Post on 18-Mar-2020
LA-5050-PREPORT
Electroexplosives Safety Qualifications
July 1 through August 31, 1972
I
I
JIa amosscientific laboratory
of the University of CaliforniaLOS ALAMOS, NEW MEXICO 87S44
UNITED STATES
ATOMIC ENERGY COMMISSION
CONTRACT W-740 S-ENG. 36
●
R&D CONTRACT STATUS REPORT
FOR
EVALUATION OF ELECTROEXPLOSIVE DEVICE (EED)RESPONSE TO ELECTROMAGNETIC RADIATION (EMR)
—-
~:LT- ‘“’
L~g-.Em ““‘–”— —.- -
Project 5610
Task 01
Period 1 July through 31 August 1972
Los Alamos Scientific Laboratory-Under AEC Contract W-7405-ENG-36. .
.-. ..
—for _— r.
Department of the Air ForceA@ Force Systems Command
Aeronautical Systems Division
-.
-.
.. ..
2.
PROJECT 5610, TASK 01
This project report
1972. Activity for this
eral areas:
1.
2.
3.
4.
5.
is for the period 1 July through 31 August
period was primarily in the following gen-
Addition of thermal time constant and EMR susceptibility/
status columns to the EED listings. ,The most current list-
ing, in three formats, is included as Attachment 1 to this
report. Also included are
which were not included in
RF firing test data.
photographs of additional EEDs
the March-April progress report.
RF field measurement instrumentation.
Antenna modeling.
Miscellaneous activities.
These various activities.
sections of this report.
There has been some
are reviewed in detail in the following
reorganization at LASL, but the conduct ofProject 5610, Task 01 will not be affected. Correspondence on the
project, however, should be addressed to WX-7 (formerly GMX-7).
I. ADDITIONS TO EED LISTING
As mentioned in the May-June 1972 progress
constants of several EEDs have been measured at
report, thermal time
approximately the dc
no-fire current level using an electrothermal bridge circuit.$e
While not extremely accurate in some cases, and considering that the
thermal time constant changes with current levels, these data are,
nevertheless, considered to be of sufficient importance to be in-
cluded in the electrical characteristics of EEDs. A column for this
information has been provided in the electrical characteristics● format, giving the thermal time constant in seconds.
~ 3:NASATR 32-1494, “Nondestructive Testing ok Insensitive ElectroexplosiveDevices by Transient Techniques”, JPL, July 1970.
Rosenthal, L. A., “ElectroexplosiveDevices”, IEEE Transactions onInstrumentationand Measurement, June 1965.
1
5
An attempt has been made to classify EED EMR susceptibility
status of EEDs in the inventory. Inasmuch as EED RF sensitivity
to date has been found to correlate with the dc sensitivity, the
following classifications,based on dc no-fire current ratings,
have been given:
dc No-fire Current Rating
0.1 ampere or less very sensitive0.5 ampere or less not recommended1.0 ampere or greater recommended0.5 to 1.0 ampere no statementunknown unknown characteristicsexperimental under development
Particular mention was made of the Mk 71 detonator sensitivity
in the May-June report. Further contact with the Naval Weapons
Laboratory, Dahlgren, Virginia has disclosed no EMR hazard problems
with this detonator> primarily because it is p=t of a mechanically
rotated safe-arm unit suitably shielded within a weapons system.
Its low firing energy is required by system constraints. Courtesy
of NWL, several of the LASL-tested EEDs and the systems in which
they appear are listed below:
Mk 71 Detonator Mk 1 Squib
The GG20D3
sitive, but the
squib operation
Sidewinder (AIM-9) “ 2.75 in. FFARChaparral ZuniSparrow (AIM-7) Sidewinder-lCShrike (AGM-45) Mk 44 TorpedoNATO SeasparrowBasic Point Defense Mk 2 Sauib
(AIM-9c)
Standard Arm (AGM-78)Standard Missile
Mk 23 JATO
Phoenix (AIM-54)ASROC (RUR-5)
Mk 52 Mine “BUnpUP (AGM-12)
Mk 57 MineBUHPUP (AGM-12)
gas generator has also been found to be quite sen-
only known USAF application is one in which parallel
reduces the sensitivity. The GG20D3 is found in
3.
the AGM-28B M5B1 thermal battery (part number 019-NA-01 or GAP 4019-7,
FSN 6135-483-4629 or 1336-650-0801). Average minimum all-fire current
for a single GG20D3 gas generator is 0.160 ampere. Average firing
4.
.
current (obtained from test-firings of out-of-date batteries supplied
by SAAMA) was 0.476 ampere for the GAP 4019-7 batteries. Per T.O.
llN-C5013-2, three squibs are wired in parallel for battery activa-
tion. As a matter of general interest, the battery activation
times (from squib firing to 28 volt constant terminal voltage) are
on the order of 300 milliseconds. Under a
the 28 volt terminal voltage is maintained
dicating a nominal l-ampere-hour capacity.
of 100 amperes have been obtained from the
ceeding one second.
constant l.1-ampere load
for one hour, thus in-
Peak currents in excess
batteries for times ex-
A similar squibs-in-parallel installation appears in the
AGM-28B Explosive Switch Box where twelve 0M351C (FSN 1336-515-5492)
explosive switches are wired in parallel. Testing results of the
characteristics of individual switches will be given’in a later re-
port. Preliminary indications are that 25 kV electrostatic (pin-to-pin
and pin-to-case) and dc firing characteristics are satisfactory.
Four carbon bridge EEDs appear in the current data listing.
Carbon bridge devices are normally not recommended because of the
ease with which relatively high voltages can be developed (because
of the characteristic high bridge resistance).
System Nominal Bridge Resistance (ohms)
1336-776-6731 M52 Fuze pistol ASM-4F/G 1,000 - 10,0001336-152-3304 Fuze AIM-9/B/E/J 2,000 - 5,000P/N 779658 Detonator AIM-9/B/E/J 700 - 15,000M52-A-3B1 Primer, electric 20 mm 1,000 - 12,000
II. RF FIRING TEST DATA
In testing for RF susceptibility, we have previously used ten EEDs
exposed to an RF power level equal to that of the dc mean. In no case
were firings observed, thus allowing a conclusion (with 5.5% risk)
that the RF mean was higher than the dc mean. It is, however, highly
desirable to obtain data on the actual level at which firings occur.
The problem is that a sufficient number of EEDs are usually not avail-
able to permit statistically precise data for the various frequencies
and various firing modes (Consider, for example, four frequencies and
pin-to-pin and pin-to-case modes; at 30 samples, for a Bruceton test,
5.
240 EEDs would be required.). We have examined other statistical
methods which might be applicable for small samples without much
success.>: It appears that a method wherein the stimulus (power
level) is continuously applied and gradually increased until firing
occurs offers about the only alternative. The data sheets presented
in the following pages were obtained in this manner. Ten samples
of each device were used for each mode; the maximum power level,
minimum power level, and average firing levels are plotted. These
data are being examined for statistical properties (standard devi-
ation, confidence level, etc.) in comparison with dc Bruceton test
data for the same devices.
III. RF FIELD MEASUREMENT INSTRUMENTATION
As mentioned in the May-June 1972 progress report, firings
in a “free-field” RF environment have been induced, but instrumen-
tation to determine the exact electric field intensity has given
widely varied results. Although this “free-field” radiation was
not directly a part of the original statement-of-work, it is con-
sidered an important supplement to the direct-drive RF firings
and network analyzer facets of the program, and is therefore being
continued. The discovery that a full-wavelength antenna was the
most susceptible lead configuration (at the MSR frequency) is a
significant example of the benefits derivable from experiments
performed in a free-field RF environment.
Using a Sandia Laboratories development~s$~as a start, a diode-
detector unit more suited to high intensity E-fields, together with
a dipole power-meter probe, are being calibrated at various fre-
quencies in a parallel plate transmission line facility similar to
that used by Sandia. Calibration results to date appear promising,
and reasonable correlatioriof peak and average field intensities
with firings is anticipated by the next report.
.
~A Reliability Test Method forNo. U-1792, August 10, 1972.
$~:SandiaReport, SC-DR-71 0219,July 1971.
t!one-shot!l Items, Aeronutronic publications
“Radio Frequency E-Field Sensor”, J. C. Barnes,
6,
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15.
IV. ANTENNA MODELING
A mathematical model of a full-wavelength antenna is currently
being exercised with previous EED RF impedance data (see March-
April progress report, p. 4). A full-wavelength antenna was shown
(by free-field experiments at the MSR frequency) to be the most
susceptible configuration. The radiation resistance for such an
antenna is high, depending upon length-to-diameterratios*, and
the reactance changes from highly inductive to highly capacitive
at the full-wavelength frequency. Using typical 24 or 26 gage
leads (such as appear on Mk 1, Mk.2, Mk 71, GG20D3 EEDs), a radi-
ation resistance of about 900 ohms was calculated. The reactance
characteristics are such that a complex conjugate match may be
easily achieved and is therefore assumed. The induced voltage is
approximately twice that of a halfwave dipole. The new model is
then:
antenna
Power delivered
is placed in an
f MHz) may then
R
+jX EED
to the resistive part of the EED, when the antenna
electric field of E volts/meter (at a frequency of
be calculated,
v. MISCELLANEOUS ACTIVITIES
a. As mentioned in past reports, we will attempt to measure
the dielectric constant of some primary explosives, as a func-
tion of frequency, using the HP 8542A Automatic Network Analyzer.
Additional fixtures for the HP 8542A have been received and
have been forwarded to the Mason & Hanger - Silas Mason Company,
AEC Plant, Burlington for loading with lead styphnate, lead azide,
and a titanium potassium perchlorate compound.
*See, for example, Jasik, H., “Antenna Engineering Handbook”, McGraw-Hill,
1961, pp., 3-4, 3-5.
16.
b. Undesirable electrical characteristics of the hot-wire type
of EED (i.e., low energy pin-case firing, electrostatic firing,
etc.) are caused principally by three factors:
10 inherent sensitivity of primary explosives
2. undesirable properties of metal additives in
explosives (higher electrical conductivity,
lowered dielectric strength)
3. physical (geometric) properties of the bridgewire
arrangement such that high voltage arcs propagate
directly through the explosive.
All of these undesirable properties could be eliminated by the
use of secondary explosives only, combined with judicious header
design (such as that of the Mk 101 illustrated on Page 12 of the
January-February 1972 progress report). The difficulty is that
second~ explosives are not easily initiated by a hot bridge-
wire. Most EBW (exploding bridgewire) detonators use only sec-
ondary ‘explosivesbecause the firing pulse and subsequent sharp
bridgewire decomposition provide adequate thermal and mechanical
shock to initiate the secondary explosive.
Hot wire EEDs, using only secondary explosives, may be
feasible if a bimetallic bridgewire composite is used. Typical
of such bridgewire materials are palladium and aluminum, plat-
inum-aluminum, or ruthenium-palladium alloy and aluminum.
(Pyrofuze, a registered trademark of the Sigmund-Cohn Company,
is one of the bimetallic bridgewire composites commercially
available.) Bridgewires, such as I@ofuze, when heated to 6600C,
react by alloying violently and exothermically, resulting in
deflagration without support of oxygen. The reaction reaches
temperatures on the order of 2800°C, and the bridgewire is
always consumed. It is believed that such a reaction may be
sufficient to initiate secondary explosives and therefore serve
as the basis for a far less vulnerable EED. Principal disad-
vantages of Pyrofuze bridgewire devices are their relative slow-
ness (millisecond firing times) and high power requirements (when
compared with EBWS). We believe such disadvantages are not
17.
applicable to the typical aircraft application where firing times
need not be precise and where 28 volt - 10 ampere firing energies
are in common use with present EEDs.
We have obtained Pyrofuze wire samples of 0.020, 0.015, 0.010,
and 0.003 in. diameters. These will be mounted on test detonator
heads with bridgewire lengths of 0.090, 0.060, 0.040, and 0.030 in.
Electrical characteristics of these assemblies will be measured
and trial initiation of various suitable secondary explosives
will be examined. This effort is intended only as a rapid feasi-
bility investigation at this time.a
.
.
ATTACHMENT I
LISTING OF KNOWN
USAF
ELECTROEXPLOSIVE DEVICES
“
.
1.
EXPLANATION OF TERHS:
Electrical Characteristics:
Low resistance
High resistance
No-fire current
All-fire current
Normal use
Continuity test
Thermal time constant
EMR Susceptibility/Status:
Not recommended
Very sensitive
Recommended
Unknown characteristics
Experimeirtal
Removed from inventory
: Lower limit, nominal bridgewire re-sistance.
: Upper limit, nominal bridgewire re-sistance.
: -5 U current value in amperes (usuallycalculated from Bruceton test data,which accurately determines the meanfiring current value and an estimateof standard deviation (Y).
: +5 (Ycurrent value in amperes (de-termined as described above).
: Recommended firing current (usuallygreater than the all-fire current).
.!.
: Maximum allowable current recommended “ “for bridgewire continuity checks; thisvalue is typically limited to one-tenththe no-fire current value or less).
: A value (in seconds) determined ex-perimentally (at approximately the no-fire current value) which is equal tothe ratio of the equivalent heat ca-pacity Cp to the heat loss factor y;i.e., T =C /y.
fThe rate at which the
bridgewire emperature climbs, observedas a transient change, is directly re-lated to @T of the system. The methodused to determine ‘ris described inJet Propulsion Laboratory TechnicalReport 32-1494, “Nondestructive Test-ing of Insensitive ElectroexplosiveDevices by Transient Techniques”,July 15, 1970. See also Rosenthal, L. A.,“Electrothermal Measurements of Bridge-wi.resUsed in Electroexplosive Devices”,IEEE Transactions on Instrumentation andMeasurement, Vol. IM-12, No. 1, pp. 17-21,June 1963.
: dc no-fire current is .1 to .5 ampere.
: dc no-fire current is .1 ampere or less.
: dc no-fire current is 1 ampere or greater.
: Electrical characteristics (no-firecurrent) unknown.
: This device still under development.
: This device no longer stocked in USAFsupply system,
——
2.
Note that EEDs with no-fire currents between ,5 ampere and1 ampere bear no EMR status decimation unless the device hasbeen-found to ~ particularly RF-sensitive.RF sensitivities follow dc sensitivities asfire current level.
Part number :
Federal stock number :
System designation .:
Manufactmer’s
As a general rule,indicated by no-
part number.
Federal stock number of the EED (ifavailable as an issue item) or ofthe subassembly of which I:heEED isa part.
Weapons system designation (e.g.,C-5A) with which the EED is uniquelyidentified; in some cases (e.g.,AERO-27/A) the EED is used with aparticular ejection rack which mayfit several aircraft.
,,
..
*
.
.
The
1,
2.
3.
4.
15-86.
SUPPLEMENTARY INFORMATION ON IMPULSE CARTRIDGES
following text from T.0, 11-1-34 isprovided for
3.
information:
Present. The,explosive devices that are presently in the
inventory and the preferred item for jettisoning applicable
store.
Substitute. The explosive devices that are authorized
substitutes for the applicable preferred item for each
application.
Interim. Explosive devices now under development that are
intended to replace the applicable present devices as the
preferred item in the inventory (see paragraph t5-86).
Goal. Explosive devices not under development that are
intended to be the ultimate replacement as the preferred
item.
‘INTERIM”CARTRIDGES.
:artridges,listed as
The Mk 124 Mod O and Mk 125
“interim” devices, are under
Mod O impulse
development.
?irst procurement, which is expected in FY69, is dependent upon
development of an approved data package. The Mk 124 Mod O is
designed to replace the ARD 446-1 and Mk 9 Mod O impulse car-
tridges, and the Mk 1 Mod 3 in some applications. The Mk 125
Mod O is designed to replace the ARD 863-1 and Mk 2 Mod 1 im-
pulse cartridges. Complete replacement,in all applications
will depend upon results of the testing program.
15-87. “GOAL” CARTRIDGESo The CCU-9/B (MLU-34/B) and CCU-10/B
(MLU-35/B) are under development and are expected to be ready
for procurement in FY70. These cartridges are specifically
being developed for high temperatures, e.g., F-ill aircraft
application. The CCU-9/B is being designed to be inter-
changeable with the ARD 446-1 and Mk 9 Mod O, or the Mk 124
Mod O impulse cartridges. The CCU-10/B will be interchange-
able with the ARD 863-1 and Mk 2 Mod 1, or the Mk 125 Mod O
impulse cartridges. Replacement of the above “present” and
“interim” cartridges in all applications with the CCU-9/B and
CCU-10/B will depend upon cost and demonstrated performance
of the present and interim cartridges.
. ..—. —.
.
-.
4.
. .
The following text from T. O. 11A16-1-7 is provided for information:
2-36. IMPULSE CARTRIDGE INTERCHANGEABILITYDATA:
2-37. The Mk 2 Mod 1 and ARD 863-1 cartridges are interchange-
able in multiple ejector rack (MER) and triple ejector
rack (TER) applications on all applicable aircraft.
2-38. The Mk 2 Mod 1 and ARD 863-1 cartridges are interchange-
able in F-105 pylon stores ejector rack.
2-39. The Mk 8 Mod O and Mk 1 Mod 3 cartridges are interchange-
able in all applicable aircraft applications except re-
fueling hose guillotine cutters.
2-40. Two each CCU-1/B cartridges are interchangeable with one
each ARD 446-1 cartridge and one each ARD 863-1 cartridge in
MAU-12 pylon ejector rack application for F-ill and FB-111
Aircraft.
... -—- ..._
5..
IMPULSE CARTRI~GE APPLICATIONS
(Ref. T.O. 11-1-34, AFATLTR 68-58)
.
Rack
A/A 37B-1 Rack Bomb Ejector (MBR-l)(Navy)
BRU-3/A Rack Bomb Ejector (MER-1OO)
MAu-41/A Rack (MER 1-6)
MAU-42/A Rack Bomb Ejector (MER-1-4L)MAu-43/A “ “ 11 (mR-1-4R)
MAU-60/A Rack Bomb Ejector (TER-3)
MAU-61/A Bomb Ejector (MER-3 R & L)
MAU-63/A Bomb Ejector (MBR-3)
MAU-73/A Bomb Ejector (MER-3C)
Rack Bomb Ejector Aircraft (MER-9)
Rack Bomb Ejector dircraft (MER-1O)
Rack Bomb Ejector Aircraft (MER 10/A)
Rack Bomb Ejector Aticraft (TER-9)
Rack Bomb Ejector Aircraft (TER-9A)
Rack Bomb Ejector Aircraft (TER-15)
MAU-12 B/A Bomb Ejector
MAU-40/A Bomb Ejector
MAU-46/A Bomb Ejector
MAU-50/A Bomb Ejector
AERO-3/A Bomb Ejector
AERO-7/A Bomb Ejector
AERO-27/A Bomb Ejector
AERO-15/C-l Bomb Ejector
Wing Tank Pylon (outboard F-4C)
MAU-12 B/A Ejector
Pylon, Type Series (Mod O, Mod R)
30” Special Purpose
Wing Pylon
Fuselage Centerline Pylon
Fuselage Multiple Ejector Rack Pylon
C!al?t??id$?es
Mk 17
ARD-863, Mk 2, Mk 125
ARD-863, Mk 125
ARD-863, Mk 125, Mk 2
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
Mk 17
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-863, Mk 2, Mk 125
ARD-446, ARD-863, Mk 124, Mk 125, CCU-1/
ARD-446, ARD-863, Mk 124, Mk 125
ARD-863, Mk 2, Mk 125
ARD-446, ARD-863, Mk 124, Mk 125
Mk 1, Mk 2
Mk 1, Mk 2, Mk 8, Mk 10, Mk 51
Mk 1, Mk 2, Mk 124, Mk 125
Mk 13 Mod O
Mk 9 Mod O
ARD-446-1
ARD-446-1
EX-107 Mod 5
Mk2Modl
ARD-446-1, ARD-863-1
ARD-446-1, ARD-863-1
.
.
6.
Rack
Pylon, T$pe Series, I, II, III,IIIA, VII,VIII, IX, X ARD-446-1
Wing Tip Launcher!Red Dog Mkl Mod3
Centerline Multiple Weapon Pylon ARD-4f+6-1,ARD-863-1
Inboard Multiple Weapon Pylon ARD-446-1, ARD-863-1
Inboard Universal Pylon ARD-446-1, ARD-863-l
Outboard Universal Pylon ARD-446-1, ARD-863-1
.
.
.- ——
7.
CARTRIDGE LIST
FSN
13’77-516-9924
1377-585-9291
1377-183-5952
NSL
NSL
1377-162-7136
NSL
1377-293-8183
1377-724-9271
1377-293-8184
1377-894-5689
1377-075-5846
1377-731-9264
1377-793-9927
1377-707-0585
1377-021-4231
1377-632-8714
1377-115-3433
1377-952-3925
1377-193-8832
1377-193-8834
NSL
1377-739-5472
NSL
1377-870-9296
Nomenclatw?e
ARD-446-1
ARD-863-1
CCU-1/B
ecu-9/B (MLU-34/B)
ecu-lo/B (MLu-35/B)
ccu-16/B
EX-107 Mod S
Mk 1 Mod 3
Mk2Mod0
Mk2Modl
Mk 2 Mod 5
Mk8Mod0
Mk9Mod0
Mk 13 Mod O
Mk 17 Mod O
Mk 17 Mod 1
Mk 23 Mod O
Mk 51 Mod O
Mk 51 Mod 1
Mk 124 Mod O
Mk 125 Mod O
MLU-8/B
MLu-9/B
10!Ju-11/c
MLu-12/c
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