Neither the United States Governmentnor any agencythereof, nor asryof their employees,makesJny warranty, expressor implied, or assumesany legalliabilityor responsibilityfor the accuracy.
Trang 1.
—
co3
“ —.
- - , ,,-,, :,
., .
., ,.
-— —-. ., .T-——
——, , - < .,,, .
, , .
-.- A -,
.,, - , :
,.
-, , , , , L
”.- ,.,
.- — ~ ., ,,,!,
— - .- . — .— - .- -.
, ,, , .“ .—.—=— —,
- —.
, , -
., -.-—,.-, , -
<., ,.
——.
- -—
-High-Temperature=SttibleDetonators
.- - —— -.
- , ,:’
—— ,- : ,
i f ;W,;
-.
:’ ‘.,!- : -, - .
.
,, “,,, , ,
:_. !
,—
n
Los
Trang 2ASSAffiitivC Action/Eqrsd @fsOtity EsSSPIO)%X
DISCLAIMER This report was preparedas an account of work sponsoredby an agencyof the United Stales (ksvemment Neither the United States Governmentnor any agencythereof, nor asryof their employees,makesJny warranty, expressor implied, or assumesany legalliabilityor responsibilityfor the accuracy.complctcrtcss.
or usefulnessof any information, apparatus, product, or processdiaclo=d, or representsthat its use would not Infringeprivatelyowned rights Reference herein to any specificcornrrrerciafproduct proce= or sertice by trade name, trademark, marrufactuser,or otherwise,does not nec-y constitute orimply its endorsement, recommendation, or favoring by the United States Government or any agency thereof llrc views and opiniona of authors expressed herein do not necessarily state or reflect thoserrf theLIniled
States Governmentor any agencythereof.
Trang 3UC-45 Issued: October 1984
High-Temperature-Stable Detonators
Robert H Dinegar
E– ——
b
—.
-=—.
-.
—s= - G
—
—
-
. —.
“ ,.
— ,-*A 2: - — : !
.
.
—-.
Trang 4by
DETONATORS
RobertH Dinegar
ABSTRACT
stable detonators involve using HMX, KP, HNS, and PYX
explosives The test.devicesemployboth
hot-wireflying-plate and slappermodes of operation Hot-wiredetonators
using HMX as the donor explosive,with HMX, KP, and HNS as
the intermediateacceptormaterialand HNS as the booster
225°C Very limitedsuccesswasachieved using PYX
explo-sive in a few experiments The program of investigation
hot-wiredevice functioningin the DDT mode of operation
explosive has been initiated to detonationby low-energyslapper
foils
The developmentof a detonatorthat will withstandelevatedtemperatures
is governedby both the temperatureregimedesiredand whetherthe explosives that are stable at those temperaturescan be initiatedto detonation In addition,it must also be determinedthat practicaland realizableamountsof
Two methodsof explosiveinitiationare consideredin this report,i.e., hot-wire and slapper-foil In the first, a small wire in contactwith an
explo-sive (donor)is ignited,and the gases that are producedrupturea metallic disc The flyingplate formed strikesa second explosive(acceptor)that is initiatedto detonation In the second,the slappersystem,the rapidpassage
Trang 5process drives material coveringthe foil into an explosive,whichis
ini-tiated to detonation A
functioning
The test device is
fractionof 1 J of energy is sufficientfor proper
mode of operation Two parallelNichromeV bridgewires,0.05 mm in diameter
densityof 1.6 g/cm3
/
waster Explosive
Hat”
2
““’S-=-.IVNM—
Steel
Acceptor Explosive
\ ,.,
-.:,
~L:;::[p’o’e
>. Al Disk Becomes
‘Flying Plate”
9EiiRi’rse: ,
Steel J - J’///i
~Ta Firing Unit
because0.2 mm of an overall
6061-T6A1 The flyerdesignis called“Top l.O-mm-thickshim fits snugglydown inside
Trang 6the flyer barrel forming a “Top Hat.” The flyer barrel has a diameterof 2.5 mm and is 7.0 mm in length The acceptorcharge holder has the same dimensions Both parts are made of 303 stainlesssteel and are screwedto-gether The boosterpellet is confinedin a brass hexagonalring glued onto the end of the acceptor charge An aluminum witness block (usually2024 Dural) is glued onto the metal ring that containsthe boostercharge
maxi-mum temperatureat which we have done experimentsis 250°C The majorityof the testing in hot-wireassemblieswas done with HMX explosive KP and HNS were looked at in some detail; the daLa on PYX were sparsebecauseof its relativeinsensitivity.The specificsurface(S.)of the explosivesdiffered HMX used in the donor and the acceptorwas 8500 and 3450 cm2/g,respectively
KP donorpowderwas 7600 cm2/gand the acceptorexplosive2350 cm2/g HNS was
balls to an S of about 30 000 cm2/g for this testing
The donor explosiveswere all fired at 10 A or more This is far above
currentvalue is only about twice the thresholdvalue
Figure2 shows the slapperdetonator Electricalenergyfrom an external source is depositedextremely rapidly in a metallic foil of the order of 0.01 mm thick There is a rapid productionof vaporizedmetal and plasma
than 0.1 mm thick placed againstthe bridge down a barrel a few tenths of a millimeterin length The impact of the rapidly moving material upon an attachedhigh-densityexplosivepellet providesenoughenergyto initiatethe explosiveto detonation
~~-potassiumpicrate
~~ 2,6-bis(picrylamino)-3,5-dinitropyridine
Trang 7: ‘.
I
enough to generatea usable pressurethat forms flying
PYX decomposesjust plates from aluminum discs The flying plates have energiesgreat enough to dent both 6061-T6A1
will work, but whether the probabilityof an explosiondevelopinginto a detonationis high enough for practicaluse remainsto be seen Extrapolation
min-utes for all-KPdetonators
donor material,HNS decomposedupon hot-wireheating to form a flyingplate but not with sufficientenergy to reactKNS or KP at 1.0 and 1.2 g/cm3 in the 4
Trang 8acceptorbarrel As an acceptormaterial, initiatedby a flyingplate driven
by anotherexplosive,it performsmuch better
of severalhours into the 200°C region It is certainlyworth seeingat how high a temperatureit will function(TableI)
TABLE I
AT ELEVATEDTEMPERATURES
NUMBER
2
2
2
2
2
1
1
1
6
9
7
EXPLOSIVE
HNs-1
II HNs-1 Km-l
f!
S = 13000 cm2/g HNs-1
It HI/s-l
t! s = 3450 HNs-1
HNs-1
CYLINDRICAL DENT VOLUME (cm3) 0.69a o.39a o.47a o.3oto
0.32t0.01 0.29
o.44a o.49a 0.29t0.02 0.32t0.04 0.32t0.04
TEMPERATURE (’JC) + 74 +100 +150 +200
+200 +225
+100” +150 +150 +200” +225
a6061-T6Alwitnessblock;all others2024 Dural
Trang 9HMX donorswill initiateHMX, KP, andHNS-1 acceptorexplosivesto deto-nation by driving flying plates withoutmuch difficultyup to +150°C Fol-lowingare detailsof the resultsof all-HMXdevicesat highertemperatures
failedto ignitedue to an open bridgewire One donor did not shear the flyer plate, and one threw the flyer only halfwaydown the barrel Althoughsome engineeringproblems still seem
Its auto-ignitiontime appears
to exist, hot-wiredetonatorsusing HMX as appearusableat 200°C
to be less than 30-45 minutes The solid
plate that was recoveredat the end of the flyerbarrel The gases evidently causedbridgewiresto come loose from their welds in severalcases The HMX
of low density (-1.2 g/cm3) in the acceptorbarrelsublimedcompletelyin two
dent in the witnessblock
explodedspon-taneouslyat differenttimes of heating (less than 30 minutes) No evidence
of initiationto detonationwas observed
W Hemsingand I M Garcia (M-7)have foundthat PYX can be detonatedin slapper-typedetonatorsat fairly low energylevels(~0.3-Jstoredenergy)at ambient temperature At high temperatures,the required energy should be significantlylower Therefore,in principle,a detonatorcapableof with-standing+300°C is at hand We are endeavoringto make a
pro-vidingthe cryogenicprotec~ionneededby present-dayfiringsystemsin under-groundwork
REFERENCE
Ex-plosives,” Los Alamos National Laboratoryreport LA-5829-MS(January 1975)
6
Trang 10NTSS
Page Range Prim Code
-.—
.—
- , , - - ~, a
- - ,.
.- — - ,
“.
.;.
- , ,, - ,
- ,
.-Printed i!l the United States of Americ.
Available from National Technical Information Service
US Dcpaflmcnt of Commerce S285 Port Royal Road Springfield,VA 22161 MicroIlchc (AOI)
N’IIS Page Range Prim Code
NTIS Page Range Price Code
NTIS PWC Range Price Code 001.025 A02
026.050 A03
0s1.075 A04
076.100 A05
101- [25 A06
126.150 A07
151.17s A08 176.200 AW 201-22s A1O 226-250 AI1 2S1.275 A12 276.300 A13
301-32S A14 326.3S0 A15 351-375 A16
376430 A17 401-425 A18
426430 A19
45[47s A20 476.500 A21 501.525 A22 526.550 A23 551.575 A24 576.600 A25
1501.up” A99
“Contact NT2S for a price quote,
Trang 11Lmlw-nnlos