The Cryotron Superconductive Computer Component
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Transcript of The Cryotron Superconductive Computer Component
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Memorandum 6M-38U3
Page 1 of 16
Division 6 - Lincoln Laboratory
Massachusetts Institute of Technology
Lexington 73, Massachusetts
SUBJECT: THE CRYOTRON — A SUPERCONDUCTIVE COMPUTER COMPONENT
To:
David R. Brown
From:
Date:
Approval:
Abstract:
Dudley A. Buck
August 22,
Torben H.
Meisling
Tne study of nonlinearities in nature suitable for computer
use has led to the cryotron, a device based on the destruction
of superconductivity by a magnetic field. The cryotron, in
its simplest form, consists of a straight piece of wire about
one inch long with a single-layer control winding wound over
it.
Current in the control winding creates a magnetic field
which causes the central wire to change from its superconduct
ing state to its normal state. The device has current gain,
that is, a small current can control a larger current and it
has power gain so that cryotrons can be interconnected in
logical networks as active elements. The device is also small,
light, easily fabricated, and dissipates very little power.
1. The Cryotron Principle
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I
Memorandum 6M-38U3 Page 2
The resistivity of many superconductive materials is relatively
high at room temperature, especially those which nave high transition
temperatures such as niobium, lead, tantalum, etc. It is interesting that
relatively poor conductors become superconductors at low temperatures whereas
good conductors such as gold, silver, and copper do not. The resistivity
of superconductive materials drops as they are cooled. Just above their
superconductive transition, the resistivity is between 10-1 and io-3 of
their room temperature resistivity, depending on the purity and mechanical
strain in a particular sample.
Below the superconductive transition the resistivity is exactly
zero.
That it is truly zero is vividly demonstrated by an experiment now
in progress by Professor S. C. Collins at M. I.T. wherein a lead ring has
been carrying an induced current of several hundred amperes since March
16, 1
0
5U>
without any observable change in the magnitude of the current.
1.2 Destruction of Superconduct vity by a Magnetic Field
The foregoing discussion of the superconductive transition is
valid only in zero magnetic field. With a magnetic field applied, the onset
of superconductivity occurs at a lower temperature. If the intensity of
the magnetic field is increased, the transition temperature is still lower.
A plot of the transition temperature as a function of the applied magnetic
field is more or less parabolic in shape, levelling out as absolute zero
is approached. Such a plot for several common elements is given in Figure
1.
If the temperature is held below the transition temperature for
one of these materials, the resistance of that material is zero. Its
resistance will remain zero as a magnetic field is applied until that
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Memorandum 6M-38U3 Page 3
I n a t y p i c a l c r y o t r o n , t h e r e s i s t a n c e b e in g c o n t r o l l e d i s i n t h e
fo rm o f a s t r a i g h t p i e c e o f w i r e a b o u t 1 i n c h i n l e n g t h . Th e magne t i c
c o n t r o l f i e l d i s g e n e r a t e d b y c u r r e n t i n a s i n g l e - l a y e r w i n d i n g w h ic h i s
w ou nd o v e r t h e c e n t r a l w i r e ( F i g u r e 3 , t o p ) . The c e n t r a l w i r e i s a n a l o g o u s
t o t h e p l a t e c i r c u i t o f a v ac uu m t u b e a nd t h e c o n t r o l w i n d i n g i s a n a l o g o u s
t o t h e c o n t r o l g r i d . I n t h i s c a s e , t h e p l a t e r e s i s t a n c e i s z e r o i n t h e
c u t o ff r e g i o n an d r i s e s r a p i d l y a s g r i d - c u r r e n t c u to f f i s r e a c h e d .
1 . 3 S u p e r c o n d u c t i n g C o n t r o l W i n d in g
T h e c o n t r o l w i n d i n g i s m ade o f a s u p e r c o n d u c t i n g w i r e w h ic h h a s a
r e l a t i v e l y h i g h t r a n s i t i o n t e m p e r a t u r e . N io biu m ( f o r m e r l y c a l l e d c olu m biu m )
i s u se d b e c a u s e i t h a s a v e r y h i g h t r a n s i t i o n t e m p e r a t u r e a n d c an b e d ra w n
i n t o f i n e w i r e w h ic h i s s t r o n g . L ea d o r l e a d - p l a t e d w i r e i s a se c o n d
p o s s i b l e c o n t r o l - w i n d i n g m a t e r i a l .
A t th e t e m p e r a t u r e u s e d , t h e c o n t r o l w i n d in g r e m a i n s a s u p e r c o n
d u c t o r a t a l l t i m e s , a n d w o u l d r e m a i n so e v e n i n m a g n e t i c f i e l d s m uch
h i g h e r t h a n t h o s e b e i n g u s e d t o c o n t r o l th e c e n t r a l w i r e . T h e r e f o r e , t h e r e
i s no r e s i s t a n c e i n t h e c o n t r o l w i n d i n g . A m a g n e ti c f i e l d , o nc e e s t a b l i s h e d ,
n e e d s no f u r t h e r e n e r g y f o r i t s s u p p o r t ^ t h e c o n t r o l c u r r e n t i s m a i n t a i n e d
a g a i n s t z e r o b a c k v o l t a g e . S i m i l a r l y , a l l i n t e r c o n n e c t i n g w i r e i s a l s o
s u p e r c o n d u c t i n g .
2 . The C r yo t ro n a s a Dev i ce
2 . 1 S t a t i c C h a r a c t e r i s t i c s
T he r e s i s t a n c e o f t h e c e n t r a l w i r e o f a t y p i c a l c r y o t r o n i s
p l o t t e d a s a f u n c t i o n o f c u r r e n t i n t h e c o n t r o l w i n d in g i n F i g u r e U . T he
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Memorandum 6M-38Ii3 Page h
current.
The magnetic field, H, at the surface is given by:
where H is in ampere-turns per meter
I is in amperes
d is in meters.
If H is given in oersteds, I in amperes, and d in mils (thousandths
of an inch) this becomes
H
= 157.5 j
oersteds d mils
It will be noted that the transition characteristics are very
sharp for high gate currents. The additional sharpness is a peculiarity
of the measuring technique wherein a current is passed through the gate
circuit and the voltage across the gate circuit is measured. When resis
tance suddenly appears, I^R loss in the gate circuit causes heating which
lowers the critical field and speeds switching.
The magnetic field due to the control winding is along the axis
of the central wire while the self-field of the wire due to its own current
is tangential to the wire. Tne two fields thus add in quadrature and the
resulting net field is the vector sum of two fields. Results indicate
that the superconducting central wire reaches its critical field when the
net field reaches a certain value, regardless of which way the net field
points in relation to the center line of the wire. In one experiment,
the curves of Figure
k
were reproduced exactly for all four combinations
rrd
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c u r r e n t th r e s h o ld th an th e f i r s t c r y o t r o n c o u ld h a n dle th ro u g h i t s
s u p e r c o n d u c t in g g a te c i r c u i t .
The c o n t r o l f i e ld i s r e l a te d to th e c o n t r o l c u r r e n t b y th e
number of tu rn s per inch in the co ntr o l winding , and the se l f f i e l d i s
re la ted to the ga te cur ren t by the d iamete r o f wire used in the ga te
c i r cu i t . Cur ren t ga in , K, i s simp ly g iven by :
I
=
Kd
I
For a given pi tc h c on tro l wind ing and a given gat e wire diam ete r , the
c u r r e n t g a in i s s p e c i f i e d . F ig u r e 5 i s a p l o t o f l in e s of c o n s ta n t K a s
a func t io n of winding p i tch and ga te wire d iam ete r . For th e c ryo tron
who se c h a r a c t e r i s t i c s a r e p l o t t e d i n F ig u r e U# K • 7 . The c u r r e n t
ga in ac tu a l ly observed for a g iven c ryo tron is o f ten le ss than ca lcu la t ed ,
presumably due to the co ns tr i c t io n of sup ercu r ren ts by smal l normal reg ion s
which nu c le a te about f laws in the wire sur f ace . Co ntro l-cu r ren t th re sho ld
p o in t s th u s fo rm a lo c u s in th e g a t e c u r r e n t - c o n t r o l c u r r e n t p la n e wh ic h
l i e s on an e l l i p s e of s ma l le r ma jo r -to - min o r a x i s r a t i o .
2 .3 Power Gain and i/R Time Constant
The input power to a cryotron, exclusive of eddy current and
r e l a x a t i o n lo s s e s , i s the p r o d u c t o f th e e n e r g y s to r e d in th e ma g n e ti c
f ie ld of the control winding and the f requency at which the control wind
ing i s en erg ized :
2
f L I
c c
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Power gain, G, can be approximated by:
X
V J 2
R
power out
m
g ii „ 1 / g \ g
power i n ,
T T
2 f l l / L
f I * *0 c
c c
In the pulse circuits of section 3* the gate current of one
cryotron becomes the control current of another^ I • I • For this condi
tion, the frequency at which the power gain becomes unity is:
R
f = _£
max L
c
which is the reciprocal of the L/R time constant of the circuit. The L
and R are on different cryotrons, but since large numbers of identical
cryotrons are involved, one can speak of the L/R time constant of a given
cryotron as being the fundamental time constant of the circuitry.
If a given cryotron is made longer while holding the pitch of
the control winding constant, the resistance and inductance increase
together such that the l/R time constant is not affected. The L/R time
constant is thus independent of cryotron length.
If the diameter of a given cryotron is made smaller while
holding the pitch of the control winding constant, the resistance increases
inversely as the diameter squared, while the inductance decreases directly
as the diameter squared. The i/R time constant thus decreases as the
fourth power of the diameter.
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C ir cu i t speed can a ls o be inc rea sed by us i ng a ho l low ce n t ra l
w i r e . Su p e r c o n d u c t iv i ty i s a s k in e f f e c t , p e n e t r a t in g b u t a few h u nd re d
atom la y er s , and th ere for e the core of a w ire can be removed and the wir e
w i l l s t i l l h av e z e ro r e s i s t a n c e i n i t s su p e rc o n d u ct i ng s t a t e . The r e s i s
tance in the normal s t a te , however , w i l l be h igh er by the ra t io of the
o r ig in a l c r o s s - s e c t io n a l a r e a to th e new c r o s s - s e c t io n a l a r e a . The c o r e
need no t ac tu a l ly be removed, p rov ided i t i s made to have a r e l a t iv e ly
h i g h r e s i s t i v i t y . W ire w i t h a h i g h - r e s i s t i v i t y c o re a nd a s up e rc o n d uc t in g
s h e l l c an b e f a b r ic a te d b y v a p or p l a t in g .
2.U Eddy C urr en ts
I t has been shown in Faber t h a t th e dela y, c , due to eddy
c u r r e n t s in th e d e s t r u c t io n o f s u p e r c o n d u c t iv i ty o f a w i r e b y a lo n g i tu d in a l
m a g n et ic f i e l d i s :
2
T - con st. K
d
. A
e
/>
U - H
c
)
wher e H is the external magnetic field, H is the threshold magnetic field
an d
/°
is the resistivity. The switching time varies directly as the square
of the diameter and inversely as the resistivity, and is a function of the
amount by which the threshold magnetic field is exceeded.
As the circuits of section 3 are speeded up by making cryotron
diameters smaller, there will be a speed range where eddy currents become
important. Lowering the diameter still further and increasing the pitch
proportionally should then increase the speed as the inverse square of the
diameter, since both circuit L/R time constants and eddy current time
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with a current gain of two. As soon as a superconducting path is estab
lished over the surface of the wire, the cryotron is in its superconducting
stat e—even if the center of the wire requires additional time to become
superconducting. While it is not anticipated that this transition will
be a major source of delay, it is interesting to note that this delay is
one which depends on the length of the cryotron.
As circuit speeds are increased by increasing the resistance of
the central wi re , thereby shortening l/R circuit time constants and
minimizing eddy current effects, a fundamental limit to the ultimate speed
exists in the form of relaxation losses. The exact frequency repion in
which these losses will become predominant is not known , but from experi
ments with superconducting coaxial cable and wave guide resonators, an
estimate is available which places the limit between 100 megacycles and
1P00 megacycles.
3. Cryotron Computer Circuitry
The low impedance level of cryotron circuitry dictates a high-
impedance power supply (current source) with circuit elements connected
in series. Each element allows the current a choice among two or more
paths only one of which is superconducting; all of the current flows
through the superconducting path. The current encounters zero back voltage
except when the paths are changing. The standby pcwer is therefore zero.
Several circuits, representative of those found in digital computers, are
described below.
3.1 Flip-Flop
A b is ta b le elem ent , one of the most common in a di g i ta l computer,
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c r y o t r o n s i s r e s i s t i v e a n d t h e o t h e r i r s u p e r c o n d u c ti v e o The g a t e c i r c u i t s
a r e j o i n e d a n d a r e a d - o u t c u r r e n t p u l s e i s a p p l i e d a t t h e j u n c t i o n . The
r e a d - o u t p u l s e w i l l ch o o se o n e p a t h o r th e t h e r , d e p e n d i n g o n t h e s t a t e
o f t h e f l i p - f l o p . The f l i p - f l o p w i t h r e a d - i n a nd r e a d - o u t c r y o t r o n s i s
shown i n F i gure 6 .
A ny n um b er o f i n p u t c r y o t r o n s c a n b e a d d e d i n s e r i e s w i t h t h o s e
a l r e a d y d e s c r i b e d ( F i g u r e 7 ) t o s e t th e f l i p - f l o p t o o ne s t a t e o r t h e
o t h e r . C o n n e c t e d a s s u c h , t h e y a r e OR g a t e s ; a n y o n e o f th em a c t i n g a l o n e
c a n s e t t h e f l i p - f l o p . S i m i l a r l y , a d d i t i o n a l c r y o t r o n ; c a n b e a dd ed w i t h
t h e i r g a t e c i r c u i t s i n p a r a l l e l w i t h t h e c o n t r o l w i n d i n g o f th e i n p u t
c r y o t r o n a l r e a d y d e s c r i b e d , b e h a v i n g a s AND g a t e s ( F i g u r e 9 ) . The f l i p -
f l o p s e t c u r r e n t i s b y p a s s e d t h r o u g h on e o r m o re o f t h e s e p a r a l l e l g a t e s
u n l e s s a l l of th em a r e r e s i s t i v e . T h is l a t t e r c o n n e ct io n i n v o l v e s s u p e r
c o n d u c t o r s i n p a r a l l e l , i n w h ic h c a se t h e c u r r e n t d i v i d e s i n v e r s e l y a s t h e
i n d u c t a n c e o f t h e p a r a l l e l p a t h s .
A d d i t i o n a l r e a d - o u t c r y o t r o n s ca n b e a d d e d i n s e r i e s w i t h t h o s e
a l r e a d y d e s c r i b e d . S i n c e t h e i r c o n t r o l w i n d i n g s a r e s u p e r c o n d u c t i n g , t h e
a d d i t i o n a l c r y o t r o n s do n o t a d d a n y r e s i s t a n c e t o t h e f l i p - f l o p . The
a d d i t i o n a l i n d u c t a n c e i n c r e a s e s t h e i / R t im e c o n s t a n t o f t h e c i r c u i t , h o w
e v e r , l e n g t h e n i n g t h e t r a n s i t i o n t im e b e tw e e n s t a t e s .
3 . 2 M u l t i v i b r a t o r
T h r ee f l i p - f l o p s m a de o f o n e - i n c h p i e c e s o f t h e c r y o t r o n s t o c k
w h os e c h a r a c t e r i s t i c s a r e g i v en by F i g u r e
h
h a v e b e en s t u d i e d i n a m u l t i -
v i b r a t i n g c i r c u i t ( F i g u r e 9 ) . The r e a d - o u t c r y o t r o n s o f f l i p - f l o p A a r e
c o n n e c t e d i n s u ch a w ay a s t o s e t f l i p - f l o p B t o t h e s t a t e o p p o s i t e t h a t o f
A . A s i m i l a r c o n n e c t i o n b e t w e e n B a n d C c a u s e s C t o a ss u m e t h e s t a t e
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The t i m e t a k e n f o r t r a n s i t i o n f ro m o n e t i m e p e r i o d t o t h e n e x t
i s a f u n c t i o n o f t h e t r a n s f e r c u r r e n t . I f t r a n s i t i o n o c c u r s a t a f i x e d
t h r e s h o l d c u r r e n t v a l u e , t h e f i n a l v a l u e o f th e r i s i n g c u r r e n t i n a g i v en
c o n t r o l w i n d i n g d e t e r m i n e s t h e f r a c t i o n o f t h e i / R t i m e c o n s t a n t r e q u i r e d
t o r e a c h t h a t t h r e s h o l d v a l u e . I f t h e f i n a l v a l u e i s ( a ) t i m e s t h e
t h r e s h o l d v a l u e , t h e t im e r e q u i r e d t o r e a c h t h e t h r e s h o l d i s g i v e n b y :
t • i / R l n ( a / a - l ) . T he p a r t i c u l a r m u l t i v i b r a t o r c i r c u i t d e s c r i b e d c o m p le te s
t h e r o u n d - t r i p t h r o u g h i t s s i x t im e p e r i o d s a t t h e r a t e o f 1 0 0 t o 1 ,0 0 0
t i m e s p e r s ec o nd d e p e n d i n g o n t r a n s f e r c u r r e n t . H ie h i g h e r f r e q u e n c y
g i v e s i n d i v i d u a l t i m e p e r i o d s of 16 7 m i c r o s e c o n d s d u r a t i o n .
To m o n i t o r t h e t r a n s i t i o n s o f o ne o f t h e f l i p - f l o p s , a n a d d i t i o n a l
c r y o t r o n g a t e i s a d d e d w i t h i t s c o n t r o l w i n d i ng i n s e r i e s w i t h o n e s i d e
o f t h e f l i p - f l o p . A c u r r e n t s o u r c e i s c o n n e c te d t o i t s g a t e c i r c u i t . W hen
t h e c o n t r o l c u r r e n t i s z e r o , t h e g a t e c i r c u i t i s a s u p e r c o n d u c t o r a nd t h e
v o l t a g e i s z e r o . W hen t h e c o n t r o l c u r r e n t r e a c h e s t h e t h r e s h o l d v a l u e ,
t h e e ja te c i r c u i t b e co m es r e s i s t i v e a n d d e v e l o p s a v o l t a g e w h i c h i s a m p l i
f i e d a n d d i s p l a y e d . T y p i c a l v a l u e s a r e : R
c
0.01 ohm, I • 100 ma;
V * 1 m i l l i v o l t . T he ta m e c u r r e n t w a ve fo rm i s n o t p r e s e r v e d b y t h e
m o n i t o r i n g g a t e d u e t o i t s i n h e r e n t n o n l i n e a r i t y p l u s t h e s h a r p e n i n g o f
i t s t r a n s i t i o n du e t o l 2 R h e a t i n g a s i t be co m es r e s i s t i v e .
3 . 3 M u l t i t e r m i n a l S w i tc h
D i s t r i b u t i n g a p u l s e am ong s e v e r a l w i r e s c a n b e a c c o m p l i s h e d b y
a c r y o t r o n sw i t c h ( F i g u r e 1 0 ) . I n f o r m a t i o n i s f e d i n t o t h e s w i t c h f ro m
c r y o t r o n f l i p - f l o p s , h e r e r e p r e s e n t e d b y t o g g l e s w i t c h e s . O ne f l i p - f l o p
c a u s e s t h e od d o r e v en ro w s o f t h e s w i t c h t o b e r e s i s t i v e , a s e co n d f l i p -
f l o p c a u s e s o dd o r e v en p a i r s t o b e r e s i s t i v e , a t h i r d f l i p - f l o p c a u s es
o dd o r e ve n f o u r s t o b e r e s i s t i v e , a n d s o o n . A s i n g l e p a t h s u r v i v e s
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INPUT
A
1
0
1
0
1
0
1
0
INPUT
B
1
1
0
0
1
1
0
0
CARRY
IN
1
1
1
1
0
0
0
0
SUM
1
0
0
1
0
1
1
0
CARRY
OUT
1
1
0
1
0
0
0
Table n . Binary Add ition Table
the sum f l ip - f lo p to i t s proper s t a te . A s im i lar group of ga tes develops
the carry for the fo l low ing stage . Note that a l l c ir cu i ts are in se r ie s
from a current source power supply.
The foregoing binary adder des ign i s described to i l lu st r a te
the way in which switch es and gate s can be interco nn ected . A design having
fewer cryotron s per stage is av ail ab le wherein the carry is handled by a
la tt ic e network shown in Figure 12. The la be l beside each of the s ix
con trol windings ind ica te s when i t i s to be ener gized . The A • B • 0 and
A • B • 1 windings can each be made of two cryotr ons in a p a r a ll e l AND
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- J*
Memorandum 6M-38U3 Pa ge 12
3.fp S t e p p i n g R e g i s t e r
S t e p p in g r e g i s t e r s a r e com monly u s e d f o r r e c e i v i n g d i g i t a l
i n f o r m a t i o n i n s e r i a l f or m a t o ne p u l s e r e p e t i t i o n f r e q u e n c y an d a f t e r a
p r e d e t e r m i n e d n um b er o f b i n a r y b i t s ha v e b e en s t o r e d , s h i f t i n g t h e i n f o r m a
t i o n o u t a t a d i f f e r e n t f r e q u e n c y . A s e c o n d common u s e f o r s h i f t i n g
r e g i s t e r s i s t o a c c o m p l i s h th e c o n v e r s i o n b e tw e e n d i g i t a l i n f o r m a t i o n i n
s e r i a l a n d p a r a l l e l f o r m . T he s t e p p i n g r e g i s t e r s i n common u s e a r e m ade
o f v ac uu m t u b e s , t r a n s i s t o r s , o r m a g n e t i c c o r e s . C r y o t r o n s ca n a l s o be
u s e d i n t h e sam e s e r v i c e . E a ch s t a g e o f t h e s h i f t r e g i s t e r c o n s i s t s o f
tw o c r y o t r o n f l i p - f l o p s w i t h r e a d - i n an d r e a d - o u t c r y o t r o n s . O ne t r a n s f e r
c i r c u i t s e t s t h e s e c o n d o f t h e tw o f l i p - f l o p s o f e ac h s t a g e t o c o r r e s p o n d
t o t h e s t a t e o p p o s i t e t h a t o f t h e f i r s t . The c o u p l i n g l i n k t o a c c o m p l i s h
t h i s i s s i m i l a r t o t h e o n e d e s c r i b e d i n s e c t i o n 3» 2 w h i ch i n t e r c o n n e c t s
s t a g e s o f t h e m u l t i v i b r a t o r . A s ec on d t r a n s f e r c i r c u i t s e t s t h e f i r s t
f l i p - f l o p o f e a ch s t a g e t o c o r r e s p o n d t o t h e s t a t e o p p o s i t e t h a t o f t h e
s e co n d f l i p - f l o p o f t h e s t a g e to i t s l e f t . A l i n e o f s u ch s t a g e s s e r v e s a s
a s h i f t i n g r e g i s t e r , c a p a b le o f s h i f t i n g d i g i t a l i n f o r m a t i o n to t h e r i g h t .
I n f o r m a t i o n ( ON E'S o r ZE RO 's) f e d i n t o t h e f i r s t f l i p - f l o p i n s y n c h r o n i s m
w i t h t h e s e c o n d o f t h e t wo t r a n s f e r p u l s e s ( c a l l e d ADVANCE B p u l s e ) , w i l l
a d v an c e t h r o u g h t h e s t e p p i n g r e g i s t e r o n e s t a g e f o r e a c h p a i r o f t r a n s f e r
p u l s e s , ADVANCE A an d ADVANCE B, which ar e d is p la c e d in t im e. F ig u re lU
s ho ws tw o s t a g e s o f a c r y o t r o n s t e p p i n g r e g i s t e r . P a r a l l e l o u t p u t g a t e s
are not shown.
3 . 6 C o i n c i d e n t - C u r r e n t C i r c u i t s
M any i n t e r e s t i n g c i r c u i t s c a n b e m ade o f c r y o t r o n s w i t h tw o o r
m o re c o n t r o l w i n d i n g s w ou nd o v e r e ac h o t h e r i n s u c h a w ay t h a t t h e n e t
m a g n e t i c f i e l d a f f e c t i n g t h e c e n t r a l w i r e i s du e t o t h e sum o f t h e m a g n e t i c
f i e l d s o f t h e i n d i v i d u a l w i n d i n g s . The d - c c r y o t r o n c h a r a c t e r i s t i c s of
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Memorandum 6M-38U3
Page 13
U . E n g i n e e r i n g a C r y o t r o n S y st em
U«l Low-Tempera tu re Env i ronm ent
T he m o s t u n u s u a l r e q u i r e m e n t of a c r y o t r o n s y s t em i s t h a t i t
o p e r a t e a t a t e m p e r a t u r e n e a r t h e a b s o l u t e z e r o . T en y e a r s a g o t h i s
r e q u i r e m e n t w o u l d h a v e p r e c l u d e d s e r i o u s t h o u g h t of s uc h a s y s t e m .
T o d ay , h o w e v e r, s u ch a n o p e r a t i n g t e m p e r a t u r e i s r e l a t i v e l y e a s y t o
ac h i e v e . ^ Th i s change i s ma i n l y due t o t he work of Samuel C . C o l l i ns
w ho se h e li u m l i q u i f i e r s r e v o l u t i o n i z e d t h e f i e l d o f l o w - t e m p e r a t u r e
p h y s i c s . A r t h u r D. L i t t l e , I n c . o f C a m br id g e, M a s s a c h u s e t t s , h a s b u i l t
s e v e n t y C o l l i n s h e li um l i q u i f i e r s o f a b - l i t r e - p e r - h o u r c a p a c i t y . The
l i q u i f i e r a t M . I . T . l i q u i f i e s 27 l i t r e s p e r h o u r . S t o ra g e o f l i q u i d h e l iu m
h a s a l s o i m p r o v e d . C o m m e r c ia l ly a v a i l a b l e d o u b l e D e w ar s w h i c h u s e l i q u i d
n i t r o g e n i n t h e o u t e r D ew ar l o s e l e s s t h a n o ne p e r c e n t of t h e i r l i q u i d
h e l i u m p e r d a y .
T he h e a t d i s s i p a t e d b y a c r y o t r o n s y s t e m c a u s e s e v a p o r a t i o n o f
t h e h e l i u m . I f t h e a v e r a g e p o w er d i s s i p a t e d p e r c r y o t r o n i s 1 0~ k w a t t ,
a n e s t i m a t e b a s e d o n p r e s e n t e x p e r i m e n t a l u n i t s , a 5 , 0 0 0 - c r y o t r o n c o m p ut er
w o uld d i s s i p a t e o n e - h a l f w a t t . T he l a t e n t h e a t o f v a p o r i z a t i o n o f l i q u i d
h e l iu m a t U .2 K i s 5> c a l o r i e s p e r g r a m , i t s d e n s i t y i s 0 » 1 2 5 7 , an d t h e r e
f o r e o n e - h a l f w a t t c o r r e s p o n d s t o a n e v a p o r a t i o n r a t e of 0 . 9 3 l i t r e p e r
h o u r . A c o n t i n u o u s s y s t e m w h i ch r e c y c l e s h e l i u m w o u l d b e m o s t e c o n o m i c a l
f o r a s t a t i o n a r y i n s t a l l a t i o n ^ a t e n - o r t w e n t y - l i t r e c h a rg e a t t h e ti m e
o f l a u n c h i n g w o uld s u f f i c e f o r p o r t a b l e s y s t e m s .
The t e m p e r a t u r e o f a l i q u i d h e l i u m b a t h c an b e c o n t r o l l e d b y
c o n t r o l l i n g t h e p r e s s u r e o f t h e b a t h . T a b le I I I g i v e s t h e b o i l i n g p o i n t
o f h e l iu m a t v a r i o u s p r e s s u r e s . B elo w 2 . 1 9 K , t h e s o - c a l l e d l a m b d a - p o i n t ,
l i q u i d h e l iu m e x h i b i t s u n u s u a l p r o p e r t i e s w hi ch m ay p r o v e u s e f u l i n a
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Memorandum 6M-38U3 Pa ge Hi
Pr e s s u r e
mom. Hg.
0.001
0 .0 1
0 .1
1 .
10.
100.
200.
300.
Uoo.
5oo.
600.
700.
710.
Temperature
degrees K
0.657
0.791
0.982
1.269
1.71.3
2.638
3.067
3.368
3.605
3.803
3.975
U.127
u.ua
Pr e s s u r e
num. Hg„
72 0
o
730.
7U0.
750.
760.
770.
780.
790.
800.
900.
1000.
1500.
1720.
Temperature
degrees K
U.156
li .170
U.18U
U.198
l i .211
U.225
U.239
U.252
U.266
h.UO
li.52
5.03
5 .20
Table i n . Bo i l ing Poin t o f He lium
U«2 P hys ical Co nstru ction
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Memorandum 6M-38U3 Page 15
extreme lew temperatures. Some are relatively good thermal insulators
(stainless steel and cupro-nickel) and may be used for mechanical support.
There is no basis for the common impression that everything falls apart
just below JAN specifications (-85 C) .
U.3 Input, Output, and Power Supply
Input pulses to cryotron circuits involve current amplitudes
which are easily achieved in the terminal equipments commonly associated
with digital computers. Since the voltage level is low, input of informa
tion to a cryotron system involves no unusual problems.
Connecting the output pulses of a cryotron system to terminal
equipment, on the other hand, is difficult due to the low power level of
the cryotron circuitry. Power cryotrons can be designed to increase the
power level, but it appears that vacuum-tube or transistor amplifiers
are necessary to bring the level up to that of most output equipments.
Magnetic amplifiers with superconductive control windings are an interest
ing possibility for power amplification.
Power supplies for cryotron systems are easy to achieve. The
low impedance of the circuitry dictates a current-source power supply.
A battery with a series resistance is adequate.
>. Conclusion
The cryotron in its present state of development is a new circuit
component having power gain and current gain so that it can be used as an
active element in logical circuits. It is easily and inexpensively
fabricated from commercially available materials and its size is small.
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Memorandum 6M-38I;3 Pa ge
16
D r a w i n g s A t t a c h e d :
F i g u r e
1
C-6333k
F i g u r e
2
A-63O87
F i g u r e 3 A-63088
F i g u r e
B-63091
F i g u r e 5 B-63U9I
F i g u r e
6
A-63090
F i g u r e
7
C-6329U
F i g u r e
8
C-63291
F i g u r e
9
C-63293
F i g u r e 10 C-63292
F i g u r e
11
C-63338
F i g u r e 12 B-63335
F i g u r e
13
C-63336
F i g u r e
lit
C-63337
F i g u r e
15
A-63679
F i g u r e
16
A-63678
D i s t r i b u t i o n L i s t :
Group
63
S t a f f
Group
35
S t a f f
Group 65 S t a f f
M.
A.
H e r l i n
D 321
B .
G.
F a r l e y
R.
P.
Mayer
» L. L. S u t r o
R.
F.
J e n n e y
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C 63334
F 2969
SN - 1220
H
c
GA U S S
FIG . I
1000
900
800
700
600
500
400
THRESHOLD
MAGNETIC FIELD
3 0
°
vs TEMPERATURE
2 0
°
FOR SE VE RA L ,oo
COMMON
SUPERCONDUCTORS
2 3 4 5 6
T E M P E R A T U R E °K
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A - 6 3 0 8 7
F 2862
SN-1169
H
N O R M A L
R E G I O N
SUPERCONDUCTING
REG
I
ON
4.2° K
FIG. 2
T H R E S H O L D M A G N E T I C F I E L D
A S A F U N C T I O N O F T E M P E R A T U R E
F O R A S U P E R C O N D U C T O R
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•
I
r\
£\
n n n
n
)
S I N G L E C R Y O T R O N
F I G . 3
C R YO T RO N B I S T A B L E E L E M E N T
( F L I P - FL O P )
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B 63091
F 2865
SN 1172
*
r €
n
rj
S I N G L E L A Y E R . 0 0 3 N I O B I U M
0 0 9 T A N T A L U M
.01
n
u
n
.0075
h
9 .005
OHMS
.0025
CRYOTRON GATE
vs.
CONTROL
100
2 0 0 3 0 0
I M I L L I A M P E R E S
c
RES
I
S T A N C E
CURRENT
400
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B 63491
F 2974
SN - 1225
5 0 0
4 0 0 -
C O N T R O L
3 0 0 -
W I N D I N G
PITCH ru
T U R N S
2 0 0
PER INCH
100 -
0
1 2 3 4 5 6 7 8
C E N T R A L W IR E D I A M E T E R ~ M I L S
CURRENT GAIN vs CONTROL WINDING
PITCH AND CENTRAL WIRE DIAMETER
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A - 6 3 0 9 0
F-2864
SN-1171
ZE RO INPUT I ONE INPUT
9 9 SUPPLY 9 o
€
a
a
€
a
a
n
{I
r
D
a
D
a
D
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TJ TJ
SUPPLY
a
u
n
u
JH
n
£
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H - Q
1
n
CJ
n
D
n
u
a
u
}
u
ONE
O U T P U T
C R Y O T R O N
C R Y O T R O N S
READ
F I G .
G
F L I P - F L O P
t
ZERO
OUTPUT
WITH READ - IN
AND RE A - OU T C RY OT RO NS
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
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C-63294
F 2968
SN 1219
A
C
c
)
I)
• )
Z E R O
I N P U T S
o -
B
o -
X
c
c
c
)
)
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S U P P L Y
S U P P L Y
O N E
N P U T S
W I T H
C R Y O T R O N FL I
P-FLOP
O R G A T E S
IN
B O T H
SI
D E S
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
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C 63291
F 2965
SN 1216
I
S U P P L Y
Z E R O
C
I N P U T C
D
ONE
P I N P U T
d
(CD,
D
D
B
C
C
d
Y
D
D
I N PU T
P U L S E
S U P P L Y
F l C i . U
C R Y O T R O N F L I P - F L O P
W I T H
AND
G A T E S
IN ONE
S
I DE
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
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o
Q .
o
CD
a
o
_i
u.
i
0 .
tr
h-
<
cr
DQ
>
o
or
h-
o
> -
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
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C-63292
F-2966
S N - 1 2 1 7
r-C
•S
€
€
€
•a
€
R E A D
n n
TD O
o n
era
O-
Q .
LTD
n n
era
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L T U
CL
n.
era
1
cnx
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4
a
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t r o
n n
t3TD
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T)
p_
TJ
n n
era
^ C ON T R O L J ^
O Q
U~U
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Q Q
Cr t7
I
C O N T R O L
Q- Q
cr
p_
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Crcr
Q Q
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8 POSITION
C R Y O T R O N S W I T C H
-°
o
I
-o
2
-°
3
-o
4
-o
6
•o 7
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C - 6 3 3 3 8 * *
F 2973
SN - 1224
CARRY
OUT
SUM
FLIP-FLOP
00 00 Oo 00
0 1 0 I
A INPUT B INPUT
CARRY
IN
ONE STAGE OF A BINARY ADDER
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
APPROVED FOR PUBLIC RELEASE CASE 06 1104
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B 63335
F 2970
SN-1221
W
A = B = 0
? Q n
a
FIG.
12
CARRY NETWORK
o o
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
APPROVED FOR PUBLIC RELEASE CASE 06 1104
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C-63336
F 2971
SN 1222
*
I CARRY
OUT
J21
A=l
r€
— •
u
D-
U~
CT
^ X B=0
m̂
- « - •
0 CARRY
OUT
iK
n
L
Q
i
r
u
B
n
b
n
n
y l
0
0 0
B
0
B
l
A=l
T 7
^ S ^
/
0 \ i
T 7
- Q
SUM
F L I P -
FLOP
€
O O
A= B
A * B
BINARY ACCUMULATOR STAGE
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
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in
H i
T 7
cr
^b^££
a o
• c r
i O .
<
u_
o
CO
j LU
] o
8
<
h-
(X)
cr
LU
K
CO
CD
LU
cr
o
z
CL
Q_
LU
co
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.
APPROVED FOR PUBLIC RELEASE CASE 06 1104
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A - 6 3 6 7 9
F I G .
15
EXPERIMENTAL CRYOTRON CIRCUITS
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APPROVED FOR PUBLIC RELEASE CASE 06 1104
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A - 6 3 6 7 8
*
FIG. 16
3 - CRYOT RON- F L I P- F LOP M ULT I V I BRAT OR
APPROVED FOR PUBLIC RELEASE. CASE 06-1104.