical position with the protective cap down.

While collecting SXBT data, the observer should be aware of expected

thermal characteristics of the local operating area. If anomalous features

are encountered, the observer should question the validity of the trace(s)

and, when in doubt, should be encouraged to launch another probe.

6

Page 14: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

TABLE 1SXBT RECORDING MALFUNCTIONS

CATEGORY MALFUNCTION PROBABLE CAUSE(S) FIGURES

1 Check mode calibration mark Improper calibration; de- 3,4other than 16.7 0C (620F) fective servo potentiometer

or printed circuit board

2 Recorder gain set Gain control out of adjust- 5,6incorrectly ment; faulty electrical

connection at launcher

3 Noise > 0.20C (0.40F) Mechanical/electrical 7,8,9interference; defectiveservo potentiomieter

4 Wire break Fouling 10,11

5 Insulation penetration Fouling; wire damage 12,13,14and leakage

6 Wire stretch Unreeling problems; tangled 15,16,17spool

7 Improper ground or Faulty launcher/ground/ 18,19leakage at launcher canister contacts

8 Doubtful features 20,21

7

Page 15: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 1 - Check mode calibration mark other than 16.70C (620F): The

calibration marks on figures 3 and 4 are not within specifications. These

probes should not have been launched. The system is out of calibration and

should be adjusted according to procedures described in appendix A. When

the recorder is calibrated to within + 0.10C at -1.10C and 34.40C (+ 0.20F

at 30OF and 940F), a temperature mark other than 16.70C (620F) during the

Check/Run Mode indicates a defective servo potentiometer or printed circuit

board.

Figures 3 and 4 show a temperature other than the 16.70C calibration

mark; therefore, they cannot be used for accurate thermal analyses nor used

as input to historical data files. However, significant acoustical

parameters such as general temperature structure, layer depth, and in-layer

and below-layer gradients can be determined from such traces.

8

- - W T, -a-

Page 16: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

i l i

X4 II

i t i

Zb~ I T R(ClDPHMTR)

0

o 177

50

0-5-50 - -5--- -- 400

Page 17: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I i

, TEMPEr" U E (0 CDEPTH (VETERS)...... -- -SURFACE' --S. .... - .. .. .....

f~I I

- -. . ... c ,

0 .. - .. .. . ... .. I g

-

5 .. -- 1_ 5 -- 20 5- .- 3.. 0- 0

_- .I '

- f ---i.. .W---. . . .-- - --- 00

S-- - -- I- ...-- - - -.4.00..

.. ..1 J. i _I ... -I -,I

L ... ..

: .. . . .. . .. .. '.- -5 6 o

I.Figure 4 Check mode calibration mark0 other than 16.70C (appears

I , .

o . ., -,at 17.7 0 C)

LOI 1 II' 113

C ~ ii

.. . , :1 -- S - - -- -~---

Page 18: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 2 - Recorder gain set incorrectly: Gain adjustment controls

the stylus slew rate (stylus travel time across the chart) and the amount

of stylus overshoot. With low gain setting, stylus response is slow and

the trace exhibits a temperature lag most noticeable at the surface (figure

5). The trace is erroneous and should not be encoded. Recorder response

to temperature change is slow for the entire trace, and temperature structure

cannot be determined accurately. When gain is set too high, the stylus

vibrates in the Check/Run Mode and overshoot exceeds the maximum allowable

value of 0.50C (l.O°F) (figure 6).

Gain and overshoot adjustment procedures are outlined in appendix B.

If a gain check indicates that no adjustments are necessary, the probable

cause of temperature lag is a faulty electrical connection in either the

launcher cable or canister head contacts.

MEN(11

lib .. . , .. - - .. .. . . _. . - -- - .. i -

Page 19: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

-4T

-4 -7

-u-

-15- 2 -.25 3200

P1 .

W,

0

-. 30

x5

+ dC't --

ja

Page 20: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Iz

im

I I I I f I V I i 1 1 1 1 1 7

(stlu ovrhIt tru ter

V)--- -- ,. . - . - - - - - -- -- .-- --- - ~ - .

Page 21: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I F"WI

Category 3 - Noise > 0.2C (0O.40F): Mechanical and electrical inter-

ference can influence recorder output. Mechanical noise (e.g., resonant

L vibration) produces open spiking (figure 7). When spiking is greater

than O.20C (O.40F), interference is greater than the accuracy of the system.

The trace is therefore erroneous and should not be encoded. Additional

probes should be launched until the problem disappears, because mechanical

noise is usually intermittent. When encoding a trace with interference

less than 0.20C (O.40 F), the noise must be smoothed.

Electrical noise (e.g., interference from the ship's radio) causes

symmetrical stylus deflections (figure 8). Since the noise is symmetrical,

the trace can be smoothed through the center of the deflections.

Sometimes a "flat" spot occurs in the potentiometer of the recorder.

This will cause a vibration at 16.7 0 C (620F) on the trace (figure 9) during

both the Check/Run and Measure Modes. As with electrical interference,

the trace can be smoothed through the vibration.

14

Page 22: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

T E I, .3 DEPTH

J-I I I , - . . . . . . . , - I':1 ... .. ; -6'i -i-i _-- . . -

]- -. . . - --.. . . : t- I .F I',' I ' . .

I IJ

:I I Fi i 7 Nis great

-;- :-,- - ' I t i I ,_u- - - , . '; i } I 1 , ' ! .. ' - -

K[LI'41f h'"IF(external mechanical

Linterfeenc L

L: ! 4 , iLlLuiF

Page 23: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

{ I Ili;~ l '

A - 5 .C, I

TE PE110-U15 25 I thI

rV ___ _ - - - i..I

"IL 0 I

>I

- T -1

L~f-. I ! I -

tII III I~t 3 - 0-

f.. f i 4: 1I'

ii ii "

] i Figure 8 -Electrical noise

- a jLL'-*-----------_- - -J~-*- -253

0

Page 24: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I ,A 1 1 1L ~ I I EI_

I IU 1 0

-A-

3 005 I I250

-211

~~-fit 11

I TItI 11. -H

Page 25: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 4 - Wire break: Figure 10 shows an obvious failure at 535 m.

(Note: A 5 m negative depth correction must be applied to this trace

because of depth offset at the surface.) The cause appears to be due to

initial wire fouling on the ship (spike to high-temperature side) followed

by wire break. This trace is usable to 535 m. In this case, the wire

broke from the spool in the launcher and the open circuit caused the stylus

to travel off-scale at the low-temperature end. When the wire breaks from

the descending probe's spool, the short circuit drives the stylus to the

high-temperature end of the scale (figure 11).

18

Page 26: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

K.. ~~T Mrl~-~- EPE RATJY. (C) - DEPTH- (tv~ k1"

_____+ r I-

__ FT

L __r'#ji~ -Aj- :~r ~~ I[1JL7{LI J1V-

L' iiI ItR~ ~ Z..h L _T~'''Ill-I

v 2'

Fiur 10 Fuigf wdb ir

I break at launcher

Page 27: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

TEP AU~ A)DEPTH (METERS)

'2~~~1 4: V4 53

i-I TR °C

.. ..

0 7 2 -( - - i

1501

A.A JL..tI.. .f I0'. 5 1 -37

5- - - 2025' - 2 30-

i i 'Figure 11 Wire break from probe spool

, i

i I ~I

I I

Page 28: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 5 - Insulation penetration: Several possible causes can

lead to wire insulation damage followed by leakage, represented on a

trace by a sharp spike toward the high-temperature end of the scale

(figures 12 and 13). Two of the most commnon causes of damage include

wire contact with the ship's hull or wire hangup on a metal burr at the

open end of the launcher tube. Data recorded below the initial insulation

penetration are erroneous even though the insulation damage tends to heal

itself through interaction between wire and seawater. However, recovery

from the damage is never complete.

Figure 14 displays leakage in one of a probe's pair of wires. This

leakage causes a trace to show excessive temperature at depth. Another

probe should be launched in such cases.

21

Page 29: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I I a

Ad

*O i

- " ------------1

I :. 1 1 - '-I

Si i I .. } I ! I ' . l

i "--- I " - I . -+' .I : ? -- - l I

-17-

Figur 12 Wire i ns t io e e r t o

(a 15- m)--- wihatmta

r-V~~J3VE~~t~... Z! Kfi I" .4I - , -; ,-, --, -- l -- ... =- -.

. ... -' -- ---- i-r-1 . z - - - --

I ,_- ... mI' I9- 9 - '

_I

'- , I-,

J i I -±_-_--1 , --

. . ._ i - - recovery

' I ' I

I I-, ,. ,.,

* 24

V.'!

Page 30: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

7 I-

It'

it I-r-~~L I~ OuIJ - 7-- [.

P 7 141 h00

3 0 *-.'3

L t _5 , _;&

(at 31 m) foloe by

Page 31: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

-u5

* 0 10 5 2 5 3100

z

-15

I-

>--4

aI , ---- -z L I hi K-- .-

- 7-

Page 32: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 6 -_Wire stretch: Increased tension due to poor wire

unreeling leads to wire stretch. This results in a characteristic bulge

to the high-temperature side that can occur at any point in the trace

(figures 15, 16, and 17). Data recorded beyond the stretch point are

erroneous because of a permanent change in the conductive characteristics

of the wire.

Subtle wire stretch within the mixed layer (figure 16) has recently

been documented during several oceanographic experiments (Dugan and

Schuetz, 1977). These features appear on traces using stock Navy T-4

probes (460 m/1500 ft). This malfunction seriously degrades data quality

by affecting the temperature gradient and thickness of the mixed layer.

Failure rate In excess of 70 percent has been noted for T-4 probes more

than 4 years old.

25

Page 33: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

-u IT

- ~ ~ _ --£-TH 1*

~ L RT - -L

7_ -7 -7o ~ 4-~I-- L I'F L 4 J_

4~~~I--~~ 774t04rK_±~K'-r- 0-z0 (

VLIX 7 ___ K -TT-2

~ ~----300I

> Tj -- L4 4

4-fI

I I. '7

I- F Figure 15 -Wire stretch (good to 405 m)

:7

Page 34: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

PEW-

F *1 I 'RI: :-C. ....... ..LA ~:

P, *~I'*z i i T\PcTJ~(C tPH

I A 7Hi1~ i _

a 75 I3Y - . .

n-7

-J ~K4

r;IeI6 WiestechiImxd ae(tac isnogod

Page 35: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

ITEPE AT -R.: (0 CDEPTH 1 ..t _ t-- -i_

4F- T I

:i- 'I , :--L -- ' -

. T, "--I F- " --I ..

__-T---7-_0_5_._..

__j4.jf

InF

-,-' -41 w --- ; . .

LigurL 17Wr techa otmo-- - 1 1-1 1

I T tI -L -! _! ,'"i " -

tracer ,su t in false

I i

.ii I I i i, I-o,.~

r - - z~ _c :n i ,_ ..... --- -

Page 36: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 7 - Improper ground or leakage at launcher: Figures 18 and

19 show the results of a faulty launcher ground and an electrical leakage

at the launcher, respectively. Both traces are erroneous. Possible

causes for these problems are 1) improper grounding of the deck-mounted

launcher, 2) leakage caused by corrosion or moisture at the canister

contacts in the launcher breech, or 3) launcher-to-recorder cable leakage.

Launcher and ground connections should be checked to assure proper contacts

and electrical continuity of the system. The operator is referred to the

Sippican Corporation Instruction Manual for the Expendable Bathythermograph

System (1975) for adjustment and troubleshooting procedures.

29

-- -'-- ( -' m T -ur n-- - ih- . =-=. - - -,,

Page 37: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

DOIjA -A _' ~ I I

* I II III ~ i~ WIN

~ UFRC---q

'EL 0t CI- ~----

F- ~-[--

K1-V4 ____ IT TD

JJ1

AL-'

Page 38: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I- I

I .[1 1 t ~ -. 00_1

I2 4 C- 01

55O

_ _ _ _F ! _ _

fi IFI-Ir 19 Lanhrlaag a 5m

Page 39: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Category 8 - Doubtful features: Without knowledge of expected oceano-

graphic conditions, an observer can have difficulty discerning good data

from bad data. Figures 20 and 21 display features which may or may not

be real. Comparison should be made between succeeding traces in the same

area to determine if the feature is real. Doubtful features can appear

at any point in the trace. Care must be taken, however, in labeling

features as doubtful. Variations in thermal structure do exist, particu-

larly in regions of oceanic fronts and eddies, but they can also occur

in relatively stable regions.

32

Page 40: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

-1T R O I !D PT

oi ,-; . ! I I I,- • _ ! ! -$ i . I ! I

, -. -: 22 - - 7__:L7 _}o

I I I vK'H'-_ '1 i' -- ---

-15

,I: • y K x i J + __- -j--,_ "..-, -0-

,VFT j_'j-2) .- ,-- , 4

71~L1Ii I2-f- r It i _ - - 0- . o O

' '- --.... F- -: I -, - - -- --- ----I 0!

TIi

i___ _I_ I_..... --l-,!. .... ,-,-ii

---- -- '- -- .. . -(- 4- -- I

14 T'FH A

) 2253iu' 20 D t f t . . t

..... 3- 1- 1 .

I: ...... lTiV'H- :---

- I 1 - Iil; -_.-,--,.__ .... - _,, mixed layer [__I_ o _ .:

I _ Figure 20 - Doubtful feature within the

ii

Page 41: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

- TEMvPE, ATURE (C~ DET OMEIE-

-SUR;

-A-

K0 l5' 2j'252

74z

44+ 1 -it ~ L 10 25-3- '4o

z -

_____4 1 t..~i~.. __

r :: - - t - .7

Page 42: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Probe hits bottom: When bottom depth is less than the rated depth

of a probe, bottoming occurs (figures 22 and 23). An indication that a

probe has hit bottom is given by a small horizontal spike in the trace

followed by an isothermal reading. However, little or no spiking may

appear if the bottom is soft. In shallow areas, it is important to

know the bottom depth so that false data do not result from encoding data

below the actual bottom.

35

Page 43: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

TEMPEATUR (oC) DEPTH (METERS)

V--_ R'- 50-"°

(J1 -- - i'-....- t 14--

M. .

forr

M cz

- -- - . ''--- T I- -T j0- 700

-b - + -- I !- _----7

317

>T1: --_ 2 5 - -

44: tTi It-

1 5 ,, ,

II~ 0 41:1 ~ 5>

r_-- __1 oO1i

Figure 22 Shallow drop - bottom spikea 32 m-) .... o.o owed b

'L r .. ..- isothermal reading as probe

15~

-L -- les n b tto

F ±7 :~ "

47VI

-> -!JEL I3' F- V11r A :

-1 I t I I 1 If

"t---' " L 1Fgr 22 Salo dro - : boto sp ike--- -

Page 44: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

TEMPE 'ATURE (IC) DEPTH (METERS) I-~ ~ '~ b -URF AC E-i

_ + ., t-. ._ -. -I

-. 1 T -- 150-

v 1 -4- -

I :Ltz T 1' ... 0VI

A - - - -- o

>' I... is nO_-_i-- L 0>E - -; .....

. ..

-41J~ 4z _____kji ii... H- S1 0_ 25-3 ... 0.

_ BOTTOM 326M2r 6M. r -3501

- LttiZ-4 ' , , ' .,1o.

___ ___ ___ 1 .Iti II'

,-' . *. . _*..I

-L [ ; t7I -t .... +25 "3"- r '3

4 - "C-.2,

5 ,-, . .-1- 3 D[

tj jFigure 23 -Shallow drop -bottomn spikeL (at 326 m) followed by wire

, " 'leakage5ii - : I I!

37'

* -F u---

Page 45: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Frontal regions: Care must be exercised in determining data quality

in the vicinity of oceanic fronts. Proper maintenance and calibration of

the system Is very important in frontal regions because the temperature

structure can vary significantly between SXBT observations. The trace

shown in figure 24 was obtained in the Gulf Strewn. The trace exhibits

a rather large (70C) temperature inversion caused by entrainment of cold,

relatively fresh water from coastal regions. This trace was originally

labeled as questionable; however, a nearby SXBT (figure 25) also shows a

temperature inversion. These temperature inversions are real. Higher-

than-normal probe failure rates should be expected near major oceanic

fronts because of increased current shear and turbulence.

38

Page 46: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

M.rEA TURE ('C) ,

-4 _' ... L ' - .- 1

I I

Vt":fj ' 4 '_L i

" I I - ... . I ' - l -

Lt.

";~ __

-_~i7~ 11.1 ! iJ [.i

LL ~ L~. 5

" i .j I5 lo1c.

ri7]Kj. L !![111:" t .+JL. . /"

, . . r .[ I I

' t 221-.I..,L - : -

-I 1 _.' I .

.II! 'j I-, , -_ _- '

ii I~I, t I , ,

1 'LI

'I 1 --

"" I I Fgr 4-Fotlregion with real

25

117 I T-T

-iI : .II I7

LL

+ -4[-

Page 47: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

TEMP A (0 C) DEPTH (T- RS)

1-USA ... .... ---+"~~~ ~~ L~!__ .......

>~~~~~~ 7|+ "+ --u- ..

i I

. i i J--- -

L I- 13101;~~ ~ ~ 2- 255- t-30 + -- , ---

IIi t. _ LJ L- I-

_-I I I L H I , I _ t"$11 1 L K.4± l I ir.L lI tl -li- i ',--1*3. + i fl? im !! i I I;° -

~ ~ i~ j I]1L1147VT i i:LL L~'iLit

---I I : !

------ -45 50.ilt II; .I '. I

" jI " + J lIJ] '

I " ' + uFiur 2-'"5 F a reio _w rith rea

_. 40' I I

Page 48: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

REFERENCES

Dugan, J.P. and A.F. Schuetz, Subtle T4 XBT malfunction, NRL memorandumreport 3612, l6pp. (unpublished manuscript), 1977.

Sippican Corporation, Instruction Manual for the Expendable Bathythermo-graph System R-603. Marion, Massachusetts. Revised 1975.

41

OIL, . . .. "' i " ' : ,,= - - 1

Page 49: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

APPENDIX A

RECORDER CALIBRATION PROCEDURES

If a recorder check indicates that the extreme calibration temperatures

exceed the specified limits of + 0.10C at -l.10C (f O.20 F at 30°F and 940F),

the recorder must be calibrated. Calibration is regulated by the servo

potentiometer and the printed circuit scan potentiometer (figure A-l).

Two separate devices can be used to calibrate the SXBT system to specifica-

tions 1) an A2A test canister to be inserted into the launcher or 2) an

A-4 XBTester to be connected to the launcher terminal block on the left

of the recorder and to the launcher cable. If neither of these testing

devices is available, the operator is referred to the instruction manual

(Sippican, 1975) for the schematic diagram of the test canister so that

the proper circuit can be constructed if electrical resistors are available.

After inserting the test canister or connecting the XBTester, the

following steps should be followed in the given order during calibration.

1. Rotate the servo potentiometer to adjust the low-scale temperature

to -l.10C/30°F within the + O.1°C/+ O.20F tolerance limit.

2. The printed circuit scan potentiometer is then adjusted to set

the high-scale temperature at 34.4°C/94°F within the same limit by turning

the scan potentiometer screw.

3. With the system set in the Measure Mode and with the chart ad-

vancing, alternately check and adjust the servo and scan potentiometers

until the temperature values are within specified limits.

42

Page 50: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

4. During a 2-second Check/Run Mode, the recorder should read

16.70 + O.10C (620 + O.20F). If notthe servo potentiometer or a resistor

in the printed circuit board is defective.

43

- - -. . . . .

Page 51: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

Figure A-i1 Recorder subassemblies, right side (Sippican, 1974)

Page 52: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

I

APPENDIX B

GAIN AND OVERSHOOT ADJUSTMENT

If a stylus slew rate and overshoct check indicates that the recorder

gain exceeds the limits for maximum full-scale slew or overshoot, the

servo amplifier gain control (figure B-1) must be adjusted.

1. With the system in Measure Mode and with the chart advancing,

alternately set the calibration switch (marked 940 - 300) to the low

(-l.1 0 C/300 F) and high (34.40C/940F) temperature ends. Adjust the gain

control until the overshoot is between 0.30C and 0.50C (0.50F to l.O°F).

2. Check the slew rate of the stylus across the chart by again

alternately setting the calibration switch to the high and low ends.

The slew rate across the chart paper should now be 1.5 seconds or less

(approximately lOm). Never overtighten the gain control, because this

increases response lag in the stylus.

45

Page 53: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

-NI -MO'--

Page 54: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

DISTRIBUTION

ATLANTIC

CINCLANTFLT FASOTRAGRULANT DET BRUNSWICKCOMSECONDFLT " " OCEANACOMSIXTHFLT " CECIL FIELDCOMNAVSURFLANT " JACKSONVILLECOMCRUDESGRU 2 "" KEY WEST

" 8 COMTRALANT" 12 COMFLETRAGRU GUANTANAMO

COMSURFWARDEVGRU COMNUWPNTRAGRULANTCOMDESRON 2 DIRNAVOCEANMET (36 copies)

" 4 USS FORRESTAL (CV 59)I" 6 "1 SARATOGA (CV 60)

10 It INDEPENDENCE (CV 62)12 " AMERICA (CV 66)14 " CALIFORNIA (CGN 36)

" 20 i SOUTH CAROLINA (CGN 37)" 22 " VIRGINIA (CGN 38)" 24 i" ALBANY (CG 10)I 26 " HARRY E. YARNELL (CG 17)" NRF 28 " DALE (CG 19)" NRF 30 " RICHMOND K. TURNER (CG 20)

COMSEABASEDASWWINGSLANT JOSEPHUS DANIELS (CG 27)COMPATWINGSLANT " WAINWRIGHT (CG 28)PATRON 5 " WILLIAM H. STANDLEY (CG 32)

" 8 BIDDLE (CG 34)" 10 WILLIAM R. RUSH (DD 714)" 11 " WILLIAM M. WOOD (DD 715)S16 " WILLIAM C. LAWE (DO 763)" 23 " CORRY (DD 817)

24 It HOLDER (DO 819)" 26 " RICH (DO 820)

30 JOHNSTON (DD 821)44 " ROBERT H. MCCARD (DD 822)45 BASILONE (DD 824)

" 49 " ROBERT A. OWENS (DO 827)56 " MYLES C. FOX (DO 829)

PATRON DET SIGONELLA " CHARLES P. CECIL (DD 835)" " ROTA " SARSFIELD (DD 837)" " LAJES " POWER (DO 839)

COMCARGRU 2 " GLENNON (DD 840)4 " FISKE (DO 842)6 VOGELGESANG (DO 862)

AIRANTISUBRON 22 " STEINAKER (DD 863)24 HAROLD J. ELLISON (DO 864)30 " CONE (DD 866)

" 31 " BROWNSON (DO 868)32 " DAMATO (DD 871)

- -?

Page 55: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

HELANTISUBRON I USS HAWKINS (DD 873)ii 3

I 5

I, 7I" 11

USS DYESS (DD 880) USS MILLER (FF 1091)" NEWMAN K. PERRY (DD 883) " THOMAS C. HART (FF 1092)" MEREDITH (DD 890) " CAPODANNO (FF 1093)" FORREST SHERMAN (DD 931) " PHARRIS (FF 1094)" BARRY (DD 933) " TRUETT (FF 1095)

DAVIS (DD 937) " VALDEZ (FF 1096)" JONAS INGRAM (DD 938) " MOINESTER (FF 1097)

MANLEY (DD 940) " TALBOT (FFG 3)DUPONT (DD 941) " RICHARD L. PAGE (FFG 5)BIGELOW (DD 942) " JULIUS A. FURER (FFG 6)BLANDY (DD 943) " GLOVER (AGFF 1)MULLINNIX (DD 944)SPRUANCE (DD 963)CHARLES F. ADAMS (DOG 2)JOHN KING (DDG 3) PACIFIC

" LAWRENCE (DDG 4)CLAUDE V. RICKETTS (DDG 5) CINCPACFLT

" BARNEY (DDG 6) COMTHIRDFLTiSAMPSON (DDG 10) COMSEVENTHFLT

" SELLERS (DDG 11) COMNAVSURFPACCONYNGHAM (DDG 17) COMCRUDESGRU 1SEMMES (DDG 18) " 3TATTNALL (DDG 19) 5

" RICHARD E. BYRD (DDG 23) COMNAVSURFGRU WESTPAC" MITSCHER (DDG 35) COMDESRON 5" FARRAGUT (DDG 37) " 7" LUCE (DDG 38) " 9

MACDONOUGH (DDG 39) " 13COONTZ (DDG 40) 15MAHAN (DDG 42) 17DAHLGREN (DDG 43) 21WILLIAM V. PRATT (DDG 44) " 23

" DEWEY (DDG 45) " 25" MCCLOY (FF 1038) " NRF 27" GARCIA (FF 1040) " 31

EDWARD MCDONELL (FF 1043) " 33BRUMBY (FF 1044) 35

" VOGUE (FF 1047) COMTRAPAC• KOELSCH (FF 1049) COMFLETRAGRU PEARL HARBOR

CONNOLE (FF 1056) COMFLETRAGRU SAN DIEGO" W. S. SIMS (FF 1059) COMFLETRAGRU WESTERN PACIFIC

PATTERSON (FF 1061) COMNUWPNTRAGRUPACVREELAND (FF 1068) FLTCOMBATSYSTRAUPAC

" BLAKELY (FF 1072) COMCARGRU I

Page 56: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

IUSS TRIPPE (FF 1075) COMCARGRU 3" JOSEPH HEWES (FF 1078) " 5" BOWEN (FF 1079) 7

PAUL (FF 1080) COMASWWINGPACAYLWIN (FF 1081) AIR ANTISUBRON 21

" ELMER MONTGOMERY (FF 1082) 29MCCANDLESS (FF 1084) 33

" DONALD B. BEARY (FF 1085) 35" JESSE L. BROWN (FF 1089) 37

AINSWORTH (FF 1090) 3841

HELANTISUBRON 6 USS COCHRANE (DDG 21)8 BENJAMIN STODDERT (DDG 22)

FASOTRAGRUPAC DET MOFFETT FIELD " WADDELL (DOG 24)BARBERS POINT DECATUR (DDG 31)

COMPATWINGSPAC JOHN PAUL JONES (DDG 32)PATWING 1 PARSONS (DDG 33)

" 2 SOMERS (DOG 34)PATRON 1 JOHN S. MCCAIN (DDG 36)

4 PREBLE (DDG 46)6 HAMNER (DD 718)9 SOUTHERLAND (DO 743)17 MCKEAN (DD 784)19 HENDERSON (DD 785)

" 22 HOLLISTER (DD 788)31 " HIGBEE (DD 806)40 " CARPENTER (DD 825)46 AGERHOLM (DD 826)47 BAUSELL (DD 845)48 LEONARD F. MASON (DD 852)50 ROGERS (DD 876)

PATWINGSPAC DET ADAK JOHN R. CRAIG (DD 885)PATWING ONE DET AGANA ORLECK (DD 886)

" " "CUBI PT " HULL (DD 945)KADENA EDSON (DD 946)

MISAWA " MORTON (DD 948)FLENUMWEACEN RICHARD S. EDWARDS (DD 950)USS MIDWAY (CV 41) TURNER JOY (DD 951)

RANGER (CV 61) PAUL F. FOSTER (DD 964)" KITTY HAWK (CV 63) KI-KAID (DD 965)" CONSTELLATION (CV 64) t HEWITT (DD 966)

LONG BEACH (CGN 9) " ELLIOT (DD 967)BAINBRIDGE (CGN 25) DAVID R. RAY (DD 971)TRUXTON (CGN 35) OLDENDORF (DD 972)

" OKLAHOMA CITY (CG 5) JOHN YOUNG (DD 973)CHICAGO (CG 11) " COMTE DE GRASSE (DD 974)

" LEAHY (CG 16) " OBRIEN (DD 975)" WORDEN (CG 18) t BROOKE (FFG 1)" GRIDLEY (CG 21) " RAMSEY (FFG 2)

ENGLAND (CG 22) " SCHOFIELD (,FFG 3)" HALSEY (CG 23) BRONSTEIN (FF 1037)

I

Page 57: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

USS REEVES (CG 24) USS BRADLEY (FF 1041)

JOUETT (CG 29) " DAVIDSON (FF 1045)

HORNE (CG 30) SAMPLE (FF 1048)STERETT (CG 31) ALBERT DAVID (FF 1050)FOX (CG 33) O'CALLAHAN (FF 1051)HENRY B. WILSON (DDG 7) " KNOX (FF 1052)LYNDE MCCORMICK (DDG 8) " ROARK (FF 1053)TOWERS (DDG 9) GRAY (FF 1054)ROBISON (DDG 12) HEPBURN (FF 1055)HOEL (DDG 13) RATHBURNE (FF 1057)BUCHANAN (DDG 14) MEYERKORD (FF 1058)BERKELEY (DDG 15) LANG (FF 1060)JOSEPH STRAUSS (DDG 16) WHIPPLE (FF 1062)GOLDSBOROUGH (DDG 20) REASONER (FF 1063)LOCKWOOD (FF 1064)STEIN (FF 1065)MARVIN SHIELDS (FF 1066)

e FRANCIS HAMMOND (FF 1067)BAGLEY (FF 1069DOWNES (FF 1070)

" BADGER (FF 1071)ROBERT E. PEARY (FF 1073)

HAROLD E. HOLT (FF 1074)FANNING (FF 1076)OUELLET (FF1077)COOK (FF 1083)BREWTON (FF 1086)KIRK (FF 1087)BARBEY (FF 1088)SAMUEL GOMPERS (AD 37)NORTON SOUND (AVM 1)

DDC (12 copies)

Page 58: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

UNCLASSI FIEDSECURITY CLASSIFICATION OF THIS PAGE (When Date Entered)

REPORT DOCUMENTATION PAGE READ INSTRUCTIONSBEFORE COMPLETING FORM

1. REPORT NUMBER 12. GOVT ACCESSION NO. 3. RECIPIENT'S CATALOG NUMBER

NOO RP-21 10 - 2 5 __

4. TITLE (and Subtitle) S. TYPE OF REPORT & PERIOD COVERED

Guide to Common Shipboard Expendable FinalBathythermograph (SXBT) Recording Malfunctions N. PERFORMING ORG. REPORT NUMBER

7. AUTHOR(s) S. CONTRACT OR GRANT NUMBER(s)

Stephen M. KronerBarry P. Blumenthal

S. PERFORMING ORGANIZATION NAME AND ADDRESS 10. PROGRAM ELEMEN1T PROJECT, TASK

AREA & WORK UNIT NUMBERS

Naval Oceanographic OfficeNSTL Station, Bay St. Louis, MS 39522

II. CONTROLLING OFFICE NAME AND ADDRESS 12. REPORT DATE

Naval Oceanographic Office Auaust 1978NSTL Station, Bay St. Louis, MS 39522 46 (nMc 2 appendixes)

14. MONITORING AGENCY NAME & ADORESS(if different from Controlling Office) 1S. SECURITY CLASS. (of this rePart)

Unclassified

ISo. DECL ASSIPIC ATION/DOWNGRADINGSCHEDULE

14. DISTRIBUTION STATEMENT (of this Report)

Approved for public release; distribution unlimited.

IT. DISTRIBUTION STATEMENT (of the abetrct nstered in Block 20, if different from Report)

IS. SUPPLEMENTARY NOTES

IS. KEY WORDS (Continue on revero side If n'ceeaom end Idontib' by block numbe,)

SXBT SystemTemperature ProfilesSXBT Quality ControlBathythermograph

20. ABSTRACT (Continue on reverse aide it necee.a ry d identify by block n, ,ber)The Sippican SXBT system is a reliable method of measuringtemperatures in the upper few hundred meters of the ocean whileunderway. The system provides information on local temperaturedistribution and sonic conditions which assists the Navy intactical decision making.

This guide has been prepared to aid the system operator in

DD , 1473 EDITION OF I Nov 65 Is OBSOLETE U/1 0102-014-601 1 S UNCLASSIFIEDs/N ol -o1,-.o,,SECuR.TY CLAMI,,',ATON O,' T.,lS ,'AGE(. be-t.a h-.,-

Page 59: l3~EC[IROIN6 MALFUNCTION~~ - Defense Technical … · The authors would like to thank the Sippican Corporation for assistance in identifying probable causes of SXBT system recording

UNCLASSIFIED

,.L.,U"TY CLASSIFICATION OF THIS PAQgC(OWh.n ate* Sn*.'d)

20. discerning good data from bad data. It describes erroneous

SXBT traces and simple methods to be employed for rectifying

the more common problems which may occur with this equip-

ment.

UNCLASSIFIED

89CURITY CLASSIFICATION Of THIS PAGEI W". DOa BR.M.*

mm~ ~~~~~~~~~~~Z, Rqzc T ... - - -- '-- - . .