field emission corporation - nasain an electrolytic tank so equipotential plots could be made. were...

38
OF FIELD EMITTED ELECTRONS GPO PRICE CSFTl PRICE(S) S I;. W. Swansoh L. C , Crouser Hard copy (HC) Microfiche (MF) Prepared far I ;i ff 653 July 65 Headquarters Nat4-51 Aeronautics and Space Administration Washington, D. C. Contract NASw- 15 16 Field Emission Corporation \ McMinnville, Oregon a https://ntrs.nasa.gov/search.jsp?R=19680025477 2020-02-22T14:36:53+00:00Z

Upload: others

Post on 12-Feb-2020

3 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

OF FIELD EMITTED ELECTRONS

GPO PRICE

CSFTl PRICE(S) S I;. W . Swansoh L. C , Crouser

Hard copy (HC)

Microfiche (MF) Prepared far I ;i

ff 653 July 65

Headquarters

Nat4-51 Aeronautics and Space Administration Washington, D . C .

Contract NASw- 15 16

Field Emission Corporation \ McMinnville, Oregon

a

https://ntrs.nasa.gov/search.jsp?R=19680025477 2020-02-22T14:36:53+00:00Z

Page 2: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

PROGRESS REPORT NO. 6

14 Februa ry 1968 to 14 May 1968

TOTAL ENERGY DISTRIBUTION MEASUREMENTS O F FIELD EMITTED ELECTRONS

L . W . Swanson L. C . Crouser

P repa red for

Headquarters

Washington, D. C . National Aeronautics and Space Administration

June 1968

CONTRACT NASW-1516

Page 3: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

TABLE OF CONTENTS

PURPOSE

I INTRODUCTION

THE MODIFIED CONCENTRIC SPHERE RETARDING POTENTIAL ANALYZER

1

2

111 THE INFLUENCE OF ADSORBATES ON THE TOTAL ENERGY DISTRIBUTION O F FIELD EMITTED ELECTRONS

IV TOTAL ENERGY DISTRIBUTION MEASUREMENTS FROM CLEAN SUBSTRATES 31

RE FE RENGES 32

8

c

i

Page 4: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

ILLUSTRATIONS

.

Figure 1. Lens system in modified concentric sphere r e t a rd - ing potential energy distribution tube consisting of lens sys t em (A - E) , collector (F) and ground shield (G).

Figure 2 . Solid curve is derived f rom equation (2 ) for p = 0.048. Data points a r e experimental values of the TED fo r clean (11 1) Mo.

Figure 3 . Solid curve is derived f rom equation ( 2 ) for p = 0.068. Data points a r e experimental values of the TED for barium on (1 11) Mo.

Figure 4. Solid curve is derived f rom equation (2) fo r p = 0.091. TED fo r barium on (1 11) Mo.

Data points a r e experimental values of the

F igure 5. Solid curve is derived f rom equation ( 2 ) fo r p = 0.060. Data points a r e experimental values of the TED f o r cesium on (1 10) W .

F igure 6. Solid curve is derived f rom equation ( 2 ) f o r p = 0.079. Data points a r e experimental values of the TED fo r cesium on (1 10) W .

F igure 7. Solid curve is derived f rom equation (2 ) for p = 0.044. Data points a r e experimental values of the TED fo r clean (110) Mo.

F igure 8. Solid curve is derived f rom equation ( 2 ) fo r p = 0.062. Data points a r e experimental values of the TED fo r cesium on (1 10) Mo.

F igure 9. The lower curves show the variation of the rat io of the adsorbate coated A to clean A, emitting a r e a and work function 8f with cov rage Q . The middle curve gives the rat io ( @ , / O f ) 31'= pc /r at various coverages The upper curve shows the variation of polarizabili tya calculated according to equation (1). These data were obtained f r o m barium on ( 1 11) Mo where monolayer coverage occurs near (r = 4 . 5 x 104.

F igu re 10. The lower curves show- the variation of the rat io of the adsorbate coated A to clean A, emitting a r e a with covera e ( r . The middle curve gives the rat io ( Q e / $ f ) 'I2 = p c upper se t of curves show the variation of a calcu- lated according to equation (1). These data were ob- tained f r o m cesium on ( 100) and (1 10) W wher f4 monolayer coverage occurs near 0' = 2 .7 x 10

at various coverages. The

.

3

14

15

16

17

18

19

20

2 2

23

ii

Page 5: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

I -

-

ILLUSTRATIONS (Cont'd)

Figure 11. The lower curves show the var ia t ion of the ra t io of the adsorbate coated A to clean A, emitting a r e a and work function with covera e b . The upper curve gives the ratio ( @ e / g f ) 3b = 0, /ir at various coverages. These data were obtained from cesium on (110) Mo. The value of A/Ao for (110) W i s given for comparison purposes. 24

ii i

Page 6: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

TABLES

TABLE I

TABLE I1

TABLE 111

TABLE IV

6

28

2 9

30

iv

Page 7: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

.

PURPOSE

The purpose of this r e sea rch program i s two-fold. F i r s t , we a r e

interested in measuring the total energy distribution of field emitted electrons

in o rde r to ascer ta in the usefulness of this technique to examine the electronic

band s t ruc ture .

various orientations of different meta ls .

involves an investigation of the effect of adsorption on the total energy

distribution.

obtain information regarding the nature of the bonding mechanism f rom such

s tudies .

During this program we plan to extend the measurements to

The second thrust of this program

According to recent theoretical studies one m a y expect to

1

Page 8: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

' - I INTRODUCTION

A new concentric sphere retarding potential energy analyzer tube

has been constructed and i s awaiting evacuation.

operation and resolution of the tube with a <310> oriented W field emi t te r since

the electron emission behavior of that direction i s well known and predictable e

It i s then hoped to extend these measurements to other meta ls in which solid

s ta te band s t ructure measurements have indicated a possibility of field emission

total energy distribution (TED) measurements elucidating the band s t ruc ture

information

I t is planned to f i r s t check

A pre l iminary study of the e f fec t of adsorbed layers on TED m e a s u r e -

m ents and total current-voltage relationships has been completed.

of field emitted electrons f rom single c rys t a l faces of cesium and bar ium coated

tungsten and molybdenum surfaces have been measu red .

men ta l pa rame te r s extracted from TED curves were compared with theoretical

va lues obtained f rom the Sommerfeld based Fowler-Nordheim theory of field

emiss ion by ,assuming the adsorbate a l t e r s the emission through the work

function t e r m .

reasonable agreement with the Fowler-Nordheim theory so far a s the TED

shapes a r e concerned.

coverage can be explained by a field polarization effect. a sharp

inc rease in the apparent emitting a r e a a t low cesium coverages m a y be due

to a resonance tunnelling effect a s predicted elsewhere

The TED

The various experi-

Resul ts of adsorption on (1 11) Mo ( 1 10) Mo and (1 10) W are in

A decrease of the apparent emitting a r e a with adsorbate

However

I1 THE MODIFIED CONCENTRIC SPHERE RETARDING POTENTIAL ANALYZER

During this period a g rea t deal of effor t has gone into the design and

construction of a concentric sphere retarding potential analyzer .

diagram of the new lens system is shown in F igure 1 .

A schematic.

Several modifications

have been

on during

system in

made in the present design when compared to the analyzer reported

the l a s t period.

o rde r to couple the accelerating lens c loser to the cathode.

An electrode A (F igure 1) has been added to the

By

2

Page 9: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

.015 THICK

I -

.)

k r Figure 1 . Lens system in modified concentric sphere retarding potential

'energy distribution tube consisting of lens system (A - E ) , collector (F) and ground shield ( G ) .

3

Page 10: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

doing this i t will be possible to operate the system at a lower total voltage

became of the c loser spacing. We a lso have attempted to reduce any lens

effects occurr ing a t e lectrodes B , C , and D by reducing the apera ture s izes .

The single c rys t a l collector in the previous design has been replaced by a

m e s h and Fa raday cup s o that only those electrons passing through the mesh

and into the Fa raday cup a r e analyzed.

eoklection will overcome the problem of the reflection of low energy- electrons

from the collector surface.

with respec t to the m e s h so any reflected electrons f rom the Faraday cup

will be f s rced to re turn to the cup and be collected.

I t i s expected that this method of

The Fa raday cup can be biased slightly positive

The necessa ry considerations in the design of a concentric sphere

retarding analyzer were pointed out in the l a s t report and involved determining

the proper voltage for the spherical electrodes of radius r according to

L R I T 0 . -- ' "k (1 - - V (r) = - r R - r

0

where r i s the inner sphere radius and R is the outer sphere rad ius .

also shown that i t is possible to cor rec t for the diverging effect of the acce lera-

ting lens apera ture (A) on the electron r ays (positive spherical aberrat ion) by

repositioning the point source on the axis a distance p f rom the innermost spheIieal

It was 0

elect.rode of radius a where

1 - l

1

4( 1 - a /b )

and b is the radius of the outer collector e lectrode.

source to appear a t the center of symmetry of the spherical sys tem.

This will cause a virtual

In o r d e r to check the above calculations a model of the design wzis placed

in an electrolytic tank so equipotential plots could be made .

were plotted by hand using graphical t ra jectory plotting techniques. The proper

position for the cathode to c o r r e c t for accelerating lens apera ture effects in thb

Electron t ra jector ie?

4

Page 11: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

I -

.

design shown in Figure 1 was determined to be .022 inches behind the center

of symmetry of the sys tem. With the cathode placed a t that position equi-

potential plots showed that electron t ra jec tor ies formed a vir tual source a t

the center of symmetry to a 6 beam half angle.

the actual beam half angle to 1 , the system should not exhibit appreciable

spherical aber ra t ion .

and calculated voltage rat ios for each electrode ic the spherical sys tem.

0 Since the present design l imits

0

Table I gives the electrode dimensions, apera ture s izes

The m o s t difficult modification made to the system was the substitution

of a mesh for the single c rys ta l collector. All of the hemispherical e lectrodes

used in the design were spun from 0.030 inch flat molybdenum stock and lapped

to final s ize and finish. F o r electrode E a copper inser t with a 0 .150 inch

diameter hole in the center and the same radius of curvature as the molyb-

denum hemisphere was brazed into the center of the hemisphere. A stainless

s tee l f o r m , lapped with the copper i n s e r t to the same radius of curvature and

oxidized in wet hydrogen a t 800 C . was made .

a 1000 line p e r inch (LPI) copper m e s h over the hole and form the m e s h to the

radius of curvature of the electrode while making a gold diffusion b raze to attach

the m e s h to the copper in se r t .

a ver t ical hydrogen furnace a t 700 C .

vapor plated with platinum to attempt to avoid the problem of oxide over layers and

patch field which would distrub the local e lec t r ic potential f rom i t s t rue value.

0 This form was then used to hold

The forming and diffusion braze were made in

The copper inser t and m e s h were then 0 -

At the present time the analyzer tube h a s been assembled and is

awaiting evacuation.

tube to check operation and resolution.

It is planned to use a (310) oriented tungsten tip in the

5

Page 12: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

I -

, -

TABLE I

E 7-e c t s o de Inner Radius ( in . ) A p , + - i ~ ~ f : Diameter (in) Re1 . Voltage

A

B

c

D

0.156

0.415

0.555

0.798

E 1.196

0.120

0 . 0 2 8

0.028

0 .028

i .o

0.264

0.164

0 . 0 6 0

0.150 (covered by 0 1000 LPI copper mesh)

6

Page 13: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

IPI THE INFLUENCE OF ADSORBATES ON THE TOTAL ENERGY DISTRIBUTION O F FIELD EMITTED ELECTRONS

One of the motivations for field emission total energy distribution (TED)

measurements of adsorbate-coated substrates s tems f rom the possibility

that the interaction potential of the adsorbate m a y a l t e r the t ransmission

probability and hence, the TED.

theoretical bas i s by Duke and Alferieff' (D and A)

through adsorbed atoms by an atomistic one -dimensional pseudo-potential

model. In the case of metal l ic adsorption, their resu l t s predict an increase

in t ransmission apa r t f rom the usual work function lowering. This approach

is in contrast to other t reatments which a s sume the adsorbed layer modifies

the Fowler-Nordheim equation either through the work function term"

image potential t e r m .

a change in both the preexponential and exponentialterms of the Fowler-

Nordheim ( F N ) equation i s predicted.

c a s e of metall ic adsorption since i t a l so predicts additional s t ruc ture in the

TED curve when the valence level of the adsorbate falls below the substrate

F e r m i level .

This expectation has been given a

who t reated field emission

or the 4

In each of these cases including the D and A theory

The D and A theory is unique in the

Recent experimental resul ts have shown the FN theory to be inadequate 5

for describing the TED f rom the (100) directions of clean molybdenum

tungsten All other ma jo r c rys ta l -

lographic directions of both molybdenum and tungsten show no g r o s s deviations

f r o m the Sommerfeld model

the non-free-electron nature of the m e t a l s .

of the Sommerfeld model in describing field emission f rom the transit ion

m e t a l s is the resu l t of the narrow energy band ("0.2 eV) sampled by field

emiss ion .

visible only when unusually smal l Fermi sur faces a r e emitting

gaps occur within -0.2 eV of the F e r m i level.

and 6

due to band splitting near the F e r m i level .

upon which the F N theory is based in spite of

The somewhat surpr is ing success

Accordingly, the specific effects of the emi t te r band s t ructure a r e 728 o r when band

Historically the F N theory has been utilized with apparer-t success to

descr ibe the field emission character is t ics of both clean and adsorbate

7

Page 14: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

coated sur faces

and energy distribution measurements to single atomically smooth c rys ta l

f a c e s , has eliminated the undesirable averaging and allows a m o r e stringent

tes t of the F N theory.

adsorption a r e a l so rel iably given by the F N equation is now substantial .

Recent use of probe techniques, which confine work function

The evidence that work function changes due to

At p re sen t , two minor modifications to field emission calculated work 3

fuactioris of zdsorbed l aye r s have been considered.

who considssed the detail shape of the contact potential w i thin the adsorbed

layer and ita effect on the F N equation. The graphical method employed by

Gomer showed i t s effect on the F N equation.

by Gomer showed that the apparent contact potentials obtained from F N analysis

a r e lower than actual due to the discreet nature of the dipole potentials of the

adsorbed a toms .

of significant consequence only a t coverages l e s s than 0 . 1 monolayer and field

strength i n excess of 3 x 10

The first is due to Gomerb ,

The graphical method employed

This correct ion, which inc reases l inear ly with field becomes

7 V/cm.

The second correct ion to field emission work function calculations s t e m s

f r o m the polarization of the adsorbate due to the applied e lec t r ic field.

cor rec t ion has now been substantiated in a number of cases 9 ’ 1 0 2 1 1 and has

succ e s sfully explained the variation of emitting a r e a upon adsorption. This

e f f e c t , which increases the work function d , i s l inear with e lec t r ic field F

and thereby in first o rde r appears as an alteration to the preexponential t e rm

of the F N equation 5 such that the ra t io of the adsorbate coated emitting a r e a A

to the clean emitting a r e a A

This

is given by: 0

7 1 / 2 log A/A = -4.20 x 10 0 g rnr a / €

0 ( 3 )

3 where G Is the adsorbate polarizability in c m , 6 the adsorbate density in a toms /

cm- , g a factor ranging f rom 2 to 4 (depending upon the degree of localization of

the induced dipole to the adsorbate) , and E is the rat io of the applied to actual

field a t the adsorbate F /F_ . One approximation of E comes f rom the Topping

3

12

3 12 U

model in which the value of E is given by E = 1 t 9 a 6 and represents the

8

Page 15: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

,

seduction in field a t a specified adsorption site due to the accumulated effect

of the field induced dipoles in a square a r r a y of adsorbed par t ic les . Exper i -

mental values of the preexponential changes in the F N equation for both

electropositive and electronegative

values of a. calculated in t e r m s of equation ( 3 ) .

the F N equation has been given by van Oos t rom,

of the image potential term by the adsorbate .

t reated as a s t ruc ture less dielectric film of finite thickness which modified

the image potential.

f i r s t correct ion

adsorption.

adso rbate s have given re a. sonable 12 9 , 1 1

An additional modification of 4

who considered the alteration

Ir; this case the adsorbate w a s

This modification, which is in the same sp i r i t a s the

mentioned above, appears to be valid only for multi layer

The above mentioned modifications to the F N theory due to adsorption

do not predict changes in the TED which cannot be accounted for by c o r r e s -

ponding changes in F a n d / o r

dimensional pseudo-potential model of field emission.

of the effect of adsorbed l aye r s on field emiss ion , i t i s shown that the adsorbed

par t ic le is able to affect resonance tunnelling of the electrons *en the valence

level of the adsorbed par t ic le is properly oriented with respect to the F e r m i

level . Under cer ta in conditions of metal l ic adsorption additional s t ruc ture

in the TED is predic ted along with la rge enhancements (10-10 ) in the pse-

exponential t e r m of the F N equation.

0. Such is not the case for the D and A one-

In this novel t reatment

4

It thus should be possible to examine the reliability of the various

modifications to the F N theory by simultaneous analysis of the F N equation

and T E D . In this study we have examined cesium and barium adsorption on

a few crys ta l planes of molybdenum and tungsten with respect to their effect

on the TED and current-voltage relationships throughout the monolayer coverage a

EXPERIMENTAL APPROACH

Before proceeding i t wi l l be helpful to l i s t the relevant equations

pertinent to the cu r ren t voltage I(V) charac te r i s t ics of field emitted electrons

and the TED. F o r the Sommerfeld mode l , upon which the F N theory of

9

Page 16: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

field emission is based , the cur ren t density p e r unit total energy J (E)

(where E is the energy E relative to the F e r m i energy E ) is given by: 13 f

J(G) = J /d (1 t e E /Pd) 0 (4)

where p = k T / d and J , the total cur ren t density (integrated over all E) a t 0 14

0 K , is given by: 0

2 (The numerical form as sumes J

expression for the parameter d i s

in A / c m , F in V / c m and 0 in e V ) . The 0

d = 9 .76 x F /81/2 t (y) ( e v ) . (6)

The image correct ion t e r m s t(y) and v(y) a r e slowly varying tabulated

functions of the auxiliary variable y = (e F) /O. If the condition E/pd<O

is m e t equation (4)can be expressed as

14 3 1 /2

J(r) 5 J eeld / d 0

(7)

In a retarding potential analyzer we note that E can be related to the collector

work function 91 and the emitter-to-collector bias potential V in the form C t

E = oc - Vt, thereby allowing equation (7) to be writ ten in the working fo rm

(8) 0

J log JCE) = log t (0 - Vt) / 2.3d

Thus , the value of d can be obtained from the slope m

log J(E) versus V

f i r s t derivative of the collector current I

= 1 /2.3d of a plot of e

Experimental values of J(E) can be evaluated from the t '

with r e spec t to V e t

J(E) = - n dI / d V t , C

where n i s an a r b i t r a r y constant of normalization.

( 9 )

10

Page 17: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

2

versus 1 /V yields a slope m which is related to the emi t te r work function

8, and the geometric factor (3= F / V as follows:

I t is further observed that a "Fowler-Nordheim" plot of log I / V 0

f

7 3/2 m f = - 2 - 9 6 x 10 0f s (y) /p ( c m ) ,

where s(y) = 0.943 over the range of y encountered in prac t ice .

Of reiative to a reference value 0 can be readily established a s shown by

rewrit ing equation (10) a s follows:

The value

where m

surface average) and the value f3 is assumed unchanged.

difficulty in determining accurate values of 8 and p , equation (10) cannot be

employed for p rec i se work function calculation; however, as . pointed out by

Young , the expressions for m and m can be combined to give

is the F N plot slope for the reference work function (usually the 0

Because of the

15 e f

8 e = - 3mf t (y) /2 m e V s(y) , (12)

where V is the anode voltage. Accordingly, within the framework of the

Sommerfeld model a value of work function can be ascer ta ined from combined

energy distribution and F N plots f rom equation (12) which eliminates assumptions

concerning and p .

It will be our purpose to examine various experimental pa rame te r s

obtained f rom TED and F N plots f o r se l f -consis tency as a function of adsorbate

coverage and attempt to in t e rp re t the :results in t e r m s of the theoretical modi-

fications discussed in the preceeding section.

EXPERIMEN TAL PROCEDURE

The experimental energy

descr ibed previously. Br ie f ly , 6 analyzer tube and procedure have been

the tube designed by van Oos t rom, 4

i s a

1 1

Page 18: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

retarding potential analyzer equipped with magnetic deflection to align

emiss ion from a part icular direction with a small aper ture in the anode

plate.

of 15 to 20 mV.

in this investigation.

to the wire axis owing to the slight a l terat ion of the TED when magnetic

deflection was employed.

to fabr icate emitters with the desired c rys t a l direction along the wise axis.

Without magnetic deflection the analyzer tube gave a resolution

Both molybdenum and tungsten subs t ra tes were employed

Attention w a s main ly given to those planes perpendicular

Zone m-r,lted sirigk crystal wire was employed

The approximate geometric emitt ing a r e a seen by the 1 mm diameter - 4 2 2

probe hole was approximately 3 . 4 x 10 r (cm ) , where r is the emi t te r - 5

rad ius . F o r emi t te r radi i of 1 to 2 x 10

emitting area was the o r d e r of 3 to 13 x 10

approximately 30 to 130 substrate a toms contributing to the probe emiss ion

f rom a (100) plane.

cm employed in this study the -14 2

c m : this cor responds to

Deposition of cesium onto the substrate was accomplished by resis t ively 0

heating to 1100

This method has proven to give a pure flux of cesium ions which can be

focused onto the emi t t e r . The bar ium source consisted of a sho r t segment

of i r o n clad bar ium wire mounted on Nichrome leads for res i s t ive heating.

A four lead tungsten loop supporting the emi t te r was utilized for heating the

emi t te r to known tempera tures .

77

liquid nitrogen cryos ta t .

K a small bead of ces ium zeolite fused onto a platinum wi re .

The r e su l t s reported he re were obtained a t 0 K ; this was accomplished by immers ing the ent i re analyzer tube in 2

RESULTS

The r e su l t s of b'asic significance to this study a re (1) the agreement

of the TED shapes with equation (4), throughout the coverage r a n g e , ( 2 ) the

variation of A/A

(d, and 0 e a r e a s are calculated both from the value of the intercepts of the FN plots

with adsorbate coverage and ( 3 ) the agreement between 0

as calculated by equations (11) and (12) respectively. The emitting

12

Page 19: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

rnd from F N slope data alone by a method described elsewhere. l 6 Both

methods yielded near ly identical A values in this investigation.

of analysis was therefore to t rea t the data according to the F N theory in

a stif -consistent manner and examine any discrepancies with respec t to

exrEting modifications of the F N theory for adsorption.

Our method

In obtaining values of fl via equation (11) for various planes or as a f function ot coverage i t shoul-d be emphasized that a uniform field factor p i s

assumed.

8, and 8 3verage p fieEd fac tors .

Thus, within the framework of the F N model disagreement betwetn

can only be attributed to a difference between the local p F; c

and the

The apparent change in p can be obtained from the

F igures 2 to 8 show representative TED curves for the various systems

investigated along with the theoretical curves derived f rom the value of d

(and hence p) obtained from the best f i t slope m

normalization constant n of equation ( 9 ) was adjusted to allow overlap in the

Latter region.

limitations imposed by the analyzer resolution. A somewhat disturbing devia-

tion from theory a t low values of d1 /dV on the low energy side of some of the c t experimenta.1 TED data i s believed to be caused by an ar t i fact of the analyzer

and should be ignored. The values of dI /dV were obtained by monitoring

the change in I Values of 6 for the C s / W , c t ’

G s / M o and the B a r n sys tems were obtained from previously established

Petationships between fl and 6

of the low energy ta i l . The e

The poor f i t on the leading edge and near the peak is due to the

c t for a 10 m V increment in V

17,18

Barium on (1 11) Mo

The TED curves for barium on (1 11) Mo give a reasonably good fit to

equation (4) as observed in F igures 2-4.

or shape changes throughout the coverage range that cannot be descr ibed by

thr, equation ( 2 ) paramete r s .

apparent value of p / p is not constant, but i s f i r s t l a rge r and then smal le r

thar unity as the coverage increases .

W e observe no anomalous hurr,ps

On the other hand , Figure 9 shows that the

C

The length of the ver t ical bare a r e

13

Page 20: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

20

IO

8

6

4

2

I .o 0.8

0.6

0.4

I I I

Mo ( 1 1 1 )

F = 27.81 MV/crn

= 4.53 eV

+c I I

-4.8 -4.9 - 5.0 -5. I Vt (Volts)

Figure 2 . Solid curve i s derived from equation (2) for p = 0 .048 . points are experimental values of the TED for clean ( 1 1 1 ) M o ,

Data

14

Page 21: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

I ’

n v) t c 3

.-

f E f!

>+

t .- 0 U

0 \

U I

0 w

20

IO

8

6

4

2

I .o 0.8

0.6

0.4

B

B d M o ( I I I )

c = 1.8 x atoms/cm2

F = 16.89 MV/cm

I I I I

-4.8 -4.9 - 5.0 -5.1 vt (‘mts)

Figure 3 . Solid curve is derived from equation (2 ) for p = 0 . 0 6 8 . points are experimental values of the TED for barium on ( 1 1 1 ) M o .

Data

15

Page 22: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

2c

IC

8

6

4

2

I .o 0.8

0.6

0.4

I I I

Ba/Mo ( 1 1 1 )

r = 5.5 x 1014 otoms/cm2

vt (Volts)

Figure 4 . Solid curve is derived from equation (2) for p = 0.091. points are experimentalvalues of the TED for barium on ( 1 1 1 ) M o .

Data

16

Page 23: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

V+ (Volts)

Figure 5 . Solid curve i s derived from equation (2 ) for p = 0 . 0 6 0 . points are experimental values of the TED for cesium on ( 1 10) W .

Data

17

Page 24: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

cs/w CT = 3.0 x

n tn t c 3

.-

2 t .- 9

0 L

Y

>t U \

0 I

u Y

-

4 -

-

2 -

1.0 -

O o 8 I 0.6

4

0

( 1 IO)

1014 atoms/c

MV/cm

eV

0

m2

-4.9 -5.0 -5.1 -5.2 v+ (Volts)

Figure 6 . Solid curve is derived from equation (2) for p = 0.079. Data points a r e experimental values of the TED for ces ium on ( 1 10) W .

18

Page 25: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

I -

20

IO 8

6

4

2

I .o 0.8

0.6

0.4

-4.6

F i g u r e 7 .

0

Mo (110)

F =37.23 MV/cm

= 4.69 eV

-4.8 -5.0 -5.2 v+ (Volts)

Solid curve i s derived f r o m equation (2) for p = 0.044. points a r e experimental values of the TED for clean ( 1 10) Mo.

Data

19

Page 26: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

20

IO

8

6

n

.- 2 4 t =I

L z t .- -P

Y 6 2 >" U \ 0

c(

U ' 1.0

0.8

0.6

0.4

- 4.6

Figure 8.

I I I I I I

Mo/Cs (110)

cT= 0.2 x ioi4 atoms/cm2 -

F = 22.40 MV/cm

+e = 3.45 eV

0 .

-4.8 -5.0 - 5.2 v+ (Volts)

Solid curve is der ived from equation (2 ) for p = 0.062. points are experimental values of the TED for ces ium on (110) M o .

Data

20

Page 27: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

the ex t reme values of p /@ determined at different field s t rengths and

probably represents the uncertainty in experimental values of m , since

no systematic variation with field strength is observed in these r e su l t s .

Adherence to the FN model yields a local field enhancement j3 / p a t

6 = 0 of 1470, @

laboratory have yielded the somewhat high value of $4

the ( 11 1) plane of Mo .

C

e

C

= 4.53 eV and @ = 4.15 eV. Several measu remen t s in this C f

= 4.5 t 0.1 e V for - e

In addition to the variation of p / E with 6 , the F igure 9 r e su l t s also C

show a significant seduction in the apparent emitting a r e a A/A

through a slight min imum with increasing C.

this minimum in A/A

which goes 0

I t i s interesting to note that

occurs near the minimum in the (8 ver sus 6 curve . 0 f

Cesium on (100) and (110) W

Representative plots of the TED data for cesium on (110) W shown

in F igu res 5 and 6 a l so indicate a reasonably good f i t to the theoret ical

expression given in equation (4) and show no anomalies in their shape with

increasing ces ium coverage. In contrast to the bar ium r e s u l t s , pc/+ inc reases

significantly above unity in the midcoverage 6

As noted previously,

plane is physically unacceptable for this highly faceted region. W e there?

fore suspect some inadequacy of the Sommerfeld model for emission f rom

the clean(110)direction of W .

values fo r both the (110) and (100) planes are l a r g e r than unity a t low coverages .

- 4 e

range as observed in F igure 10.

the occurrence of a value p /E71 for the clean (110) C

Also, in cont ras t to the B a / M o r e s u l t s , A / A 0

Cesium on (110) Mo

Resul ts for cesium on (110) Mo have been limited to the low coverage

region and are shown in F igure 11. The Mo resu l t s show a value of p - / p -N = 1 c 14 2

forC<O.3 x i o a t o m s / c m , in agreement with the (110) W data. Also in

ag reemen t with both the previously discussed sys t ems , the TED data ag rees

reasonably well with equation (4) in the l imited range of Cinves t iga ted .

The m o s t striking cont ras t with the (110) W resu l t s is the much

2 1

Page 28: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

n

Y 2

Figure 9 . The lower cu rves show the variation of the rat io of the adsorbate coated A to c lean A, emitting area and work function of with coverage r. The middle curve gives the rat io (oe/@43/2= pc/p at various coverages . polarizabili ty Q calcdated according to equation ( 1 ) . These data were obtained from barium on ( 11 1 ) Mo where monolayer cove r - age occur s n e a r C = 4.5 x 10 14 .

The upper curve shows the variation of

22

Page 29: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

25

F i g u r e 10. The lower cu rves show the variation of the ratio of the adsorbate coated A to c lean A, emitting area with coverage r . The middle curve gives the ra t io (8e/0$/2 = pc/p a t various coverages. The upper s e t of curves show the variation of a calculated according to equation (1 ) . (110) W where monolayer coverage occur s near C = 2.7 x 10 14 .

These data were obtained f rom cesium on (100) and

I I I I I I

- cs /w -

2 3

Page 30: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

10.0 -

0

\Q a

3.0

c~ ( x Io '~ ) atoms/cm2

n > Q, Y

-8-

Figure 11. The lower curves show the variation of the ra t io of the adsorbate coated A to clean A, emitting a r e a and work function with cover- ageCT. The upper curve gives the rat io ( 0 e / @ f ) 3 / 2 = pc/p a t zzrioils coverages. (110) Mo. purposes .

Tnese data were obtained f rom cesium on The value of A/Ao for (110) W is given for comparison

24

Page 31: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

l a rger increase in A/A I t should

be pointed out that the value of A = 1 x 10 a toms /cm is considerably

smaller than the (1 10) W value of 46 x 10

that both emi t t e r s possessed almost identical rad i i .

of the FN theory the small value of A

local magnification; however, this explanation is undesirable in view of

fi / p e l . ' C

fully descr ibe clean ( 1 10) Mo emission a s in the case of (110) W .

fo r (1 10) Mo a t low cesium coverage. 14 2

14 2 atoms / c m ,

0

0

in spite of the fact

Within the framework

can only be explained by a la rge 0

This r a i s e s suspicion th2t t h e FX preexponeniial t e r m may not

DISCUSSION

F r o m these prel iminary resul ts one m a y make severa l observations

regarding the adequacy of the F N model in i t s original and modified forms

to descr ibe metal l ic adsorption.

the apparent emitting a r e a seen by the probe varied ,substantially with

adsorbate coverage--a r e su l t not explained by the unmodified FN theory.

polarization correct ion described by equation (3 ) predicts a decrease in

A/A with increasing value of 8 6 and has been employed to evaluate

an effective value of u for the adsorbed par t ic les .

A / A > 1 a t low cesium coverage which c lear ly cannot be rationalized by

the polarization mpdel , we have evaluated the apparent u throughout the mono-

l a y e r coverage where A/A <1 and give the resu l t s in F igures L0;md 11. In

spite of the c lass ica l and phenomenological nature of the polarization cor rec t ion ,

it yields a reasonable and cpnstant value of a throughout m o s t of the monolayer

coverage for bar ium and cesium.

F i r s t , in each of the sys tems investigated

The

1 / 2 0

Excluding the values of

0

'0

The values of A/A which occur for cesium 0

on (110) M o , (100) and (110) W a t ( 0 . 1 monolayer m a y be attr ibuted to a

resonance tunnelling'enhancement of the emission as descr ibed by D and A .

Inasmuch as cesium a t low eoverage on the (100) and (110) planes of W and

the ( i 10) piane of Mo give a negative value for the difference between the

adsorbate ionization potential V. and work function V. - 8 one expects a smal l

i nc rease in coverage to align the broadened valence level of the adsorbate

with the substrate F e r m i level. It is under the la t ter conditions that maximum

1 1

2 5

Page 32: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

resonance tunnelling, manifested by an enhanced apparent emitting a r e a

dnd s t ruc ture in the TED, is expected.

becomes l a r g e r (in a positive sense) and resonance tunnelling diminishes due

to a decrease in the interaction between the tunnelling electrons and the

adsorbate valence band. The conspicuous absence of values A / A > 1 for

bar ium on (111) Mo can be attributed to the l a rge r positive value of V. - 0 Fl eV

a t ze ro coverage which positions the adsorbate valence level below the

substrate F e r m i leve l , thereby reducing adsorbate-induced r e m nance tunnelling.

1 With increasing coverage V - 0 i

0

1

One m a y speculate further that becuase V. - 8 = -0 .94 for cesium on 1

(110) M o , as opposed to -1.95 for cesium on (110) W , the valence level of the

fo rmer i s m o r e favorably aligned with the substrate F e r m i level a t low

coverage.

Fu r the r examination of the unusually small value of A

per formed before firm conclusions based on detailed comparison of the relative

magnitudes of the A/A

This m a y account for the much l a rge r values of A / A for ( 1 10) Mo. 0

for Mo should be 0

values should be made . 0

Although possible meanings of the variation in /3 /p with adsorbate C

coverage a r e manifold, i t is basicallya measure of the self-consistency between

the energy spectrum description of field emission as given in equation (4) and the

I (V) relationship given in equation (5 ) .

the F N model p i s a geometr ical factor which can be influenced by atomic sized

per turbat ions a s demonstrated in the

adsorbates such as cesium on a smooth (110) plane of W o r Mo should cause an

increase in / p , part icular ly i f clustering occur s ; pc/p should then decrease

as a smooth monolayer is formed.

p lane , such a s a (1 11) , m a y not exhibit such an increase in p / p , but r a the r a

dec rease i f the surface of the overlayer i s geometrically smoother .

apparently the c a s e i f one compares the g ross features of the variation in

p /p w i t h 6 for bar ium on (111) M o and cesium on (110) W .

geometr ic e f fec ts alone can account for the exceptionally la rge values of

pc/p in the midcoverage range of cesium on (110) W .

Specifically, within the framework of

field ion microscope. In this s e n s e , large

C

By the same token an atomically rough

C

Such i s

I t i s unlikely that C

2 6

Page 33: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

At this point i t is important to emphasize that p / p is proportional

, thus an increase i n m due to other effects should cause a C

3 I 2 to l / m

reduction in p /r . According to the D and A theory,

effects for adsorbed atoms whose valence level is aligned below the F e r m i

level a r e manifested in the TED curves by l a rge r values of m . effect would a s s e r t itself in our results as a diminution in p / p and m a y be

a contributing cause to the low and constant values for p !E a t low cesizm

coverages on the (1 10) plane of Mo and W where previously mentioned increase

in A / A occur s .

1 e e resonance tunnelling

C

This e

C

C

0

I t is noteworthy that in spite of these r e su l t s which give some measu re

of support to resonance tunnelling at small o r negative values of V. - PI , we

find no apparent f ield dependent structure in the TED curves in the c o r r e s -

ponding coverage interval as predicted by D and A . Rathe r , analysis of the

Table I1 to IV tabulations of the data show m o( 1 / F in general agreement with the

F N model .

1

e

CONCLUSIONS

The r e su l t s of this investigation which a r e prel iminary in nature provide

a m e a s u r e of support for adsorbate induced resonance tunnelling.

this support comes from the increase in the apparent emitting a r e a , since

the additional prediction of structure in the TED curve was not observed. The

experimental evidence supporting resonance tunnelling occurs only when V - 8 i is n e a r z e r o , a s expected. Over the major portion of the monolayer region the

var ia t ion in apparent emitting a rea and can be described by the field polarization

model . F r o m this study i t i s apparent that field emission TED and I(V) measu re

m e n t s of appropriate surfaces m a y be potentially useful in shedding light on the

na tu re of adsorbate bonding modes. However, additional investigations of

the TED of field emitted electrons for other sys tems are necessa ry before

a c l ea r picture of the relative importance of the various modifications to the

F N theory due to adsorbed l aye r s can be clearly established.

P r i m a r i l y

27

Page 34: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

~

N 4

m

co d m

co 9

4

d 0

N

0 00

4

d 0

N

I- m m

In 0

m

9

d

4

N co m

co In

d .

In 0

*

m 00

4

In N

N

m P

4

In N

N

I- 0

N

In 0

N

m o\

N

N ul N

m In

N

N In

N

In d

m

In 0

m

I- 03

m

co d m

In t-

*

In 0

*

m In

*

In

* 4

P 9

d

9 m

0 9 - 0

m m . .

00 4

In

0 N

9

4 * 9

4

9

* 4 4

m

4

r-4

In

0 N

Q\

9 m P

N 4

In N

0 9

P 4

0 00

P r-4

P 0

co N

N

In 4

d In 4

m

N d 0 4

N d 0 d

t- 9 N 4

In co N 4

* d 9 4

m In In d

P d P ,-.I

0

00 4

P d e 4

0 m m N

In co 0 N

m N 33

In In I-

In

e 4

P IC t-

rn cI\ 4

P I- 9

4

Q\

N 4

4

d 9 In 4

00

In d

4

m 9 03

N 9 4

N

In d 9

N

0 In 9

N

m d N

m

m 0 I-

m

d I- 4

m

In 9 N

4

d m N

N

4

N o\

N

" N m N 4

m t- o\ In

m I - I - - O C N I n 9

r N \o

4 9 I-

3 0 I- N 4 4

0 I- N 4 4

0 d I- m 4

0 d I- m 4

0 m co In 4

0 I- N Ih 4

0

P I-

4

1-4

4 * r- 4

4 * t- 4

4

0 N 9

4

0 N 9

In 0

4

In 0 4

In

In

co 4

rr)

0

m 0

In

rr,

4

d

r-4

* I-

m t - I n

m m . . m

m I-

0

I-

0

Ln

0 0

28

Page 35: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

N m 9

N co m

0

9 d

m m m

0

D

m

4

0

9 (r

4

4

0

t- 9

N

N N

N

P-

m

In In m

N m rn 4

0 N 9 *

0

m

m m N

d co 4

d d

m m m

[c- co ul

4

0 m d m

d N

0 N

N

t- 9

4

m d

co 9 m

0

9 4

4

0

0 m

4

N

N

4 4

N

N In 4

m -+

N N m

4 * In 4

0 m 9 N

m 4

ul m N

m [c-

4

9

9

m m m

In N t- 4

0 m m 4

m 4

m b

m

(r t-

m

0

N -+

co m 4

4

0 9 t-

N

0

m 0

4

4

m 0

Page 36: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

9 9

m

9 rn m

0

0 4

P- .-(

4 4

4

m P-

m

dr b

o\ 4

0 N

0

9 m m

In In

m

In

rn

o\ * m 4

9 00 dr cr)

m m dr o\

0 N

0

In * m

In In

m

In

rn

P- .-(

4 I-(

m 9 0

*

m el -+ o\

0 N

0

dr cr)

m

0 m m

00

co

P- o\ Q\

F- 9 h

*

Fi

r r a3

ln N

0

0 9

m

m m m

00

6)

dl I- tF

o\ * dr

4

I+

P- IC 00

In N

0

30

co 4

m

* 0

m

F

m

P- o\ o\

m In 0

m

N 9 * P-

0 0

0

0 m cr)

dr 0

m

P-

m

3 00

In VI N

cr

0 N 9 lc

0 m 0

tF 9

dr

m 00

dr

rr lc

0

P- In 00 4

IC In a3

N

0 9 m dr 4

0

Page 37: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

IV TOTAL ENERGY DISTRIBUTION MEASUREMENTS FROM CLEAN SUBSTRATES

L

t

Work has continued on a l i t e ra ture review for suitable me ta l s with

which band s t ructure effects m a y be examined by field emission techniques.

Since the only band s t ructure effects that can be detected by field emission

are within 0.1 to 0 . 2 e V of the F e r m i energy careful evaluation of theoretical

band s t ruc ture calculations m u s t be made due to the uncertainties in de t e r -

mining positions of predicted band s t ruc ture effects with respec t to energy.

I t was planned to examine a t l ea s t one of the group Va me ta l s such

a s Ta or N b for a wmpar i son with the neighboring group V1.a elements W

and Mo.

fabricate a field emi t te r : however, c lose examination showed the rod to be

A Ta rod was zone melted from which i t was expected to be able to

polycrystalline r a the r than single c rys t a l .

m e l t Ta and we a r e continuing the effort with the expectation that i t w i l l

be possible to reor ient the rod for use as field emission cathodes.

I t i s known to be possible to zone

I'

,

3 1

Page 38: Field Emission Corporation - NASAin an electrolytic tank so equipotential plots could be made. were plotted by hand using graphical trajectory plotting techniques. The proper ... patch

REFERENCES

1. C . Duke and M . Alferieff , J . Chem. P h y s . 46 , 923 (1967). - 2. R . G o m e r , J . Chem. Phys . 21 , 1869(1953) . - 3 . R . Gomer , Fie ld Emiss ion and Fie ld Ionization (Harvard University

P r e s s , Cambr idge , Mass. , 1961), p . 50.

4 . A .

5 . L .

6 . L .

7 . R .

8. F .

9 . D .

10. L .

11. A .

12. J .

13. R .

14. R .

van Oostrom , P h i l ips Res . Suppl. (Netherlands) 11 , 102 (1966). -

Swanson and L . Crouser , P h y s . Rev . Le t t e r s 19 , 1179 (1967). - Swanson and L . C r o u s e r , P h y s . Rev . 163 , 622 (1967). - Stra t ton , Phys . Rev . 135A, 794 (1964).

Itskovich , Soviet Phys . J E P T 23 , 945 (1966). I

Menzel and R . Gomer , J . P h y s . Chem. 41 , 3311 (1964). - Schmidt and R . Gomer , J . Chem. Phys . 42 , 3573 (1965). - Bell and L . Swanson , Surface Sci. 10 , 255 (1968).

Topping , F r o c . Royal SOC . (London) A1 14 , 67 (1927).

-

Young , Phys . Rev. 113 , 110 (1959).

Good and E . M h e r , Handbuch d e r Physik , (S. FlGgge , Springer -

-

Verlag , Ber l in 1956) Vol. 21 , p . 188.

R. Young and €3. Cla rk J . Apply. P h y s . L e t t e r s 9 , 265 (1966).

F. Charbonnier and E . Mar t in , J . Appl. Phys . 33 , 1897 (1962).

L . Schmidt , J . Chem. Phys . 46 , 3830 (1967).

L. Swanson a n d R . S t r a y e r , J . Chem. Phys . 48 , 2421 (1968).

15.

16.

17.

18.

-

-

-

-

,

32