Optical characteristics of LEXEL 85 argon ion laser and Gsanger LM0202P modulator: application to AM-FM light conversion

Survival, Water, Medical Field Manuals

Military Manuals

Wallace, Harlan V.

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NAVAL  POSTGRADUATE  SCHOOL 
MONTEREY,  CALIFORNIA 


THESIS 


OPTICAL  CHARACTERISTICS  OF  LEXEL 

85  ARGON  ION  LASER  AND  GSANGER 

LM0202P  MODULATOR:  APPLICATION  TO 

AM-FM  LIGHT  CONVERSION 


by 


Harlan  V.  Wallace 


June,  1996 


Thesis  Advisor: 


D.  Scott  Davis 
Andres  Larraza 


Thesis 
W222342 


Approved  for  public  release;  distribution  is  unlimited. 


DUDLEY  KNOX  LIBRARY 

NAVAL  POSTGRADUATE  SCHOOL 

MONTEREY  CA  93943-5101 


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1.       AGENCY  USE  ONLY  (Leave  blank) 


REPORT  DATE 
June,  1996 


REPORT  TYPE  AND  DATES  COVERED 
Master's  Thesis 


4.       TITLE  AND  SUBTITLE   OPTICAL  CHARACTERIZATION  OF  LEXEL  85 
ARGON  ION  LASER  AND  GSANGER  LM0202P  MODULATOR: 
APPLICATION  TO  AM-FM  LIGHT  CONVERSION 


6.     author(S)  Harlan  V.  Wallace 


FUNDING  NUMBERS 


7.       PERFORMING  ORGANIZATION  NAME(S)  AND  ADDRESS(ES) 

Naval  Postgraduate  School 
Monterey  CA  93943-5000 


PERFORMING 
ORGANIZATION 
REPORT  NUMBER 


SPONSORING/MONITORING  AGENCY  NAME(S)  AND  ADDRESS(ES) 


10.     SPONSORING/MONITORING 
AGENCY  REPORT  NUMBER 


1 1 .    SUPPLEMENTARY  NOTES  The  views  expressed  in  this  thesis  are  those  of  the  author  and  do  not  reflect 
the  official  policy  or  position  of  the  Department  of  Defense  or  the  U.S.  Government. 


12a.    DISTRIBUTION/A VAILABILITY  STATEMENT 

Approved  for  public  release;  distribution  is  unlimited. 


12b.  DISTRIBUTION  CODE 


13.     ABSTRACT  (maximum  200  words) 

The  purpose  of  this  thesis  is  to  examine  the  possibility  of  using  a  commercial  electro- 
optical  modulator,  the  LM0202P  modulator  manufactured  by  Gsanger  Opto-Elektronic  of 
Germany,  to  amplitude  modulate  an  argon  ion  laser,  the  LEXEL  model  85,  for  proving  a 
theory  of  the  conversion  of  amplitude  to  frequency  modulation  of  light  in  fiber  optics.  The 
main  focus  is  to  analyze  the  spectral  output  of  the  laser  both  before  and  after  being  directed 
through  the  modulator.  Also  to  be  considered  is  launching  the  laser  light  down  a  length  of 
optical  fiber.  It  was  determined  that  the  laser  does  not  produce  a  single  mode, 
monochromatic  spectral  line.  Further,  it  was  determined  that  when  the  laser  is  directed 
through  the  modulator,  the  structure  on  the  laser  profile  tends  to  blur.  This  effect  increases 
when  DC  bias  voltage  is  applied  to  the  modulator.  Additionally,  when  the  modulator  is 
driven  with  an  AC  modulation  superimposed  on  the  DC  bias  voltage,  the  resultant  optical 
spectral  profile  does  not  correspond  to  that  expected  for  sinusoidal  amplitude  modulation. 


14.    SUBJECT  TERMS  Spectral  Analyis  of  Argon  Ion  Laser 


15.    NUMBER  OF 
PAGES      57 


16.     PRICE  CODE 


17.  SECURITY  CLASSIFI- 
CATION OF  REPORT 
Unclassified 


SECURITY  CLASSIFI- 
CATION OF  THIS  PAGE 
Unclassified 


19.     SECURITY  CLASSIFI- 
CATION OF  ABSTRACT 
Unclassified 


20.     LIMITATION  OF 
ABSTRACT 
UL 


NSN  7540-01-280-5500 


Standard  Form  298  (Rev.  2-89) 

Prescribed  by  ANSI  Std.  239-18  298-102 


11 


Approved  for  public  release;  distribution  is  unlimited. 

OPTICAL  CHARACTERISTICS  OF  LEXEL  85  ARGON  ION  LASER 
AND  GSANGER  LM0202P  MODULATOR:  APPLICATION  TO  AM-FM 

LIGHT  CONVERSION 


Harlan  V.  Wallace 

Lieutenant,  United  States  Coast  Guard 

B.S.,  University  of  Utah,  1989 

Submitted  in  partial  fulfillment 
of  the  requirements  for  the  degree  of 

MASTER  OF  SCIENCE  IN  PHYSICS 

from  the 

NAVAL  POSTGRADUATE  SCHOOL 
June,  1996 


DUDLEY  KNOX  LIBRARY 

NAVAL  POSTGRADUATE  SCHOOL 

MONTEREY  CA  93943-5101 


ABSTRACT 


The  purpose  of  this  thesis  is  to  examine  the  possibility  of  using  a  commercial 
electro-optical  modulator,  the  LM0202P  modulator  manufactured  by  Gsanger  Opto- 
Elektronik  of  Germany,  to  amplitude  modulate  an  argon  ion  laser,  the  LEXEL  model  85, 
for  proving  a  theory  of  the  conversion  of  amplitude  to  frequency  modulation  of  light  in 
fiber  optics.  The  main  focus  is  to  analyze  the  spectral  output  of  the  laser  both  before  and 
after  being  directed  through  the  modulator.  Also  to  be  considered  is  launching  the  laser 
light  down  a  length  of  optical  fiber.  It  was  determined  that  the  laser  does  not  produce  a 
single  mode,  monochromatic  spectral  line.  Further,  it  was  determined  that  when  the  laser 
is  directed  through  the  modulator,  the  structure  on  the  laser  profile  tends  to  blur.  This 
effect  increases  when  DC  bias  voltage  is  applied  to  the  modulator.  Additionally,  when  the 
modulator  is  driven  with  an  AC  modulation  superimposed  on  the  DC  bias  voltage,  the 
resultant  optical  spectral  profile  does  not  correspond  to  that  expected  for  sinusoidal 
amplitude  modulation. 


VI 


TABLE  OF  CONTENTS 

I.  INTRODUCTION 1 

II.  OVERVIEW  AND  PRELIMINARY  MEASUREMENTS 7 

A.  INTRODUCTION 7 

B.  LASER 8 

C.  MODULATOR 10 

D.  ELECTRONIC  DRIVING  CIRCUIT 15 

E.  DETECTORS  AND  POWER  METERS 19 

F.  ALIGNMENT 21 

G         FABRY-PEROT  INTERFEROMETER 25 

III.  LASER  OUTPUT  SPECTRUM  AND  SEARCH  FOR  AM  SIDEBANDS 27 

A  OUTPUT  SPECTRUM  OF  LEXEL  85  ARGON  ION  LASER 27 

B          EFFECT  OF  LM0202P  MODULATOR  ON  LASER  SPECTRUM  ....  29 
C.         SEARCH  FOR  AM  SIDEBANDS 31 

IV.  FIBER  OPTIC  COUPLING 35 

A.  INTRODUCTION 35 

B.  ATTENUATION 40 

V.  CONCLUSIONS  AND  RECOMMENDATIONS 43 

LIST  OF  REFERENCES 45 

INITIAL  DISTRIBUTION  LIST 47 


vn 


I.  INTRODUCTION 

Due  to  self-interaction  effects,  the  frequency  of  a  wave  in  a  dispersive  medium  is 
amplitude  dependent,  and  in  the  weakly  nonlinear  regime  it  is  of  the  form 

co(k)  =  co0(k)  +  co2(k)e  .        (1.1) 

In  expression  (1.1),  co0(k)  is  the  linear  dispersion  relation,  co2  (k)  is  the  nonlinear 

coefficient,  and  e  is  the  energy  density  which  is  proportional  to  the  square  of  the  wave 
amplitude.  For  the  case  of  fixed  frequency,  positive  group  velocity,  and  co2  >  0,  the  effect 

of  nonlinearity  is  to  decrease  the  wavenumber  k  as  the  amplitude  of  the  wave  field 
increases. 

To  understand  the  combined  effects  of  dispersion  and  nonlinearity,  we  follow 
closely  the  physical  argument  given  by  Larraza  and  Coleman  [1].  Consider  an  initial  state 
of  a  modulated  wave  observed  in  a  frame  moving  with  the  group  velocity  (Figure  la).  An 
observer  in  this  frame  would  see  the  crests  of  the  wave  propagate.  Because  of  dispersion, 
the  group  and  phase  velocities  are  different. 

Consider  now  the  case  where  the  nonlinear  coefficient  (o2>0.  An  observer  in  the 

frame  moving  with  the  linear  group  velocity  would  observe  bunching  of  the  crests  when 
the  modulation  amplitude  is  low  and  anti-bunching  when  the  modulation  amplitude  is  high 
(Figure  lb).  For  positive  dispersion,  co  (k)>0, 

5vg  =co//(k)5k  (1.2) 

increases  towards  the  troughs  of  the  modulation.  Dispersive  effects  cause  the  energy  to 
approach  the  troughs  of  the  envelope,  and  the  modulation  propagates.  Thus,  to  an 
observer  moving  with  the  linear  group  velocity,  the  modulation  is  no  longer  stationary. 
Instead,  the  modulation  can  propagate  with  both  a  velocity  that  is  either  higher  or  lower 
than  the  linear  group  velocity.  This  result  is  general,  when  the  product  co2co   is  positive. 


(a) 


(b) 


Figure  1.  Modulated  waves,  (a)  Initial  state  of  a  modulated  wave  in  the  frame  moving  with  the  group 

velocity  v„.  (b)  For  positive  dispersion,  co  (k)  >0  and  ©2  >  0,  dv„  increases  toward  the  troughs 
of  the  modulation,  and  the  modulation  propagates. 


The  stability  of  the  modulation  has  the  important  consequence  of  AM-FM 
conversion.  This  effect  can  be  physically  understood  by  considering  again  a  modulated 
wave  in  a  frame  moving  with  the  linear  group  velocity  (Figure  2a).  Assume  that  both  the 
dispersion  and  the  nonlinear  coefficient  co2  are  positive.  Due  to  nonlinear  effects,  an 

observer  at  a  fixed  location  in  this  frame  would  see,  after  some  time,  alternating  bunching 

and  anti-bunching  of  the  wave  crests  (Figure  2b).  Because  dispersive  effects  cause  the 

energy  to  approach  the  troughs  of  the  envelope,  for  this  observer  it  would  appear  that  at 

some  time  later  the  initial  amplitude  modulation  has  become  a  frequency  modulation 

(Figure  2c).  Dispersive  effects  would  again  remove  energy  from  the  region  where  the 

crests  are  more  spread  apart  to  the  region  where  the  crests  are  closer  together.  For  the 

observer  fixed  in  the  frame  moving  with  the  group  velocity  it  would  appear  that  an 

amplitude  modulation  is  superimposed  upon  the  frequency  modulated  signal  (Figure  2d). 

Nonlinearity  will  prevent  an  overshoot  of  energy  flow  to  the  crest  of  the  modulation,  and 

an  amplitude  modulation  1 80°  out  of  phase  with  respect  to  the  original  signal  results  at  a 

later  time  (Figure  2e).  In  the  frame  moving  with  the  group  velocity,  the  process  repeats 

periodically,  and  an  observer  in  this  frame  sees  that  the  modulations  experience  beats.  In 

the  laboratory  frame  if  a  source  is  generating  an  amplitude  modulated  signal,  some 

distance  away  it  will  become  frequency  modulated.  Larraza  and  Coleman  [1]  also  give  a 

quantitative  theory  for  this  effect.  They  have  shown  that  an  amplitude  modulated  signal 
with  amplitude  ^/e^ ,  modulation  amplitude  m,  modulation  frequency  Q,  and  carrier 

frequency  co  will  evolve  according  to 

a(x,t)  =  A/e^[l  +  mcos(Ax)cos(Qt-'nx)] 

(1.3) 


cos 


k0x-cot 


—^rJ-ZjT  sin(Ax)cos(Qt-r|x) 

i2       V    ^o 


where  A  =  Q-^co q co 2©o  ^o' 


(a) 


time 


(b) 


(c) 


(d) 


(e) 


Figure  2.  Time  evolution  of  modulation.  An  observer  in  a  frame  moving  with  the  linear  group  velocity 
observes  AM-FM  conversion  in  time. 


A  possible  application  of  this  result  is  broadband  tunable  lasers  using  fiber  optics. 
Here,  we  are  interested  in  single  mode  fibers  consisting  of  a  glass  core  of  high  index  of 
refraction  surrounded  by  a  cladding  with  a  lower  index  of  refraction  (about  0. 1%  smaller). 
In  this  case,  for  light  in  the  visible  range  the  dispersion  is  normal  with  co  „(k)  <  0.  For  light 
with  intensity  I,  the  index  of  refraction  is  given  by  n(I)  =  n0  (co)  +  n2I ,  where  nrj«l  .5. 
Thus,  the  frequency  nonlinear  coefficient  co2  ~  -ou^coo  ^n  ls  negative,  where  a  is  a 
numerical  factor  of  order  unity.  The  order  of  magnitude  of  the  coefficient  n2  (in  units  of 
cm2/W)  is  typically  about  1CT11  or  higher  in  doped  glasses. 

Because  the  product  a0  (k)co2  >  0,  the  physical  picture  presented  above  applies  to 
this  case.  In  particular,  for  aO.lW  source  operating  at  a  frequency  of  5.8  x  1014  Hz  and  a 
50%  amplitude  modulation  of  1010  Hz  in  a  10  urn2  fiber,  the  distance  xm  =  7t/2A  for  AM- 

FM  conversion  is  about  20  m  in  doped  glasses.  The  corresponding  FM  frequency 
spectrum  has  a  range  of  about  3.5x1 014  Hz  in  doped  glasses.  Thus,  in  doped  glasses,  an 
amplitude  modulated  green  light  alternating  between  bright  and  dim  at  the  source  will 
alternate  between  red  and  blue  at  a  rate  of  1010  Hz  at  a  location  about  20  m  down  the 
fiber.  This  mechanism  allows  the  possibility  of  producing  tunable  phased-locked  coherent 
light  from  a  single  frequency  coherent  source. 

The  purpose  of  this  thesis  research  consists  of  three  tasks.  First  is  to  evaluate  the 
frequency  output  of  an  argon  ion  laser  source  in  single  mode  operation  at  514.5  nm.  The 
objective  is  to  know  precisely  how  well  the  laser  produces  a  single  mode  output.  The 
second  task  is  to  evaluate  the  side  bands  of  that  same  argon  ion  laser  source  when  it  is 
amplitude  modulated  at  frequencies  of  the  order  of  100  MHz.  The  objective  is  to  obtain 


high  enough  resolution  with  a  Fabry-Perot  interferometer  to  actually  distinguish  the  AM 
sidebands  from  the  carrier  and  thus  verify  that  amplitude  modulation  behaves  as  expected. 
The  third  task  is  to  measure  the  attenuation  of  the  green  laser  light  in  a  typical  silica-based 
optical  fiber.  This  information  will  all  be  used  in  follow-on  work  towards  the  ultimate  goal 
of  AM-FM  light  conversion. 

Chapter  II  discusses  the  set-up  of  the  overall  experiment  (Figure  3)  and  describes 
each  component  of  the  experiment  in  detail.  Some  preliminary  measurements  and  results 
are  also  presented  in  Chapter  II.  Chapter  III  discusses  the  measurements  of  the  frequency 
output  of  the  argon  ion  laser  and  the  search  for  AM  sidebands.  Chapter  IV  discusses  fiber 
optic  coupling  and  the  measurement  of  attenuation. 


Figure  3.  Photographs  of  the  set-up  of  the  experiment.  Left:  modulator,  mirrors  and  filters, 
interferometer.  Right:  laser,  power  supplies,  oscilloscope,  power  meters. 


H.  OVERVIEW  AND  PRELIMINARY  MEASUREMENTS 

A.  INTRODUCTION 

This  chapter  discusses  the  details  of  each  component  of  the  experiment.  Figure  4 
shows  the  overall  set-up  of  the  experiment.  A  continuous  wave  argon  ion  laser  is  used  for 


Detector 

.         Mirror 


Laser 


Modulator 

-+I 


Microscope 
Slide 


Electronic 
Circuit 


Detector  to 
Oscilloscope 


Interferometer 


Optical 
Fiber 


Fiber  Optic 
Coupler 


Figure  4.  General  set-up  of  experimental  components.  The  modulator,  microscope  slide,  mirror,  and  fiber 
optic  coupler  are  all  mounted  on  a  rail  such  that  they  can  be  individually  removed  and  replaced 


the  light  source.  The  laser  beam  is  directed  through  an  electro-optic  modulator  for 
amplitude  modulation.  A  Brewster  cube  is  attached  to  the  exit  end  of  the  modulator  and 
acts  as  a  beam  splitter  sending  one  beam  parallel  to  the  incident  beam  and  a  second  beam 
perpendicular  to  the  incident  beam.  The  perpendicular  beam  is  directed  into  a  detector  so 
that  the  average  value  of  the  optical  power  can  be  is  monitored.  Both  the  frequency  of 
modulation  and  the  amplitude  of  modulation  are  determined  by  the  electronic  circuit 
connected  to  the  modulator.  The  circuit  can  be  tuned  to  produce  different  frequencies  and 
amplitudes  of  modulation.  A  microscope  slide  is  used  to  reflect  a  small  portion  of  the 
forward  beam  into  a  detector  whose  output  is  sent  to  an  oscilloscope.  The  majority  of  the 


beam  passes  through  the  microscope  slide  and  is  guided  to  propagate  down  a  fiber  optic 
cable.  A  mirror  can  be  placed  in  front  of  the  optical  fiber  and  used  with  a  second  mirror  to 
direct  the  beam  through  a  Fabry-Perot  interferometer.  The  remainder  of  this  chapter 
discusses  the  specifics  of  each  of  these  components. 
B.  LASER 

A  LEXEL  Model  85  continuous  wave  argon  ion  laser  (Figure  5)  is  used  for  the 
light  source.  This  model  is  a  class  3b  laser.  The  maximum  optical  power  output  was 
experimentally  determined  to  be  approximately  320  mW  in  single  mode  operation  with  a 
wavelength  of  514.5  nm. 


Figure  5a.  LEXEL  model  85  laser. 


„_ga 


-       ft* 

— •        •    * 


•  •  • 

•x    tt    m 
•    •    t 


Figure  5b.  LEXEL  model  85  power  supply. 


The  laser  has  two  operational  controls:  light  control  and  current  control.  When  the 
laser  is  operated  in  the  current  control  mode,  the  plasma-tube  current  is  maintained  at  a 
selected  level.  This  setting  provides  a  reasonably  constant  optical  power  output,  but  it 
does  not  compensate  for  any  minor  changes  in  the  optical  components,  such  as  thermal 
variations  of  cavity  length,  during  operation.  This  can  result  in  fluctuations  in  the  optical 
power  output.  When  the  laser  is  operated  in  the  light  control  mode,  a  small  portion  of  the 
laser's  output  is  sampled  by  a  beamsplitter  inside  the  front  of  the  laser  head.  This  sampled 
light  is  detected  by  a  silicon  photocell,  and  an  electrical  voltage  proportional  to  the 


X 


intensity  of  the  light  is  fed  back  to  a  regulatory  circuit.  A  differential  amplifier  in  the 
regulator  compares  this  voltage  with  a  reference  voltage  that  is  set  by  the  light  control 
potentiometer,  and  an  error  signal  proportional  to  the  difference  between  the  two  is 
generated.  The  error  signal  is  amplified  to  drive  the  power  transistors  in  the  regulator 
passbank,  causing  them  to  increase  or  decrease  the  plasma-tube  current  as  required  to 
maintain  the  output  beam  at  a  constant  output  power  [2].  In  light  control  mode,  the 
plasma-tube  current  may  vary  considerably.  In  general,  the  light  control  provides  a  very 
steady  optical  power  output  that  is  considerably  more  stable  than  that  provided  by  current 
control  mode. 

The  laser  output  was  experimentally  confirmed  to  be  linearly  polarized  with  the 
electric  field  in  the  vertical  direction,  that  is,  perpendicular  to  the  optical  table.  The  beam 
diameter  was  experimentally  determined  to  be  approximately  1.2  mm  (Figure  6).  This  was 


-0  5  0.0  0.5 

Position    (mm    ) 


Figure  6.  Plot  of  laser  beam  power  as  a  function  of  transverse  position.  Beam  profile  is  approximately 
Gaussian  with  a  width  of  approximately  1.2  mm. 


done  by  painting  one  side  of  a  microscope  slide  flat  black  and  then  scoring  a  slit  in  the 
paint  with  a  razor  blade  and  straight  edge.  The  slit  was  then  passed  through  the  beam  and 


back  again  both  in  a  direction  parallel  to  the  table  and  a  direction  perpendicular  to  the 

table.  Measurements  of  position  were  recorded  using  a  micrometer  tool.  This  provided 

four  sets  of  data  with  which  to  plot  position  versus  optical  power.  An  average  of  the  four 

sets  of  data  is  plotted  in  Figure  6.  The  laser  specifications  list  the  beam  diameter  as  1. 1 

mm. 

C.  MODULATOR 


Figure  7.  LM0202P  Electro-optic  modulator.  The  input  aperture  is  3  x  3  nun  square.  A  Brewster  cube  is 
mounted  to  the  exit  end.  Microdot  connectors  are  used  to  apply  voltage. 


A  Gsanger  model  LM0202P  intensity  modulator  was  used  to  amplitude  modulate 
the  continuous  wave  laser  beam  source.  The  LM0202P  takes  advantage  of  the  linear 
electro-optical  phenomenon  known  as  the  Pockels  effect.  This  effect  is  a  temporary  double 
refraction  induced  in  many  solids  by  application  of  an  electric  field.  The  applied  electric 
field  causes  a  shift  in  the  material's  anisotropic  index  of  refraction  which  in  turn  causes  a 
modification  of  the  relative  phases  of  different  polarization  modes.  Controlling  the 
polarization  of  the  laser  light  electronically  can  lead  to  amplitude  modulation  when  the 
resulting  beams  traverse  polarizing  elements.  The  LM0202P  has  a  Brewster  cube  attached 
to  the  exit  end  of  the  modulator  which  is  the  single  polarizing  element  necessary  as 
analyzer. 


10 


The  LM0202P  uses  four  KDP  crystals,  in  series  optically  and  in  parallel 
electrically.  The  crystals  must  be  oriented  in  a  particular  position  relative  to  incident 
polarized  light  in  order  for  proper  amplitude  modulation  to  occur.  Consider  a  standard  x, 
y,  z  coordinate  system  where  z  is  in  the  direction  of  propagation  of  the  laser  beam  and  x,  y 
are  oriented  along  the  crystal's  principle  axes.  If  an  electric  field  is  applied  along  the  z  axis 
of  the  crystals,  then  the  x,  y  optical  axes  are  rotated  to  a  new  position  x',  y\  This  changes 
the  relative  position  between  the  plane  of  polarization  of  the  light  source  and  the  optical 
crystal's  axes.  This  change  in  relative  position  causes  a  modification  in  the  phase  between 
the  two  polarization  modes  as  described  above.  When  the  electric  field  of  a  linearly 
polarized  light  source  is  oriented  45  degrees  from  the  optical  axes  of  the  crystals  and  with 
no  voltage  applied,  the  modulator  will  act  as  a  quarter  waveplate  and  change  the  linear 
polarization  to  circular. 

As  the  voltage  applied  to  the  modulator  is  increased  from  zero,  the  net  phase  shift 
between  the  two  components  will  generally  result  in  elliptically  polarized  light  due  to  the 
change  in  relative  position  between  the  plane  of  polarization  of  the  light  source  as 
described  above.  At  some  point,  the  phase  changed  induced  by  the  applied  voltage  will  be 
nil  and  the  polarization  will  once  again  become  circular.  The  Brewster  cube  splits  the  two 
components  of  the  circularly  polarized  light.  One  is  sent  in  the  same  direction  of 
propagation  but  is  now  oriented  with  its  plane  of  polarization  in  the  horizontal  direction 
parallel  to  the  optical  table.  The  other  is  sent  perpendicular  to  the  direction  of  propagation 
but  keeps  its  orientation  with  the  plane  of  polarization  in  the  vertical  direction 
perpendicular  to  the  table  (Figure  8).  When  the  voltage  applied  results  in  elliptically 
polarized  light,  the  components  are  separated  by  the  Brewster  cube  and  the  two  exiting 

11 


beams  are  unequal  in  magnitude.  If  aligned  as  described  above,  the  LM0202P  will 
therefore  change  linearly  polarized  light  into  circularly  polarized  light  with  no  voltage 
applied  and  then  again  at  some  specific  value  of  voltage.  That  value  was  experimentally 
determined  to  be  1 65  V  by  incrementally  increasing  voltage  applied  to  the  modulator  and 
recording  the  optical  power  of  each  beam  exiting  the  Brewster  cube  (Figure  9). 

There  remains  some  concern  as  to  whether  or  not  this  is  indeed  the  proper  way  to 
align  the  modulator.  It  is  evident  from  Figure  9  that  the  DC  characterization  curve  is  not 
symmetric  and  this  is  a  point  of  concern.  It  is  considered  that  the  correct  alignment  may 
possibly  be  for  maximum  transmission  in  the  perpendicular  beam  and  minimum 
transmission  in  the  forward  beam.  Nevertheless,  the  curve  in  Figure  9  was  reproducible 
time  and  time  again.  The  data  for  Figure  9  was  taken  with  68  mW  of  input  into  the 
modulator  and  30  mW  of  output  from  each  beam  exiting  the  Brewster  cube  for  an  overall 
transmission  of  approximately  88%  with  0  volts  DC.  Both  spots  were  crisp  and  clear. 

At  165  V,  the  horizontal  and  vertical  components  of  the  exiting  beam  are  equal  in 
magnitude.  The  result  is  two  perpendicular  beams  of  light  equal  in  optical  power  exiting 
the  Brewster  cube.  At  85  V,  there  is  extinction  in  the  direction  of  propagation  and 
transmission  in  the  direction  perpendicular  to  propagation.  At  255  V,  the  reverse  occurs 
with  transmission  in  the  direction  of  propagation. 

An  alternating  voltage  that  ranges  from  85  to  255  V  applied  to  the  modulator 
results  in  100%  amplitude  modulation.  A  greater  range  results  in  over-modulation  and 
distortion.  Data  taken  with  a  modulation  frequency  of  1  kHz  at  different  ranges  of  voltage 
shows  these  three  conditions  (Figure  10). 


12 


Beam  Perpendicular 
to  Propagation 


Vertically  Polarized 
Light  Source       ► 


] 


Vertically  Polarized 


Horizontally  Polarized 


Beam  in  Direction 
of  Propagation 


Figure  8.  Effect  of  Brewster  cube  at  exit  end  of  modulator. 


O 
CL 


80 


60 


40 


20 


Detector  2 


/ 


i 

\ 


\ 


/  \ 
/     \ 

.     Detector  1   /  \ 


/ 
/ 

\      /DC  Bias  Voltage  =  165  V  - 


0  50  100  150  200  250  300 

Applied  DC  Voltage  (volts) 

Figure  9.  Applied  DC  voltage  versus  optical  power  output  for  LM0202P  intensity  modulator. 


13 


(a) 


Time  (msec) 
(b) 


Figure  10.  Representative  outputs  of  modulator  at  various  voltages.  Shown  are  outputs  for  AC  voltages 
(a)  57  Vpp  (b)  165  Vpp  (c)  284  Vpp  [3], 


14 


The  electro-optical  properties  of  the  crystals  in  the  modulator  are  extremely 
temperature  sensitive.  Experimental  results  are  most  consistent  when  the  laser  is  run 
through  the  modulator  for  approximately  one  half  hour  before  any  voltage  is  applied.  It  is 
best  to  wait  nearly  that  long  again  after  applying  DC  voltage  to  allow  the  optical  output  to 
stabilize  before  applying  any  AC  voltage.  AC  voltage  causes  dramatic  thermal  fluctuations 
every  time  that  it  is  applied  to  the  modulator.  After  the  fluctuations  settle,  the  DC  voltage 
must  once  again  be  adjusted  in  order  to  obtain  circular  polarization  and  equal  magnitude  in 
the  beams  exiting  the  Brewster  cube. 
D.  ELECTRONIC  DRIVING  CIRCUIT 

The  modulator  was  initially  thought  to  act  as  a  capacitor  element.  The  capacitance 
was  measured  to  be  approximately  82  pF.  This  is  true,  however,  only  with  very  short  (half 
an  inch  or  less)  leads  to  the  pin  connections  of  the  modulator.  As  soon  as  any  connections 
at  all  were  made  between  an  electronic  driving  circuit  and  the  modulator,  inductive  loops 
were  produced  and  the  modulator  no  longer  acted  as  a  simple  capacitor.  This  problem 
proved  extremely  difficult  to  address,  and  in  the  end  an  entire  separate  thesis  was 
conducted  to  characterize  and  to  understand  the  electronic  operation  of  the  LM0202P 
modulator.  Three  separate  circuit  designs  were  constructed  and  tested  in  the  research.  A 
summary  of  each  design  and  the  results  of  the  testing  make  up  the  rest  of  this  section.  The 
third  and  final  design  was  the  one  used  to  drive  the  modulator  for  the  final  results  of  this 
thesis. 

It  was  originally  decided  to  drive  the  modulator  through  a  tuned  radio  frequency 
transformer  with  both  the  primary  and  secondary  circuits  tuned  to  the  working  frequency. 
It  turned  out,  however,  that  the  Q-factor  of  the  secondary  circuit  was  not  sufficiently  high 


15 


to  boost  the  output  voltage  to  160  Vpp,  and  it  became  necessary  to  make  use  of  a  RF 
amplifier  to  enhance  the  voltage  supplied  by  the  signal  generator.  Note  that  the 
arrangement  includes  provision  for  applying  a  DC  voltage  to  the  modulator  in  addition  to 
the  RF  voltage.  This  allows  the  adjustment  of  the  bias  voltage  to  ensure  that  the 
modulator  operated  at  the  50%  transmission  point  for  symmetrical  modulation.  The 
purpose  of  the  0.01  uF  capacitor  is  to  ensure  that  the  bottom  end  of  the  secondary  is  at  AC 
ground  while  being  at  an  elevated  DC  voltage.  The  100  kQ  resistor  protects  the  DC 
power  supply  from  an  accidental  short  circuit  [3]. 


Modulator 


RF 
Signal 
Generator 


RF 
Amplifier 


Figure  11.  Equipment  setup  for  transformer  action  [3]. 

Separate  transformers  were  wound  with  different  numbers  of  secondary  turns  to 
resonate  at  different  frequencies.  They  were  tested  with  an  82  pF  capacitor  before  being 
used  to  drive  the  modulator.  In  each  case,  the  primary  turns  were  adjusted  for  maximum 
secondary  voltage  at  resonance.  Satisfactory  results  were  obtained  up  to  20  MHz.  Above 


16 


that  frequency,  however,  a  transformer  could  not  be  used  because  the  required  number  of 
turns  in  the  primary  and  secondary  windings  was  so  low  that  there  was  a  severe  mismatch 
between  the  primary  impedance  and  the  output  impedance  of  the  amplifier.  The 
transformer  was  therefore  replaced  by  a  parallel  tuned  circuit  [3]. 


DCPwr 
Supply 


100  kD. 


-wv 


RF 
Signal 
Generator 


RF 
Amplifier 


Jl 


005fiF 


X 


Modulator 


Figure  12.  Parallel  tuned  circuit  [3]. 

The  resonant  frequency  of  the  parallel  tuned  circuit  was  varied  through  proper 
selection  of  the  inductor  with  or  without  a  parallel  capacitor.  The  equipment  setup,  with 
appropriate  RF  screening  methods,  remained  the  same  as  that  used  for  lower  frequencies 
which  made  use  of  a  transformer.  The  0.0050  uF  capacitor  provides  an  AC  ground  while 
allowing  the  use  of  the  DC  bias.  The  100  kO  resistor  is  present  again  to  protect  the  DC 
power  supply  from  an  accidental  short  circuit.  The  RF  amplifier  with  a  maximum  power 
output  of  4  W  (into  a  50  Q  load)  could  not  supply  a  voltage  greater  than  40  Vpp  to  the 
parallel  tuned  circuit  [3]. 


17 


A  third  arrangement  was  developed  where  the  DC  and  RF  voltages  were  both 
supplied  through  the  same  coaxial  cable  with  the  help  of  a  hybrid  circuit.  The  hybrid 
circuit  could  drive  the  modulator  through  a  coaxial  cable  connected  to  one  of  the  SMC 
connectors  on  the  modulator,  with  the  other  SMC  connector  grounded.  This  arrangement 
precluded  the  use  of  an  inductor  to  resonate  with  the  crystal  capacitor.  Nor  did  it  make  it 
possible  to  measure  and  regulate  the  RF  voltage  at  the  modulator  terminals  so  as  to 
determine  the  true  frequency  response  of  the  modulator.  But  it  did  eliminate  the  inductive 
loop  in  the  external  open  connections  to  the  modulator  [3]. 


(a) 


• 

RF  Signal 
Generator 

RF 

nyuuu 

Ivr 

1                1 

Amplifier 

DC  Power 
Supply 

Modulator 

(b) 


From  RF  Amplifier 


C, 


R 


H 


To  Modulator 


X_Q 


From  DC  Power  Supply 


Figure  13.  Setup,  (a)  Equipment  set-up  with  no  RF  voltage  monitoring.  Connections  between  components 
are  via  coaxial  cable,  (b)  Close  up  of  hybrid  connector,  d  =  0.01  u.F  500V,  C2and 
C3  =  0.0047  u.F  500V,  R  =  100  kQ.  1/2  W,  L  -  RF  choke  1  uH  [3]. 


18 


E.  DETECTORS  AND  POWER  METERS 

A  Coherent  Model  205  power  meter  and  sensor  is  used  to  determine  the  maximum 
optical  power  output  of  the  laser  and  for  start-up  each  time  the  laser  is  used.  It  is  mounted 
to  the  table  such  that  it  can  be  easily  swung  in  front  of  the  laser  to  act  as  a  "laser  light 
dump"  while  adjustments  are  being  made.  The  sensor  is  a  thermal  disc  whose  maximum 
intensity  rating  is  200  W/cm2.  The  response  time  of  this  detector  is  less  than  one  second. 

Two  identical  detectors  with  power  meters  are  used  to  measure  the  optical  power 
output  of  the  perpendicular  beams  from  the  Brewster  cube  at  the  end  of  the  modulator. 
These  are  Newport  model  815  power  meters  and  model  818-SL  detectors.  The  detectors 
each  have  a  neutral  density  filter  of  density  factor  3,  which  allows  for  input  up  to  2  W/cm2. 
The  power  meters  also  have  an  output  connection  that  allows  the  signal  to  be  sent  to  an 
oscilloscope.  In  this  way,  the  peak-to-peak  amplitude  modulation  can  be  measured 
accurately. 


SQ0 

i           '           I           •           I           i           i           i           I 

400 

-                   y      - 

S 

slope  =  9.85                   yS 
sd  =  0.04             /* 

t    300 

/ 

Voltage 

■         /                        [ 

100 

-     y7 

n 

x 

20  30  40 

Power  (rriW) 


Figure  14.  Response  curve  for  Newport  detector.  The  voltage  is  measured  with  an  oscilloscope  from  the 
analog  output  of  the  detector.  Power  is  controlled  via  the  laser  power  supply. 


19 


The  Newport  detectors  use  a  silicon  diode  with  a  rise  time  of  2  u,s.  This  leads  to  a 
theoretical  maximum  response  time  of  500  kHz.  Beyond  500  kHz,  the  detectors  can  only 
be  used  as  power  meters  because  they  effectively  average  the  time-varying  incident  flux. 

A  series  PD30  ultra  high  speed  photodetector  with  PS30  power  supply  from  Opto- 
Electronics  Incorporated  is  used  for  experiments  at  frequencies  above  100  kHz.  The 
detector  was  experimentally  tested  for  accurate  response  up  to  250  MHz.  It  uses  an 
avalanche  silicon  photodiode  with  a  rating  of  100  mW  of  average  optical  power.  The 
detector  is  designed  for  use  with  the  power  supply  operating  at  approximately  1 00  u,A  of 
bias  current,  where  the  diode  current-voltage  curve  is  approximately  linear  with  a 
maximum  power  supply  current  of  200  uA.  As  Figure  1 5  shows,  experimental  data  taken 
with  1 00  uA  of  current  through  the  power  supply  exhibits  an  approximately  linear 
behavior. 

Detector  3  Calibration  Curve 


Intensity  (mW) 


Figure  15.  Calibration  curve  for  PD30  ultra  high  speed  photodedector.  Throughout  the  experimental 

work,  this  detector  was  referred  to  as  detector  three.  The  Newport  detectors  were  designated 
as  one  and  two. 


20 


A  microscope  slide  is  used  to  reflect  a  fraction  of  the  modulated  beam  into  the  high 
speed  detector.  A  device  was  constructed  to  aim  the  reflected  beam  into  the  small  aperture 
of  the  detector.  The  microscope  slide  is  hung  from  an  arm  that  is  attached  to  a  control  that 
allows  for  precise  rotation  of  the  arm  (Figure  16).  This  rotates  the  slide  in  a  plane 
perpendicular  to  the  table  and  adjusts  the  reflection  vertically  up  and  down  along  the  face 
of  the  detector.  This  rotation  stage  with  the  attached  arm  is  mounted  to  a  post  that  fits  in  a 
holder  which  allows  the  post  to  rotate  which  in  turn  rotates  the  slide  parallel  to  the  table. 
This  provides  adjustments  of  the  reflection  horizontally  from  side  to  side  along  the  face  of 
the  detector.  The  device  is  braced  to  reduce  vibrations,  and  neoprene  spacers  are  used  to 
dampen  vibrations  in  order  to  maintain  a  steady  reflection  from  the  slide. 


Figure  16.  Microscope  slide  reflector. 
F.  ALIGNMENT 

As  in  any  optical  set-up,  the  key  to  success  with  this  experiment  is  careful 
alignment.  The  laser  sits  on  two  large  lab  jacks  which  provide  initial  macroscopic  changes 
in  the  height  and  tilt  of  the  beam.  The  modulator  and  fiber  optic  coupler  mount  to  a  rail 
which  is  fixed  to  the  table  in  front  of  the  laser  with  the  center  line  parallel  to  the  beam. 


21 


Each  component  on  the  rail  can  be  removed  and  replaced  at  any  time.  Most  of  the  optical 
mounts  are  combinations  of  New  Focus  and  Newport  equipment. 

A  New  Focus  Model  9082  five-axis  aligner  is  used  for  the  base  support  of  the 
modulator  in  order  to  align  the  beam  through  the  tube.  Four  of  the  adjustments  combine 
for  tilt  or  pivot  about  the  center  of  the  base  and  also  translation  vertically  or  horizontally 
perpendicular  to  the  beam.  The  fifth  adjustment  allows  for  horizontal  translation  parallel  to 
the  beam  and  is  not  actually  necessary.  A  mounting  had  to  be  designed  that  would  both 
hold  the  modulator  fixed  on  the  five-axis  aligner  and  that  would  allow  azimuthal  rotation 
about  the  long  axis  of  the  modulator. 

A  plastic  tubular  sleeve  was  fitted  over  the  modulator.  A  second  sleeve  of  shorter 
length  was  then  fitted  over  the  first  sleeve.  This  allowed  end  ring  clamps  to  be  used  to 
both  tighten  the  inside  ring  snugly  against  the  modulator  and  to  prevent  the  inner  tube 
from  moving  longitudinally  relative  to  outer  tube.  The  modulator  is  rotated  by  grasping  an 
end  ring  and  rotating  that  ring  which  results  in  the  rotation  of  also  the  inner  sleeve  and 
modulator.  There  is  sufficient  friction  between  the  inner  and  the  outer  sleeve  to  hold  the 
modulator  in  place  after  rotation  is  complete  and  the  desired  position  is  established. 

The  plastic  sleeves  had  to  be  drilled  with  several  holes  to  allow  for  cooling  of  the 
modulator.  The  modulator  is  encased  in  aluminum  to  help  minimize  thermal  effects  that 
would  cause  the  crystals  to  expand  and  contract,  thereby  changing  the  optical  path.  A  fan 
was  used  to  blow  air  across  the  modulator  and  this  air  was  able  to  reach  the  aluminum 
casing  through  the  drilled  holes. 


22 


Locking 
Ring 


Modulator 


Locking  Ring 


Inner  Ring 


Modulator 


Locking 
Screw 


Figure  17a.  Exploded  view  of  mounting  for  azimuthal  rotation  about  the  long  axis  of  the  modulator. 


Figure  17b.  Photographs  of  modulator  fixed  to  complete  alignment  mounting.  Left:  entrance  end  of 
modulator  with  ground  connection.  Right:  exit  end  of  modulator  with  Brewster  cube. 


The  next  challenge  in  the  alignment  process  was  the  mounting  for  the  fiber  optic 
cable.  The  laser  beam  is  focused  into  the  fiber  optic  cable  with  a  microscope  objective 
lens.  It  is  critical  that  the  beam  hit  the  aperture  of  this  lens  on  center  and  perpendicular  to 
the  lens.  The  height  of  the  beam  is  fixed  once  alignment  through  the  modulator  is 
established.  Therefore,  it  is  required  to  make  the  mounting  for  the  objective  lens  such  that 


23 


the  center  of  the  lens  can  be  physically  moved  into  the  beam  while  allowing  alignment  that 
is  also  perpendicular  to  the  beam. 

The  mounting  that  is  used  for  the  microscope  objective  lens  is  a  Newport  F-916 
series  fiber  coupler.  The  fiber  coupler  attaches  to  a  Newport  base  that  allows  for  small 
adjustments  either  in  the  tilt  or  pivot  (two-axis  alignment)  of  the  lens  compared  to  the 
beam,  but  not  for  translation  vertical  or  parallel  to  the  table.  The  Newport  base  was 
replaced  with  a  New  Focus  model  9071  four-axis  aligner  to  allow  vertical  and  horizontal 
translation  as  well  as  tilt  and  pivot.  A  spacer  was  fabricated  to  place  the  fiber  coupler  in 
the  approximately  correct  position  and  was  also  utilized  to  connect  the  mechanically 
incompatible  Newport  and  New  Focus  parts. 


Figure  18.  Newport  fiber  coupler  with  New  Focus  four-axis  aligner  attached  to  rail. 

The  final  and  most  interesting  alignment  challenge  came  in  directing  the  beam 
through  the  Fabry-Perot  interferometer.  A  second  device  similar  to  the  one  described 
previously  for  holding  the  microscope  slide  (Figure  16)  was  built.  Mirrors  were  attached 
to  the  arms  of  each  device.  The  beam  was  reflected  from  one  mirror  to  the  other  and 


24 


through  the  interferometer.  By  simultaneously  adjusting  both  mirrors,  the  height  and  slope 
of  the  beam  as  well  as  the  horizontal  path  of  the  beam  were  easily  controlled.  In  this 
manner,  the  beam  was  directed  through  the  center  of  the  Fabry-Perot  and  perpendicular  to 
its  optical  elements. 
G.  FABRY-PEROT  INTERFEROMETER 

A  Tropel  model  360  Fabry-Perot  interferometer  and  Tropel  model  361  Fabry- 
Perot  controller  were  used  in  the  experiments.  The  Fabry-Perot  interferometer  is  a 
multiple-beam  interferometer.  The  two  glass  plates  that  make  the  etalon  spacing  are 
coated  on  the  inner  surfaces  such  that  an  incoming  wave  is  reflected  many  times  between 
the  two  surfaces.  An  interference  pattern  is  produced  as  in  two-beam  interference; 
however,  as  the  number  of  interfering  beams  increases  by  reflections  back  and  forth  in  the 
etalon,  the  fringes  become  sharper.  With  a  monochromatic  broad  diffuse  source,  the 
interference  fringes  will  be  narrow  concentric  rings,  corresponding  to  the  multiple  beam 
transmission  pattern.  The  position  of  the  fringes  depends  upon  the  wavelength.  That  is, 
each  wavelength  gives  a  separate  fringe  pattern  [4]. 

The  Fabry-Perot  interferometer  can  be  used  to  resolve  very  close  wavelengths  into 
separate  fringe  patterns.  The  resolving  power  is  determined  by 


(2nd\ 
*  =  <— J,        (2.D 


where  F  -  ;zR/(l-R)  is  known  as  the  finesse,  n  is  the  refractive  index  between  the 
mirrors,  d  is  the  distance  between  the  mirrors,  and  R  is  the  reflection  coefficient  of  the 
mirrors.  For  nd  of  10  cm,  R  of  .9  and  X  of  514.5  nm,  the  resolving  power  is  on  the  order 
oflO7. 


25 


26 


m.  LASER  OUTPUT  SPECTRUM  AND  SEARCH  FOR  AM  SIDEBANDS 

A.  OUTPUT  SPECTRUM  OF  LEXEL  85  ARGON  ION  LASER 

To  determine  the  frequency  structure  of  the  laser,  the  Fabry-Perot  interferometer  is 
illuminated  with  a  collimated  laser  beam,  and  all  the  light  transmitted  through  the  Fabry- 
Perot  is  focused  on  a  detector,  whose  output  is  displayed  on  an  oscilloscope.  One  of  the 
two  etalon  plates  is  on  a  piezoelectric  mirror  mount.  As  the  voltage  to  the  piezoelectric 
crystal  is  varied,  the  etalon  separation  is  varied  The  light  output  as  a  function  of  plate 
separation  gives  the  spectral  frequency  content  of  the  laser  source  [4]. 

One  of  the  Newport  model  815-SL  detectors  was  used  with  a  Hewlett-Packard 
model  3  5670  A  Dynamic  Signal  Analyzer  to  record  the  spectral  frequency  content  of  the 
LEXEL  model  85  argon  ion  laser.  Figures  19-28  present  plots  of  detector  voltage  versus 
frequency  for  the  data  collected.  Both  scales  are  relative.  The  frequency  difference 
between  corresponding  portions  of  the  line  profile  in  neighboring  spectral  orders  is 
calculated  from  the  measured  etalon  spacing.  That  is,  the  free  spectral  range  is 

FSR=^     ,       (3.1) 

where  n  is  the  refractive  index  of  air  and  d  is  the  etalon  spacing.  The  measurementst  were 
done  with  an  etalon  spacing  of  approximately  9.32  cm,  the  free  spectral  range  is 
approximately  1.61  GHz.  This  value  can  be  used  to  interpolate  each  profile's  frequency 
structure  from  the  plots.  Figures  19  and  20  of  this  section  show  plots  of  the  laser 
spectrum,  unaffected  by  any  other  optics 

It  is  evident  form  these  plots  that  the  output  of  the  laser  is  certainly  not  single 


27 


I.VJ 

0.9 

— •■  ■          i           ■           i 

0.8 

. 

0.7 

0.6 

|Q5 

^   0.4 

;    | 

i 

0.3 

I 

i 

0.2 

\ 

ft 

0.1 

I             J 

l^ 

0.0 

i                      i 

0.0 


0.5 


1.0 


Frequency 


Figure  19.  Scan  of  entire  free  spectral  range  from  laser.  Variations  from  order  to  order  are  artifices  of 
discrete  sampling  by  the  Hewlett-Packard  analyzer. 


Figure  20.  Detail  of  unmodulated  line  profile  directly  from  laser. 


28 


mode.  The  laser  line  profile  typically  shows  three  simultaneous  modes  with  a  spacing  of 
approximately  50  MHz.  This  profile  was  observed  continuously  for  several  hours  and 
appears  to  be  relatively  stable  in  time.  Therefore,  any  search  for  modulator-induced  effects 
must  assume  this  complicated  laser  line  structure  as  a  base. 
B.  EFFECT  OF  LM0202P  MODULATOR  ON  LASER  SPECTRUM 

Insertion  of  the  modulator  into  the  optical  path  of  the  beam,  with  no  voltage 
applied  to  the  modulator,  caused  a  dramatic  change  in  the  spectrum.  Additional  structure 
was  added  to  the  base  line  structure  and  the  valleys  between  the  three  original  modes  were 
filled.  As  DC  bias  voltage  was  applied  to  the  modulator,  additional  spectral  changes  were 
noticeable.  Examples  are  presented  in  Figures  21-24.  This  makes  the  base  profile  even 
more  complex,  and  complicates  the  search  for  AM  sidebands. 


1.0  f r 


0.8  - 


0.6  - 


TO 

>    0.4 


0.2 


i ■ 1 ■ 1 > 1 > r 


0.0  L L 


0.0  0.1  0.2  0.3  0.4  0.5 

Frequency 

Figure  21.  Spectrum  exiting  modulator  with  40  volts  DC  bias  applied  to  modulator 


29 


1.0 

1 

r         ■          i         ■         i          ' 

I         '         i       ■- 

08 

• 

• 

0.6 

" 

Voltage 

o 

— 

~ 

0.2 

- 

- 

■     A       j 

v ■ 

0.0 

i        .        i        .        i        .        i 

I.I- 

0.0 


0.1  0.2  0.3  0.4  0.5 

Frequency 


Figure  22.  Spectrum  exiting  modulator  with  80  volts  DC  bias  applied  to  modulator. 


1.0 

-           !             i    ■     ■■ 

■ 

i    •    i    - 

0.8 

- 

0.6 

Voltage 

o 

;        i 

1 

- 

0.2 

. 

, 

- 

i 

V       A 

0.0 

i —  .    i    .    i    .    i    .    i    . 

0.0  01  0.2  0.3  0.4  0.5 

Frequency 


Figure  23.  Spectrum  exiting  modulator  with  100  volts  DC  bias  applied  to  modulator. 


30 


1.0 
0.8 

_■■■    1         1 

■         1         •         1         1 

i       '       i      - 

■ 

0.6 

Voltage 

o 

■ 

• 

0.2 

- 

■  _J 

I      A 

0.0 

1          .         1          .         1          .         1          .          1          .         1        - 

0.0 


0.1 


0.2 


0.3 


0.4 


0.5 


Frequency 
Figure  24.  Spectrum  exiting  modulator  with  180  volts  DC  bias  applied  to  modulator. 

C.  SEARCH  FOR  AM  SIDEBANDS 

Finally,  AC  modulation  was  superimposed  on  the  DC  bias  voltage.  This  yielded 
evidence  of  complicated  sideband  structure  (Figures  25-28).  However,  the  observed 
structure  did  not  look  as  expected,  even  when  the  complicated  base  line  profile  discussed 
above  was  taken  into  account.  The  modulated  profiles  are  difficult  to  decipher  and  seem 
to  make  little  sense:  For  instance,  it  is  known  that  the  modulator  produces  a  nice 
sinusoidal  amplitude  modulation,  as  verified  directly  with  an  oscilloscope.  This  modulation 
should  produce  a  single  symmetric  pair  of  sidebands.  However,  it  is  evident  from  Figures 
25-28  that  the  sideband  distribution  is  asymmetric.  At  the  time  of  this  writing,  both  the 
cause  of  the  asymmetry  and  the  overall  modulated  profile  are  not  well  understood. 
Extensive  follow-on  research  will  be  required  to  address  these  issues. 


31 


1.0  f r 


0.8 


0.6 


|5 

>     0.4 


0.2 


1—1 ' 1 "- 


0.0 


-> r 


0.1 


0.0  t I i I . I i L 


0.2  0.3 

Frequency 


0.4 


0.5 


Figure  25.  Spectrum  modulated  at  125  MHz  with  20  volts  DC  bias  applied  to  the  modulator  and  a 
superimposed  AC  amplitude  of  unknown  value,  resulting  in  a  measured  25  %  optical 
modulation. 


o.o 


0.1 


0.2  0.3 

Frequency 


1.0 
0.8 

I '  "  ' — 1 T 

i              ■              1              ■              l 

'          I 

0.6 

I 

I                                 1 

i 

■2 

■ 

1 

>    0.4 

y 

\ 

1 

1 

0.2 

\ 

K 

j 

V____/ 

\^ 

0.0 

-     L.           .              1              . 

I.I.I 

i      - 

0.4 


0.5 


Figure  26.  Spectrum  modulated  at  125  MHz  with  180  volts  DC  bias  applied  to  the  modulator  and  a 
superimposed  AC  amplitude  of  unknown  value,  resulting  in  a  measured  25  %  optical 
modulation. 


32 


1.0  f r 


0.8 


0.6 


% 


■s 

>    0.4   - 


0.2   - 


0.0  l= L 


0.1 


0.2  0.3 

Frequency 


Figure  27.  Spectrum  modulated  at  36  MHz  with  0  volts  DC  bias  applied  to  the  modulator  and  a 
superimposed  AC  amplitude  of  unknown  value,  resulting  in  a  measured  63%  optical 
modulation. 


o.o 


0.1 


0.2  0.3 

Frequency 


Figure  28.  Spectrum  modulated  at  36  MHz  with  170  volts  DC  bias  applied  to  the  modulator  and  a 
superimposed  AC  amplitude  of  unknown  value,  resulting  in  a  measured  63%  optical 
modulation. 


33 


34 


IV.  FIBER  OPTIC  COUPLING 

A.  INTRODUCTION 

There  are  three  primary  considerations  to  effectively  launch  a  collimated  light 
source  down  a  fiber  optic  cable.  The  first  is  to  focus  the  beam  to  form  a  cone  of  specific 
size  and  shape.  The  second  is  to  properly  cleave  the  end  of  the  optical  fiber  so  that  it  is  flat 
and  perpendicular  without  any  cracks  in  the  glass.  The  third  is  to  position  the  center  of  the 
end  of  the  optical  fiber  at  the  focal  point,  which  is  the  apex  of  the  cone.  These  three  steps 
combine  to  allow  the  full  cone  of  light  to  enter  and  propagate  down  the  optical  fiber  with 
minimum  insertion  loss.  These  three  primary  considerations  make  up  the  discussion  of  this 
section. 

It  is  necessary  to  focus  the  beam  in  order  to  launch  it  down  a  fiber  optic  cable.  The 
beam  profile  exiting  the  modulator  was  measured  in  the  same  manner  as  described 
previously  for  the  laser  beam  diameter.  It  was  found  that  the  beam  profile  spread  in  width 
by  approximately  one  half  centimeter  in  passing  through  the  modulator,  that  is,  the 
diameter  of  the  beam  exiting  the  modulator  was  experimentally  determined  to  be 
approximately  1.7  mm  (Figure  29). 


•1.5  -1.0 


-OS  00  OS 

Position  (  mm    ) 


Figure  29.  Plot  of  laser  beam  power  versus  transverse  position.  The  beam  width  is  approximately  1.7  mm. 


35 


A  500  m  communications  grade  optical  fiber  with  a  numerical  aperture  of  0.29  is 
used  in  the  experiment.  The  first  step  is  to  determine  the  lens  characteristics  necessary  to 
focus  the  beam.  This  calculation  is  dependent  on  the  diameter  of  the  laser  beam  and  the 
numerical  aperture  of  the  fiber  optic  cable.  If  ni  is  the  index  of  refraction  of  the  core  and 
n2  is  the  index  of  refraction  of  the  cladding,  the  numerical  aperture  is 


NA  =    V".2-»22   •    (4-1) 
The  numerical  aperture  is  related  with  the  ability  of  the  fiber  to  guide  rays.  An 
optical  ray  is  guided  by  total  internal  reflections  within  the  fiber  core,  provided  that  the 
angle  of  incidence  on  the  core-cladding  boundary  is  greater  than  the  critical  angle 
0c  =  sin"1(n2/ni),  measured  with  respect  to  the  normal  at  the  core-cladding  interface 
(Figure  30).  Thus,  for  a  ray  incident  from  air  into  a  fiber  to  become  guided,  the  angle  0  it 
makes  with  the  fiber  axis  must  be  smaller  than  the  complementary  angle  for  total  internal 
reflection  0c.  At  the  air-core  boundary,  the  angle  0o  in  air  corresponding  to  7t/2-0c  in  the 
core  is  given  by  Snell's  Law 


sin(0o)  =  nisin(7c/2-0c)  =  nicos(0c) , 


(4.2) 


By  using  the  value  for  0c,  we  find 


sin(0o)  =  ni 


(     V 
Ik 

\Vi\J 


~     Vni2-n2 


(4.3) 


Therefore, 


0o  =  sin^A)  .         (4.4) 


36 


air 


IE       cladding 


ni       core 


nj cladding 


Figure  30.  Light  ray  diagram  for  a  step-index  fiber  optic  cable. 

Equation  (4.4)  defines  a  cone  of  angles  that  the  fiber  can  accept  for  propagation.  Thus,  a 
focused  beam  within  the  cone  determined  by  Go  will  be  guided  (Figure  31). 


Laser  Light 


Lens 


focal  length 


[    N  ]      ^^^^^Q" 


Fiber  Optic  Cable 


Figure  31.  Focusing  a  collimated  light  source  into  a  fiber  optic  cable. 


From  the  trigonometry  of  the  above  drawing  tan(0o)  =  (^d)  /  f,  where  d  is  the 
diameter  of  the  laser  beam  and  f  is  the  focal  length  of  the  lens.  Thus,  the  focal  length  of 
the  lens  necessary  to  launch  the  laser  light  down  the  fiber  optic  cable  is 

d 


f* 


2tan[siiT,(M4)] 


(4.5) 


37 


For  a  numerical  aperture  of  0.29  and  a  laser  beam  diameter  of  1.7  mm,  equation 
(4.5)  yields  a  focal  length  of  approximately  2.8  mm.  A  focal  length  slightly  higher  than 
this  should  be  used  to  allow  for  losses  at  bends  in  the  optical  fiber. 

Typical  microscope  objective  lenses  are  labeled  with  two  numbers  corresponding 
to  magnifications  and  numerical  apertures.  The  overall  magnification  of  a  microscope  is 
the  product  of  the  linear  magnification  of  the  objective  multiplied  by  the  angular 
magnification  of  the  eyepiece  when  viewing  the  final  image  at  infinity  [5].  It  is  difficult  to 
determine  the  exact  focal  length  of  most  microscope  objective  lenses  with  only  the 
information  stamped  on  them. 

Table  1  shows  approximate  values  of  focal  lengths  for  several  common  microscope 
objectives.  These  values  should  be  treated  only  as  a  general  guide  since  precise  values  vary 
slightly  from  lens  to  lens  and  manufacturer  to  manufacturer. 


4x 

42.50  mm 

lOx 

17.00  mm 

20x 

8.50  mm 

40x 

4.25  mm 

60x 

2.80  mm 

lOOx 

1.70  mm 

Table  1.  Approximate  values  of  focal  lengths  for  several  common  microscope  objectives. 

Without  a  well  prepared  end  it  will  be  impossible  to  get  a  good  launch  down  a 
fiber.  The  cleaved  end  must  be  examined  under  a  microscope  to  be  sure  the  face  is  flat, 
perpendicular  to  the  fiber,  and  that  there  are  no  cracks  in  the  glass.  The  best  way  to  obtain 
a  good  cleave  is  with  a  sharp  razor  blade  or  specialized  tool  designed  for  this  purpose.  A 
small  score  is  made  in  the  fiber  and  tension  is  then  applied  from  both  ends  to  break  the 


38 


glass  with  a  clean  surface.  The  process  requires  applying  the  slightest  pressure  to  score  the 
fiber  while  simultaneously  pulling  on  the  fiber  with  the  other  hand.  Figure  32  shows  what 
a  typical  cleaved  end  will  look  like  under  a  microscope. 


C 


Lip 


Scribe  Mart  /"  *V»— 7  &**&  running 

'  into  the  core 


<a»  <b)  (c) 

Figure  32.  Cleaved  fiber  ends,  (a)  Good  cleave,  (b)  Cracked  fiber,  (c)  Side  view  of  a  lip.  [6] 

Once  a  lens  is  selected  and  in  position,  and  the  end  of  the  optical  fiber  is  prepared, 
the  final  step  is  to  position  the  end  of  the  fiber  at  the  focal  point  of  the  lens.  Newport 
makes  a  fiber  positioner  that  is  designed  for  this  purpose.  The  end  of  the  fiber  optic  cable 
slides  into  a  slotted  metal  cylinder  and  a  metal  filler  slides  in  behind  the  fiber  to  hold  it  in 
place.  The  cylinder  then  slides  into  a  mounting  that  allows  for  3 -axis  movement.  The 
directions  of  movement  are  parallel  to  the  beam,  perpendicular  to  both  the  beam  and  the 
table,  and  perpendicular  to  the  beam  but  parallel  to  the  table. 


Figure  33.  Fiber  Optic  Positioner  with  Cylinder  to  Hold  Fiber  in  Place. 


39 


One  of  these  positioners  mounts  to  the  back  end  of  the  fiber  optic  coupler.  The  positioner 
allows  for  extremely  fine  adjustments  in  the  three  different  directions  and  in  this  way  the 
fiber  can  be  positioned  precisely  for  propagation  of  the  light  down  the  cable. 
B.  ATTENUATION 

If  a  beam  of  power  P;  is  launched  into  one  end  of  a  fiber  optic  cable,  and  if  Pf  is  the 
power  remaining  after  a  length  L  (in  kilometers)  has  been  traveled,  then  the  attenuation  in 
db/km  is  given  by 


Attenuation  = (4.6) 


Optical  transmission  loss  (attenuation)  in  fibers  is  wavelength-dependent.  The  two 
primary  loss  mechanisms  intrinsic  to  fibers  are  absorption  bands  of  the  material  and 
scattering  from  inhomogeneities  in  the  refractive  index  of  the  fiber.  The  inhomogeneities 
are  due  to  thermal  fluctuations  when  the  fiber  is  in  the  molten  state  and  to  impurities  in  the 
glass.  As  the  fiber  solidifies,  these  fluctuations  cause  variations  in  the  index  of  refraction. 
If  the  scale  of  these  variations  is  of  the  order  of  X/\0  or  less,  each  irregularity  acts  as  a 
point  source  Rayleigh  scattering  center  [7].  Absorption  losses  are  mainly  from  the 
presence  of  impurities  in  the  fiber  material.  A  graph  depicting  the  attenuation  versus 
wavelength  from  0.7  urn  to  1.6  \im  of  a  typical  silica-based  optical  fiber  is  shown  below  in 
Figure  34. 

Most  of  the  success  in  reducing  attenuation  has  come  from  better  control  of 
impurity  concentrations.  The  only  real  impurity  of  consequence  that  remains  in  optical 
fibers  of  today  is  water  in  the  form  of  (OH ")  radicals.  The  absorption  bands  for  (OH  ") 
are  at  950,  1250,  and  1380  nm  [7].  Outside  of  these  absorption  bands,  Rayleigh  scattering 

40 


is  the  dominant  loss  mechanism.  Quality  fibers  are  sometimes  characterized  by  how  closely 
they  approach  the  Rayleigh  scattering  limit  [6].  An  extrapolation  of  the  Rayleigh  scattering 
from  Figure  34  to  lower  wavelengths  is  shown  in  Figure  35. 


',.    ,f,-.iv.s:.    ■;.    ' 


rj;  ■        '<■:.  •"■■....<'..••  '  ■'\.]-  "•.  "  >• 


Figure  34.  Attenuation  of  an  optical  fiber  as  a  function  of  wavelength  [6]. 


so 

40 
30 
20 
10 

■:■•■•••••• 

1 

.     \ 

T3 

\ 

1 
1 

400  450  500  550 

Wavelength   (nm    ) 


Figure  35.  Extrapolated  Rayleigh  scattering  curve. 


41 


Attenuation  for  the  500  m  of  optical  fiber  was  measured  to  be  approximately  23 
dBkm"1  with  a  P;  of  30  mW  and  a  Pf  of  2.8  mW.  An  objective  lens  of  40  times  with  a  focal 
length  of  4.3  mm  was  used  to  focus  the  laser  beam.  The  experimental  value  of  23  dbkm"1 
is  near  the  Rayleigh  limit  of  approximately  20  dBkm"1  which  can  be  deduced  from  Figure 
35  for  a  wavelength  of  514.5  nm. 


42 


V.  CONCLUSIONS  AND  RECOMMENDATIONS 

The  primary  objectives  of  this  thesis  research  were  outlined  at  the  end  of 
Chapter  I.  The  results  of  the  research  are  briefly  summarized  here. 

Attenuation  of  green  light,  such  as  the  514.5  nm  argon  ion  laser  output,  in  a  silica- 
based  optical  fiber  is  approximately  20  dB/km  due  to  Rayleigh  scattering.  This  means  that 
the  optical  power  output  of  the  laser  must  be  increased  in  order  to  have  an  appreciable 
amount  of  light  at  the  end  of  a  long  length  of  fiber.  Because  of  this  requirement, 
experiments  with  the  modulator  were  conducted  with  a  significant  amount  of  optical 
power,  on  the  order  of  60  mW.  The  modulator  did  not  perform  as  well  as  specified  by  the 
manufacturer  when  confronted  with  this  load  of  optical  power.  Further  tests  are  required 
to  determine  if  the  behavior  of  the  modulator  is  primarily  a  result  of  high  optical  power 
input,  an  electrical  or  electro-optical  problem,  or  some  other  effect. 

Once  it  is  warm,  the  laser  produces  a  very  stable  spectral  output  However,  it  does 
not  produce  a  single  mode,  monochromatic  spectral  line.  When  the  laser  is  directed 
through  the  modulator,  the  structure  on  the  laser  profile  tends  to  blur.  That  is,  the  valleys 
in  the  spectral  profile  become  filled,  indicating  that  additional  spectral  structure  is  being 
injected  by  the  modulator.  This  effect  increases  when  DC  bias  voltage  is  applied  to  the 
modulator.  Additionally,  when  the  modulator  is  driven  with  an  AC  modulation 
superimposed  on  the  DC  bias  voltage,  the  resultant  optical  spectral  profile  does  not 
correspond  to  that  expected  for  sinusoidal  amplitude  modulation.  It  appears  that  some 
nonlinear  behavior  is  taking  place  as  the  beam  passes  through  the  modulator.  It  has  been 
speculated  [8]  that  this  unexpected  behavior  may  be  due  to  Brillouin  scattering  [9]  of 


43 


photons  by  thermal  phonons  in  the  KDP  modulator  crystals.  This  would  account  for  the 
blurring  of  spectral  detail.  However,  verification  or  refutation  of  this  hypothesis  will 
require  additional  work. 

It  is  recommended  that  follow-on  work  begin  at  the  beginning  with  DC 
characterization  curves  of  the  modulator.  It  must  be  determined  whether  the  modulator  is 
to  be  aligned  as  if  it  were  a  quarter  waveplate,  a  whole  waveplate,  or  some  other 
configuration  with  no  DC  voltage  applied.  Then  DC  curves  such  as  the  one  presented  in 
Figure  9  should  be  constructed  at  various  levels  of  optical  power  input  to  the  modulator 
from  the  laser.  From  there,  experiments  can  be  designed  to  attempt  and  understand  more 
about  the  issues  of  the  modulator  discussed  above  and  throughout  this  paper.  A  good 
place  to  start  may  be  to  cool  the  modulator  and  study  the  effects  of  temperature  on  its 
behavior. 


44 


LIST  OF  REFERENCES 


1 .  Larraza  and  Coleman,  Nonlinear  Propagation  in  Optical  Fibers:  Applications  to 
Tunable  Lasers,  Andres  Larraza,  paper  prepared  for  thesis  students. 

2.  Model  85  Ion  Laser  Operator  Manual,  Cooper  LaserSonics  Inc.,  1984. 

3.  Michael  C.  Ladner,  Optical  Modulator  LM0202P  Characteristics,  Naval 
Postgraduate  School  Thesis,  June  1996. 

4.  Sybil  P.  Parker,  Encyclopedia  of  Physics,  McGraw-Hill,  1982. 

5.  Frank  L.  Pedrotti  and  Leno  S.  Pedrotti,  Introduction  to  Optics,  Prentice-Hall,  Inc., 
1987. 

6.  Projects  in  Fiber  Optics,  Newport  Corporation,  Fountain  Valley,  CA. 

7.  J.  Wilson  and  J.F.B  Hawkes,Optoelectronics,  An  Introduction,  Second  Edition, 
Prentice  Hall,  Englewood  Cliffs,  New  Jersey,  07632,1989. 

8.  D.  Scott  Davis,  Professor  of  Physics  Naval  Postgraduate  School,  Personal 
Conversation. 

9.  Bendow,  Birman  and  Agranovich,  Theory  of  Light  Scattering  in  Condensed 
Matter,  Plenum  Press,  1976. 


45 


46 


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Department  of  Physics 
Naval  Postgraduate  School 
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Department  of  Physics 

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Department  of  Physics 

Naval  Postgraduate  School 
Monterey,  California  93943-5002 

6.  Professor  Scott  Davis,  Code  PH/Dv 1 

Department  of  Physics 

Naval  Postgraduate  School 
Monterey,  California  93943-5002 

7.  Professor  J.  H.  Luscombe,  Code  PH/Lj 1 

Department  of  Physics 

Naval  Postgraduate  School 
Monterey,  California  93943-5002 

8.  Professor  D.  Walters,  Code  PH/We 1 

Department  of  Physics 

Naval  Postgraduate  School 
Monterey,  California  93943-5002 

9.  Commandant  (G-SIR) 2 

2100  Second  Street  S.W. 

Washington,  DC  20593-0001 


47 


10.        Commandant  (G-SEC) 

2100  Second  Street  S.W. 
Washington,  DC  20593-0001 


11.        Commanding  Officer 

USCG  R&D  Center 

1082  Sheene  Cossette  Road 

Groton,  CT  06340-6096 


12.  LT  Michael  C.  Ladner 

2350  South  2300  East 
Salt  Lake  City,  UT  84109 

13.  LT  Harlan  V.  Wallace 

4479  Camille  St 

Salt  Lake  City,  UT  84124 


48 


DUDLEY  KNOX  LIBRARY 

NAVAL  POSTGRADUATE  SCHOOL 

MONTEREY  CA  93943-5101 


DUDLEY  KNOX  LIBRARY 


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