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Approved for public release; distribution isunlimited. Document partially illegible.
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USAMC ltr, 2 Jul 1973
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M C P A M w i t r
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\JS
fQ E CK K l sA L
R E P O R T
S E C T I O N
1
/
V L
POSTGR A D U A TE
S C H O O L
MONTERtV,CALIFORNIA
9394Q
M C
P M P H L E T
M C P706-244
THISIS AREPRINTWITHOUTCHANGEOFORDP20-244
R E S E A R C HA N D
D E V E L O P M E N T
O M A T E R I E L
ENGINEERINGDESIGNHANDBOOK
A M M U N I T I O N
S E R I E S
S E C T I O N 1 ,
A R T I L L E R Y
A M M U N I T I O N - G E N E R A L
WITH
TABLEOFCONTENTS,GLOSSARYANDINDEX
FORSERIES
B E S T
A V A I L A B L E
C O P Y
HEADQUARTERS,U .S.ARMYMATERIELCOMMAND EPTEMBER963
8/10/2019 Artillery Ammo General
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i
HEADQUARTERS
UNITED
STATES
ARMY
MATERIEL
COMMAND
WASHINGTON
25,
.C.
30
September
1963
AMCP
706-244,
ection
1,
ArtilleryAmmunition--General,
formingpartof
the
Ammunition
Series
oftheArmyMateriel
Command
Engineering
DesignHandbook,
spublished
for
the
information
and
guid-
anceof
allconcerned.
( A M C R D )
FOR
THE
COMMANDER:
SELWYN
D.SMITH JR.
MajorGeneral USA
Chiefof
Staff
OFFICIAL:
DAVIDSON
Colonel,S
Chief,
Administrative
Office
DISTRIBUTION:
Special
(
8/10/2019 Artillery Ammo General
5/88
F O R E W O R D
T heA R T I L L E R YA M M U N I T I O NSERIES
sbeing
ssued
s
an
interim
publicationofth e
O rdna nceEngi neeri ngD es ign
H an d bo o k,
a
comprehensive
sequenceof
publications
planned
to
treatth eentire
ield
ofO r d n a n c e
design.hen
th eH a ndbook
w as
begun
it
w as
found
tobe
impractical
o
ntegrate
nto
t
he
series
relating
to
Arti l lery
Am m u n i-
tion
alr ead y
in
preparation
under
th e
direction
ofPicatinnyArsenal.
A l-
thoughhey
were
imilar,
he
bjectivesofh e
w o
rojectswer e
ot
identical.h esubjectbrea kdownadoptedfo r
th e
H an d bo o k
would
have
necessitated
edistribution
f
heaterial
f
h iseriesh r o u g h o u t
severalofth eplanned
volumes
of
th e
H an d b oo k ,
with
onsequent
elay
in
publication
of
much
ofth ematerial .t
w as
therefore
decidedto
issue
this
m at er ia l
intactasan
interim
publication
to
makeit
ava i lableasearly
as
ossible.
he
m at er ia lppearing
inthisserieswil lbegradual l ysu -
perseded
s
ertinent
olumesfherdnance
ngineering
esign
H an d bo o k
become
available.
Mat er ia lfo rthisseries
w as
prepared
y
he
echnical
riting
Service
of
th e
M c G r a w - H i ll
B o o k
Company,
under
Contract
D AI-2 8 -01 7 -
5 0 1 - O R D - (P )- 91 2 .
echnical
supervision
and
much
f
th e
basic
nfor-
mationer e
urnished
y
icatinny
Arsenal.
ngineers
romther
O r d n an c eDes i gn
Centers
alsosuppliedmuchinformation,andaidedin
th e
review.
nfact ,
so
ma ny
persons
havegivent imeandenergy
to
this
projectthatithasbeendifficult
to
compile ompleteistofcknowl-
edgements.
T he
fol lowing
wer eresponsiblefo rth econceptionand directionof
th eroject.
A R T I L L E R Y
A M M U N I T I O N
S E C T I O N ,
ARTILLERY
A M -
M U N I T I O N A N D
ACKING
D E V E L O P M E N TL A B O R A -
T O R Y ,
S A M U E L
F E L T M A N
A M M U N I T I O N
L A B O R A -
TORIES,PICATINNYARSENAL
A l fredF.Teitscheid
hief,
Arti l lery
Am m u n it io nB r a n c h
W i ld e r
R .
Carson
hief,
Arti l lery
Am m u n it io n
B r a n c h
R oyH .W o o d
hief,
Arti l lery
Am m u n it io n
Laboratory
A
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M A J O R
C O N T R I B U T O R S
GeorgeDemitrack
Lars
Enequist
H e n r y
P.Hitchcock
Dr.
RobertH .
K e n t
Charles
Lenchitz
Prof.
A r t h u r
F.
M a c C o n o c h i e
A r n o l dO .
Pallingston
Richard
E .
T o d d
Col.
H e r m a n
U .
W a g ne r ,
U SA
(Retired)
Picatinny
Arsenal
Ballistics
Research
Laboratory
Ballistics
Research
Laboratory
BallisticsResearch
Laboratory
Picatinny
Arsenal
Prof.f
Mechanical
Engineering,
Uni-
versity
of
Virginia
Picatinny
Arsenal
Interior
Ballistics,
P
rope H a n t s
Lethality
Criteria
Exterior
Ballistics
Exterior
Ballistics
Thermodynamics
of
Explosive
Materials
M a n u f a c t u r i n g
M e t h o d s
Physical
Testing
f
Explosive
Materials
Picatinny
Arsenal
Qual i ty
Control
GeneralContributor
andConsultant
M u r r a y
Weinstein
Picatinny
Arsenal
PhysicalTesting
f
Explosive
Materials
Dr.LewisZernow
Col.H e r m a n
H .
Zornig,U SA
(Retired)
BallisticsResearch
S h a p e d
Charge
Laboratory
heory,Blast
O r d n a nc e
Specialist
andCon sul tan t
G E N E R A LA S S I S T A N C E
K e n ne th
H .
A bbott
Theodor
A d v o k a t
N o r m a nE .Beach
D o n a l dR .Beeman
W a t er t ow n
Arsenal
KineticE n e r g y
A m m u n i t i o n
PicatinnyArsenal
PicatinnyArsenal
Picatinny
Arsenal
SpecialPurpose
Shell
ChemicalTesting
f
Explosive
Materials
H e a d
A m m u n i t i o n
DesignB r a n c h
11
8/10/2019 Artillery Ammo General
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G E N E R A L
A S S I S T A N C E
(cont)
W i ll a r d
R .
Benson
lcatlnnyArsenal
WarrenBllttersdorf
rankford
Arsenal
Joseph
I.
B l u h m
at er t o wnArsenal
WilliamByrne
rankfordArsenal
John
E .
Capell
lcatinny
Arsenal
Herbert
N .
C ohen
icatinny
Arsenal
C o r w i nS.
Davis
lcatinny
Arsenal
A b r a h a m
L.
D o r f
m a n
icatinny
Arsenal
CyrusG .
D u n k l e
icatinnyArsenal
LeonardH .EriksenicatinnyArsenal
H a r o ld
N .
E u k e r
PatrickFalivene
A r t h u rP.Field
A l
Fox
Leo
J .Frey,
Jr.
RobertFrye
A n d r e w
J.
G a l k o
ThomasH a l l
Dr.
DavidH a r t
FloydHill
SidneyJacobson
Frankford
Arsenal
PicatinnyArsenal
Picatinny
Arsenal
Frankford
Arsenal
Picatinny
Arsenal
Picatinny
Arsenal
Picatinny
Arsenal
Picatinny
Arsenal
PicatinnyArsenal
Ballistics
Research
Laboratory
PicatinnyArsenal
Lethality
Theory
Cartridge
Case
Design,
Manufac-
tur i ng
M e t h o d s
R o t a t i n g
B a n d s
Cartridge
Case
Ammunition
Design
Standards
Pyrotechnics
C hi efPropellant
Section
Pyrotechnics
Sh apedCharge
Ammunition
ExplosivesChem-
istry
Laboratory
A PShell
PropellantIgnition
Inspection
M a n u f a c t u r i n g
M e t h o d s
Special
Purpose
Shell
H e a d
Chemical
Branch
G B
Shell
H E P
Shell
H e a d
Pyrotechnics
Laboratory
T a n kVulnerability
KineticEnergy
Ammunition
111
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G E N E R A L
A S S I S T A N C E
cont)
WilliamJosephs
K u r t
K u p fe r m a n
Picatinny
Arsenal
Picatinny
Arsenal
RobertG .
Leonardi PicatinnyArsenal
WilliamL.
Lukens
Propellants
Sh aped
Charge
A m m u n i t i o n
Primer
Ignition
Formerly
incharge
of
Ammunition
De-
sign
Branch,
PicatinnyArsenal
Ulysses
S.
M a c D o n a l d
Picatinny
Arsenal Inspection
James
R -M c K a y
icatinnyArsenal
Special
Purpose
Shell
H a r o ld
M a r k u s
rankford
Arsenal
A P
Shell
Ant hony
Muzicka
atervlietArsenal
Jacob
H .
Niper
K a r l
G .
O t t os o n
PicatinnyArsenal
Picatinny
Arsenal
LawrenceW .Pell Picatinny
Arsenal
BallardE .
Quass
icatinnyArsenal
Lt.Richard
Rhiel
Dr.
William
H .
R i n k e n b a c h
D
P
SAberdeen
Proving
G r o u n d s
GilbertE .
Rogers PicatinnyArsenal
M a x
Rosenberg
WilliamM .
R o w e
SamuelSage
Picatinny
Arsenal
PicatinnyArsenal
Picatinny
Arsenal
M a r v i nB .Schaffer Picatinny
Arsenal
A r t h u r
B .Schilling Picatinny
Arsenal
Rifling
and
G u n
Chambers
Inspection
Asst.
Chief,
Chem-
ical
Test
Section
H i g h
Explosives
Special
Purpose
Shell
Plate
Penetration
Monograms
Formerly
ncharge
of
Picatinny
Arsenal
General
Artillery
Ammunition
Design
Ammunition
Design
H E PShell
Chief,
H i g h
Ex-
plosives
Section
Canister
Shell
ForeignAmmunition
IV
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G E N E R A LA S S I S T A N C Econt)
RobertM .
Schwartz
Picatinny
Arsenal
William
F.Sh irkicatinny
Arsenal
M o r g a n
Smith
allisticsResearch
Laboratory
JosephV.
Sperazza
BallisticsResearch
Laboratory
JosephSterne
BallisticsResearch
Laboratory
Theodore
W .
Stevens
icatinnyArsenal
N o a h
A .
Tolch
allisticsResearch
Laboratory
Paul
B .
T w e e d
icatinny
Arsenal
Robert
J .
Vogel
icatinny
Arsenal
LeoVolkheimericatinnyArsenal
Stanley
W a c h te il
Garry
Weingarten
icatinny
Arsenal
General
Ammunition
Design
Canister
Shell
Aircraft
Vulnera-
bility
BlastTheory
Lethality,
Frag-
mentation
H i g hExplosives
Lethality,Frag-
mentation
H i g hExplosives
Assistant,
Research
and
Development
Section
W P
Shell
Chief,
Physical
TestSection
H e a d ,
Chemical
ResearchSection
Pyrotechnics
Laboratory
E d w a r d
Wurzell
PicatinnyArsenal InteriorBallistics
8/10/2019 Artillery Ammo General
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P R E F A C E
T h is
eries
s
ompilation
ofvailable
ata
n
h e
esign
f
arti l lery
ammunition.tisintended
to
introduce
th e
graduate
engineer
toth ea rtofammunitiondesignandtoserveas
areadyreference
fo r
th e
practicingarti l leryammunitiondesigner.
Inform ati on
ontainednheseublicationsas
ee n
btained
from developmentreportsandd r awin g s
of
ammunition
items,fromproof
firing
records,
an d
from
research
reports
by
Uni ted
States
nd
B r i t i s h
government
agencies.
he
nformation
obtained
fromthese
sources
w as
corroborated
and
supplemented
y
mea ns
of
direct
interviews
and
cor-
respondencewithpersonnelofU .S.overnmentnd
rivate
esearch
and
designagencies.
Th is
series
consistsofsixsections.
ection
1
is
anintroduction
to
th e
general
subjectof
ammunition
an d
it s
design.
t
is
prima ri ly intended
to
familiarizenewcomers
to
th e
fieldw i th
th e
nomenclature
and
classifi-
cation
of
ammunition
items.Forconveniencein publication,th efeatures
applyingto th eentireseries,
such
as
Table
f
Contents,
Glossarynd
Index,
have
been
bound
w i th
Section
1 .
Section
2
is
concerned
w i th
terminal
ballistics,orth eproduction
ofeffect
by
th evarioustypes
of
ammunition.
ection
3
dealswith
h e
control
offlight,
and
exterior
ballistic
esignofot hin-stabilizednd
spin-stabilizedrounds.
Section
4,ondesignorprojection
ofmmunition,ncludes
h e
designofpropel lantsfo rdesired
nteriorballisticcharacteristics ,stress
analysis,
and
th e
designof
cartridgecase,
u n
chamber,and
ifling
nd
rotating
bands.
Section5
describes
th e
inspection
aspects
of
arti l lery
ammunition
design.
t
is
included
to
ac q u ain t
th e
designer
with
imensioning
rac-
t ices
nd
h e
at u r e
of
he
imitations
placedondesignbyth e
require-
ments
of
gaginga ndqualitycon tro l
Section6,on
m anufacturi ng
methods,
a s
ee n
ncluded
o
iv e
th e
neophyte
designer
some
insight
into
th e
overal lproblemof
th e
ma nu-
VI
8/10/2019 Artillery Ammo General
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facture
f
etal
artsfmmunitiontems,incemethods
of
ma nu-
facture
impose
l imitationsupon
th e
design
of
such
items.
M u c h
effortas
ee n
pent
n
ocatingnderifying
h is
ata.
H o w e v e r ,
in
spiteofthis,itisprobable
hat
aluableources
ave
ee n
overlooked
andthat
a
certainpercentage
f
h enformationslready
obsolescent
ecause
f
he
apiddvances
eing
made
n
he
ield.
t
ishopedthatth eusersofth e
Arti l lery
mmunition
eries
wil lnform
th eO f ficeofO rdna nceR esear c h ,
B ox
CM ,D u k e
Station,
D u r h a m ,
N o r t h
Carolina,
of
any
omissions
or
errorsthattheym ay
notice.
Vll
8/10/2019 Artillery Ammo General
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table
o f
contents
Section
age
Paragraphs
F O R E W O R D
iii
P R E F A C E ix
1
R T I L L E R YA M M U N I T I O N
G E N E R A L 1
Types
and
Classification
of
Complete
R o u n d s
1
-1o
1-12
Types
f
Projectiles2
-13to
1-21
Projectile
C om ponents3
-22to1-28
Fuzes,
Boosters,
ndDetonators
...
1-4
-29to
1-37
Explosives
for
A m m uni t i on
6-38
to
1-41
Propelling
Charges
6
-42to1-50
GeneralDesignRequirements
8-51to
1-54
ReferencesandBibliography
8
2
E S I G N
FO R
T E R M I N A L
E F F E C T S
2-1
Introduct i on
1-1
o
2-16
BlastEffect 7-17to2-49
viu
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Section a ge Paragraphs
2ESIGN
FO RT E R M I N A L
E F F E C T S(cont)
Re fe re nce sandBibl iography
-
20
Characteristics
of
High
Explosives
.
-2 2
2-50
to
2-70
Shaped
Charge
Ammunition
-30
2-71
to
2-153
Fragmentat ion
-93
2-154
to2-207
R e f e r e n c e s
and
Bibl iography
-
1
1
3
K inetic
Energy
Ammunition
fo r
th e
De f e a tofA r m o r-1 17
2-208
to 2- 265
Re fe re nce s
and
Bibl iography-14 8
Canister
Ammunition
-
1
5
0
2 - 2 6 6
to
2-278
Re fe re nce s
and
Bibl iography
-1 55
H igh -E x plosive
Plastic
( H E P )
Shell.
- 1 5 6 2-279to2-291
R e f e r e n c e s
an dBibl iography
-1
59
Special
Purpose
Shell
-1
6 0
2-292
to
2-371
Re fe re nce san dBibl iography-199
3
ESIGN
FO R
C O N T R O L
O F
FLIGHT
CHARACTERISTICS
-1
D e s ign
for
Precision-1
-1to3-22
R e f e r e n c e s
and
Bibl iography
33
D e si gn
fo r
Maximum
Range
or
Minimum
Tim e
ofFlight
-38 3-23to
3-48
R e f e r e n c e san dBibl iography-77
Projectile
Geometry
-81
3-49
to
3-64
4
ESIGNFO R
P R O T E C T I O N
-
1
Propellants
nd
InteriorBallistics
4 -1
-1
to
4-75
Cartridge
Case
an d
Gu nChamber
D e s i g n -11 7
4-76
to4 - 1 1 6
R e f e r e n c e s
an dBibl iography-1 37
ix
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Section
age
Paragraphs
4
ESIGNFO R
PROJECTION
cont)
Rotating
Bandand
Rifling
Design4-149-117
to
4-154
ReferencesandBibliography
1
76
StressnShell
1
77
4-155to
4-177
References
and
Bibliography
190
5
NSPECTION
ASPECTS
OF
ARTIL-
LERY
AMMUNITION
DESIGN
1
QualityAssuranceAspectsof
Ammunition
Design
1
-1
to5-21
References
andBibliography12
Effect
of
Dimensioning
and
Tol-
erancing
onInspection
13
5-22
o5-28
6
ANUFACTUREOFMETALLIC
COMPONENTSOFARTILLERY
AMMUNITION1
Introduction 1-1o
6-10
Forging
of
HE
Shell
4-11
to
6-33
Machiningof
HE
Shell
14
-34to
6-56
ColdExtrusionofH E
Shell
21
-57to6-68
Compromise
Method
ofShell
Forming 25 6-69to6-70
Manufacture
of
High-Explosive
Plastic
Shell 26 6-71
to
6-77
Manufacture
of
Armor-Piercing
Shotand
Caps29 6-78
to6-86
The
Manufacture
of
Hypervelocity
Armor-Piercing
HVAP)
Shot
35
6-87
to
6-91
TheManufactureofTungsten
Carbide
Cores
36 6-92to
6-95
The
Manufacture
ofBrass
Cartridge
Cases
37 6-96
to
6-103
The
Manufacture
of
Drawn-Steel
CartridgeCases4 1
6-104o
6-122
x
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Section age Paragraphs
6A N U F A C T U R EO F
M E T A L L I C
C O M P O N E N T S
O FA R T I L L E R Y
A M M U N I T I O N
cont)
T h e
M a n u f a c t u r eol
Trapezoidal-
W r a pp e dSteel
Cartridge
Cases . 6-46 6-123
to
6-131
T he
M a n u f a c t u r e
l
Perforated
Cartridge
Cases
48
6-132
to
6-133
References
nd
Bibliography
49
G L O S S A R Y -l
I N D E X 1
xx
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G L O S S A R Y
ABSOLUTE
EVIATION:
Theshortest
distance
between
heenterf
he
arget
ndhe
point where a projectile hits or
bursts.
ABSOLUTE
RROR:
hortestdistance
between
the
enterf
mpact
r
heenter
ofburst
of
roup
f
hots
nd
he
ointofmpact
or
urst
f
ingle
hotithinheroup.
ACCURACY
IFE:
he
stimated
verage
number
founds
hat
articulareapon
can
ireeforets
ube
ecomes
oworn
that
its
accuracy
tolerance is
exceeded.
ACCURACY
F
IRE:
he
easurement
f
the
recisionfire
xpressed
s
hedis-
tancef
he
enterfmpactromhe
center
ofthetarget.
ADIABATICLAMEEMPERATURE:he
temperature
a
combustiblesystem
would
at-
tain
f
ll
he
nergy
f
ombustion
ent
into
he
ormation
fasithout
nergy
losstothe
surroundings.
AMATOL:ig h
xplosive
made
of
a
mixture
of
ammonium
itrate
nd
rinitrotoluene;
sometimes
sed
s
urstingharge
n
high-explosiveprojectiles.
AMMONAL:
igh-explosive
ubstance
made
of
aixture
f
mmonium
itrate,
rinitro-
toluene,
nd
laked
r
owdered
luminum.
Ammonal
sometimes
seds
ursting
charge
n
igh-explosive
rojectiles,
nd
producesbrightflashesonexplosion.
AMMUNITION
ATA
CARD:
Identification
card
preparedorach
ndividual
lot
of
ammuni-
tion
manufactured,
ivingheypeand
com-
position
fhemmunition,
nd
dentifying
its components by lot
number andmanu-
facturer.
he n
ecessary,
t
ay
lso
include
nstructions
or
handling
theammu-
nition.
AMMUNITIONDENTIFICATIONODE:ode
symbolforxample,
5HBA)
ssigned
o
each
mmunition
tem
or
dentificationand
to
acilitatehe
upply
fmmunition
o
the
ield.
heirstwoharacters
refero
theertinent
rdnance
atalog,
nd
he
re-
maining
hree
haracters
ohe
eapon
group,
ype
nd
odel,
nd
ackaging.
n
small
rms
mmunition
he
rade
s
n-
dicated.
AMMUNITIONOT
UMBER:
ode
umber
that
dentifies
articular
uantity
f
m-
munitionrom
ne
manufacturer.
Thenum-
bersssignedoeach
otf
mmunition
when
its
manufactured.
ANGLE
FEPARTURE:ngleetweenhe
line
fightndhe
xis
fhe
oreof
a
gun
at
he
nstant
he
rojectile
eaves
he
muzzle.
ngle
f
eparture
s
he
um
f
the
ngles
f
ite,
levation,nd
ertical
jump.
ANGLE
F
ALL:
ngle
etween
heori-
zontalnd
he
angento
he
rajectory
t
thepointatwhichaprojectile
falls.
ANGLEF
MPACT:cute
ngle
etween
the
tangento
he
rajectory
theoint
f
impactfrojectilendtheplane
tangent
toheurface
fheround
thepointof
impact;
ngle
t
hich
projectile
trikes
thegroundor
a
target.
ANGLE
F
NCIDENCE:
nglet
hich
projectile
trikes
urface;
cute
ngle
between
he
angent
o
he
ine
of
mpact
of
a
rojectile
nd
heerpendicularo
he
surfacef
he
ground
at
thepointof
mpact.
It
s
heomplementoftheangleofmpact.
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A R E A
A R G E T :Targetfor
gunfire
orb omb in g
covering
onsiderable
space,
uch
as
am-
munitions
actory,irport,rreightyard.
A narea
arget
differs
rom
oint
target,
which
is a
particular
bject
rtructure.
A R M I N G :sppliedo
uzes,h eh an gin g
fromsafecondition
toastate
freadiness
for
nitiation.
enerally
uze
is
caused
to
arm
ycceleration,
otation,
lock
mech-
anism,rir
ravel,
r
by
combinations
of
these.
A R M O R :rotectiveovering,
especially
metal
platessedn
ships,
anks,
motor
vehicles,
etc.
A R M O R - P I E R C I N G :ermappliedo
bullets
and
rojectiles
esigned
o
ierce
rmor
plate.
A R M O R - P I E R C I N G
A P P E D :
erm
pplied
to
armor-piercing
rojectiles
hich
a ve
steelapnrontfheprojectile
poin t ,
o
assistnefeatingace-hardenedrmor
plate.
A U T O M A T I C(Self-Acting):
M o v i n g
or
acting
by
itself.
Afterth e
first
ound
is
fired,n
auto-
matic
e a p o n
ires,
xtracts,
jects,
nd
reloads
w i t h o u tapplicationofpowerfroma n
outsideource,epeating
he
ycles
long
as
the
firing
mechanism
sheld
in
the
proper
position.
utomatic
ction
nvol^s
epeat-
in g
he
ycle
f
peration,
s
distinguished
from
emi-automatic,w h i c hisrestricted
to
on e
complete
cycle
a t
a
time.
A U T O M A T I C
EEDE C H A N I S M :
Mechanism
inan
utomatic
u n
hat
u tsresh
hells
into th e chamber
in
positionor
firing.
B
B A C K - B L A S T :
earwardlastf
gases
rom
the
reech
f
ecoilless
eaponsand
rock-
ets
pon
h eurn in g
f
h e
ropellant
charge.
t
s
ometimes
eferred
o
s
breech-blast.
B A L L I S T I C
A P:
a p
or
projectile,designed
toimproveitsballistic
efficiency.
B A L L I S T I CO E F F I C I E N T :easuref
h e
abilityf
issile
overcomeire-
sistance.
B A L L I S T I C
O N D I T I O N S :
onditionshich
affect
h e
otionfprojectile
nth ebore
andh roughheatmosphere,ncluding
muz-
zle
elocity,eightfrojectile,izend
shapef
rojectile,otation
f
h e
arth,
densityf
h e
ir,lasticity
fheira nd
th ew i nd.
B A L L I S T I C
U R V E :
ctual
a th
r
trajectory
of
a
bullet
or
hell.
B A L L I S T I CE N S I T Y :
o m p u t e d
constantir
density
h a t
w oul d
h a v e
thesametotaleffect
on
rojectileurin g
ts
light
s
he
varyingdensitiesactuallyencountered.
B A L L I S T I C
F F I C I E N C Y :
bilityfro-
jectileo
vercome
he
esistance
f
h e
air.
allisticfficiency
epends
hieflyn
th eeight,
iameter,
ndhape
f
h e
projectile.
B A L L I S T I C
I M I T :
elocity
t
h ich
given
type
f
rojectileill
erforate
iven
thicknessnd
ypefrmorlatet
specified
obliquity.
B A L L I S T I C
O R T A R :
nstrument
sedode-
termine
heelativeenergyobtainable
from
explosivematerials.
B A L L I S T I C S :
T h e
projectiles.
science
of the
motion
of
B A L L I S T I C
E M P E R A T U R E :
Acomputedcon-
stantemperature
ha t
ouldhaveth esame
total
ffectnprojectile
raveling
rom
theu n
o
h e
arget
s
h e
arying
em-
peratures
actuallyencountered.
B A L L I S T I CA V E :udib le
isturbancer
wave
ausedy
h e
ompression
f
ir
a h e a d
ofaprojectile
in
flight.
B A L L I S T I C
I N D :
ssumed
constant
wind
that
w o u l d
aveheameotalffect
n
apro-
jectileravelingrom
he
u n
o
h etarget
as
th e
varying
winds
ctually
ncountered.
B A L L I S T I T E :mokeless
owder
seds
propellingcharge
nsmall-armsandmortar
ammunition.
B A L L O T I N G :The
boundingfromside
to
side
of
a
projectile
inth e
bore
fagun.
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B A S EJ E C T I O N
S H E L L :
T y p e
of
special
pur-
pose
hell
w h i c h
unctions
y
expelling
ts
filleru t
f
he
base
of
th e
shell.
Expulsion
issuallychievedymallcharge
f
propellant,called
a n
expelling
charge.
B A S E
I N E :
Line
of
k n o wn
length
and
direction
between
w o
oints
hose
ocations
re
known;used
in
firecontrol.
B A S E
P L U G :
Seal
in
base
ofprojectile.
B A S E
F
R A J E C T O R Y :
traightorizontal
linerom
h e
enter
f
h e
uzzle
f
w e a p o n
to
th e
point
inth e
d o w n w a r dcurveof
th ea th
f
a
projectile
t h a tis
levelwithth e
muzzle.
B A S E
S P R A Y :
See
S P R A Y . )
B I O L O G I C A L
A G E N T :
iruses,ny
fcertain
classifications
f
icro-organisms
nd
toxic
ubstances,erived
rom
iving
or-
ganisms
sedo
produce
eath
r
disease
in
m a n ,animals,
nd
growing
plants.
B I O L O G I C A L
A R F A R E :
actics
nd
ech-
niques
f
on ductin g
arfarey
se
f
biologicalagents.
B L A C K
O W D E R :
ensitive,easily
ignitible
explosive
ixture,hi chroduces
ense
smoke;
ew
emaining
ilitary
uses,
uch
as
gniters,
xpelling
nd
lank-fire
charges.
lack
p o w d e rwasused
as
pro-
pellant
efore
h e
dventfo-called
smokeless
p o w d e r .
B L A N K
A M M U N I T I O N :
m m uni t i onontaining
poweru toprojectile.lank
ammunition
is
sed
n
raining,
n
ignaling,nd
n
firing
salutes.
B L A S T :
u d d enir
ressurereated
y
h e
dischargefu nrh explosion
f
charge.
B L A S T I N G
A P:Small
cylindrical
casewitha
thin
alln
h ich
s
nclosedaensitive
explosive,
uch
sercury
fulminate,used
as
detonator
o
et
ff
n oth er
xplosive
charge.
h e
explosive
nth e
blasting
ca p
is
fired
ither
y
aurni ng
use
r
y
elec-
tricity.
Also
calleda
detonator.
B L A S T
C U B E :
ngle
ron
rame
overed
with
alumin um
heets;
used
for
testingeffective-
ness
of
blast.
B L A S TU B E :evice
sed
orh e
t u d y
f
shockaves,nd
or
alibration
f
ir-
blast
gages.
B L A S T I N G
A C H I N E :
mall
and-powered
generatoror
lectrically
iring
ne
r
more
etonatorsr
quibs
o
xploder
ignite munitions or series ofmunitions.
B L O W B A C K :scape,oheear
nd
nder
pressure,f
gases
ormed
duri ng
the
firing
of
u n.
l o w b a c k
a y
e
ausedy
defectivereech
echanism,
u p t u r e d
cartridge,or
a
faulty
primer.
B O A T - T A I L :
ear
nd
f
projectile
ha t
s
tapered
orcone-shaped,
nd
notcylindrical,
asn
rojectile
avi ngquare
ase.
B O O S T E R :High-explosiveelement,ufficiently
sensitive
o
be
ctuated
y
mall
explosive
elements
n
a
uze,nd
powerful
nough
to
causeetonationf
he
a in
xplosive
filling.
B O R E :
he
ylindrical,
ndsuallyifled,
portion
f
h eu n
ub e,
r
arrel
interior,
extending
rom
h e
forcing
cone
toth e
muz-
zle.
ore
is
used
both
for
the
inside
surface
of
he
arrel
r
u be
f
u n,
it h
its
rifling,ndorhe
ylindricalpace
en-
closedby
thatportion
of
th e
tub e.
B O R E
M P R E S S I O N :mpressionf
th e
bore
of
a
u nu b e ,
m a d ew i tha
plastic
ubstance
n
ordero
etermine
h e
ondition
fh e
rifling.
B O R E S A F E
U Z E :
ype
f
uze
avi ng
a n
in-
terruptor
n
he
xplosive
rainh a t
pre-
vents
unctioning
ntil
after
the
projectile
has
cleared
the
muzzle
of
a
w e a p o n .
B O U R R E L E T :inely
achined
bandor
ringof
metal
ustehindh e
give
fa
projectile,
designed
o
upport
he
rontportionof
th e
projectile
yiding
he
ands
as
he
pro-
jectileravelshroughheore
f
u n.
B O W
W A V E :
(See
B A L L I S T I CW A V E . )
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BREECH:heearartfheoref
a
gun,
especially
hepening
that
permitsthe
pro-
jectile
to
be
inserted
at
therearof
thebore.
BREECH-BLAST:
SeeBACK-BLAST.)
BREECHBLOCK:
ovable
teellockhat
closes
he
ear
art
f
he
arrel
n
firearm.
CANISTER:
1)
Metalcylindercontainingmetal
fragments
hich
re
cattered
hen
he
cylinder
breaks.
2)
Cylinder
containingma-
terials
orpecial
erminal
ffects,
uch
as
smoke,
propaganda
leaflets,
haff,
tc.
CANNISTER
MMUNITION:hellontaining
preformed
metal
fragments
hich
re
is-
persed
y
he
entrifugal
orce
aused
by
theshell'srotation.
BRIDGEAVES:achavesausedyhe
interaction
f
wo
hock
aves
oform
third
hat
ridges
heolumebetweenhe
original
two.
BRISANCE:hattering
ower
figh
x-
plosives.
BURNING
of
ropellant):
Se e
LINEAR
BURN-
IN G
RATE.)
BURST:xplosion
faprojectilen
the
air,
or
whenitstrikesthegroundor
target.
BURSTER:
xplosive
harge
sed
o
reak
open
nd
pread
he
ontents
f
hemical
projectiles,
bombs,
or
mines.
BURSTERUBE:
ubehatoldshe
urster
in
a
chemical
projectile.
BURSTING
CHARGE:
Quantity
of
explosive
which
breaks
to
produce
or chemical
CHARGE.)
the
asing
f
rojectile
demolition,
ragmentation,
action.
(See
EXPLOSIVE
CANNELURE:
1) ing-likeroovenhe
jacket
f
bullet
which
provides
a
meansof
securely
rimpingheartridge
case
tothe
bullet;
nalogous
o
he
rimping
rooven
artillery
mmunition.2)
ing-like
roove
for
ockinghe
acket
fanarmor-piercing
bullet
oheore.
3)
ing-like
roove
n
the
otating
and
ofaprojectile,ntendedto
lessenhe
esistanceffered
o
heun
riflings.
4)
roove
round
the
ase
f
he
cartridge
ase,
here
he
xtractor
akes
hold.
CANNON:1)ixedr
mobile
eapon,
arger
than
mall
arms,hat
jects
ts
rojectile
byhection
f
n
explosive.
annon
nc-
clude
uns,
owitzers,
nd
reech-loading
mortars.2)
hat
ortionf
uch
a
weapon
requiredo
fire
projectilethats,ube,
breech
mechanism,
ndfiringmechanism),
as
ontrasted
o
that
portion
whichsupports
the
eapon
nd
hich
is
called
the
carriage
ormount.
CANT:
object;
gun.
leaning
or
tilt,
one
ide,
fan y
militarily,
he
idewiseiltingf
CALIBER:
1)
Diameter
of
the
bore
of
a
gun.
n
rifled
gun
bores
healiber
s
btainedby
measuring
between
opposite
lands.
A
caliber
.4 5
evolver
has
barrelwitha
land
diam-
eter
5/100
f
n
nch.
2)
iameter
f
projectile.
3)
nit
f
measureusedto
ex-
pressheengthfheore
f
weapon.
The
umberf
alibers
s
eterminedby
dividing
thelength
of
the
bore
of
the
weapon,
from
hereech
ace
f
he
ubeo
he
muzzle,
y
the
iameter
f
tsore.A
gun
tube
hoseore
s4 0
feet(480
nches)
ong
and2
nches
ndiameters
aid
obe4 0
caliberslong.
CAP:
1)
osepiecen
rojectile.
2)
See
BLASTING
CAP.)
CARTRIDGE ound
of
ammunition
wherein
the
propellant
nd
rimerreontainedna
casing
nd
n
which
he
propellant,
primer,
and
rojectile
re
ssembled,
tored,
shipped, and
issued asa
ompleteunit.
CARTRIDGE
AG:
lothagoldinghe
ro-
pelling
charge
forsome
typesof
annon.
CARTRIDGEASE:ontainer
hatolds
he
primer
ndropellant,ndo
hichhe
projectilemay
beaffixed.
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CONFINEMENT:
Degree
ofphysicalrestriction
to
assagefetonation
av e
hrough
x-
plosivematerial.
COOK-OFF:
unctioning
fa
chambered
round
of
mmunition,
nitiated
y
he
eatf
he
weapon.
COPPER
RUSHER
AGE:
evice
sed
o
measurepressuredeveloped
in
gunchamber
byeasuring
he
eformation
f
copper
cylinder.
COPPERING:Metal
ouling
eft
nthe
ore
of
a
eapon
yhe
otating
andorthe
jacket
of
a
projectile.
CORDITE:
ouble-base
owder
n
the
orm
of
cords,
composedof
guncotton,
nitroglycerin,
and
ineral
elly,
sed
y
ome
oreign
nations
s
ropellant
n
roundsofammu-
nition.
COUNTERRECOIL:
orwardovementf
gu n
eturning
ofiringposition
after
recoil.
CROSS-WINDORCE
LIFT):
omponent
f
air
esistance
n
direction
erpendicular
to
heotionfheenterf
gravity,
n
theplaneofyaw.
CRYSTAL
ENSITY:
Maximum
de;
sity
attain-
able
for
a
given
substance.
DECELEROTOR:evice
or
lowing
he
rota-
tionf
arachute-containing
rojectile,
e-
fore
ejection
oftheparachute.
DEFLAGRATION:
apideactionexplosion)
with
volution
f
onsiderableheat,accom-
panied
y
ome
isruptive
ffect
ut
ess
violent
than
adetonation.
DEGRESSIVE
GRANULATION:
Propellant
grain
which
urns
ith
ontinually
ecreasing
surfacentil
he
rain
s
ompletely
on-
sumed.
DELAY
UZE:
uze
hat
as
delayelement
incorporatednheuze
rain,
ermitting
the
missile
to penetrate
he
arget
is-
tance
orrespondingto
the
delay.
Such
fuzes
are
sed
o
ermit
penetration
ofthetarget
before detonation, or
for mining effect.
DESIGN
ROCEDURE:
utlinef
teps
tofol-
low
n
designing
an
tem.
DETERRENT:
aterial
diffused
nto
he
ur-
face
f
ropellant
grains
to
control
burning.
DETONATE:
Explodesuddenly andiolently.
DETONATING
G E N T :
xplosivesed
o
set
offnotherexplosive.Fulminate
of
mercury
and
etryl
re
sed
s
etonatinggentsto
set
of fother
less
sensitive
explosives.
DETONATINGHARGE:
Charge
used
toset
off
a
high-explosive
charge.
DETONATING
ORD:
Flexible
fabric
tube
con-
taining
iller
f
igh
xplosive
thats
set
offyblasting
cap
or
by
an
electric
deto-
nator.tas
n
extremely
igh
ate
ofex-
plosion,
nd
s
sed
o
et
ff
ther
igh-
explosiveharges.
he
etonating
ord
currently
n
se
s
nown
ommerciallyas
primacord.
DETONATING
r
'LOSIVE.)
EXPLOSIVE:
(See HIGH
EX-
DETONATION:
xtremelyapid
eaction
with
evolution
f
onsiderable
eat
ccompanied
by
onsiderable
iolently
isruptive
ffect
and
ntense
hock
wave.
See
lso
DEFLA-
GRATION.)
DETONATION
FRONT:
See
WAVE
FRONT.)
DETONATION
ATE:
elocity
t
hichhe
detonation
wave
travels
through
an
explosive
material.
DETONATION WAVE:
(See
SHOCK
WAVE.)
DETONATOR:
ensitive
xplosive
sed
o
et
off
n
xplosive
rain,
as
well
as
he
mech-
anism
an d
container connected
therewith.
DEVLOPEDUZZLE
ELOCITY:
he
ctual
muzzle
velocity
producedbyanygun.
DOUBLE-BASE
POWDER:
SeeDOUBLE-BASE
PROPELLANT.)
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D O U B L E - B A S ER O P E L L A N T :
ropellant
whose
rinciplectivengredients
rei-
trocellulosend
itroglycerin.See
R O -
P E L L A N T . )
D R A G :om ponent
f
ir
esistance
n
h e
direction
pposite
o
h a tfh e
otion
f
th e
centerfgravityf
projectile.
D R I L L
M M U N I T I O N :
m m u n i t i o n
i thout
n
explosiveharge,
used
n
training
a nd
prac-
tice.
D U M M Y
R O J E C T I L E :
hell
h a t
as
oex-
plosiveharge.
D u m m yprojectiles
are
used
forpracticend
trainingpurposes.
E . C.
B L A N KI R E :
See
.
P O W D E R . )
C.
M O K E L E S S
E .
.
M O K E L E S S
O W D E R :
r a n g e
r
in k
explosive
owder,
esembling
oarse
a n d .
It
ssed
s
hargen
mallrms,n
bl ank
artridges.
lso
alled
lank-fire
p o w d e r
orE .C.blankfire.
E C C E N T R I C I T Y :
istance
romenterine
to
center
ofgravityfprojectile.
E L A S T I C
T R E N G T H
R E S S U R E :
h eom-
pu t ednternalgas
ressuren
a
gu n
w h i c h ,
a t
h e
ectionnder
onsideration,
ill
stress
h e
etal
n
ome
ayer
f
h ewall
tangentially,
p
o
h e
inimum
lastic
limit
hich
s
rescribedor
h e
etal
fromw h i c h
th emember
s
m a d e .
E L E C T R I C
R I M E R :
Metallicevice
ontain-
in g
mall
m o u n t
f
a
sensitiveexplosive
or
harge
f
black
p o w d e r
w h i c h
s
actuated
by
nergizingn
electric
ircuit.
t
sused
for
etting
ff
xplosive
rropelling
charges.
E L E C T R I CQ U I B :ommercial
flash-fuze
de-
vice
or
lectricaliring
f
u r n in g
yp e
munitions
u c h
s
moke
ots.
t
onsists
essentially
f
mall
u be
ealed
it h
sulfur,
ontaining
mallcharge
of
p o w d e r
compressedroundine
esistance
ire.
Thererehree
ypes:
pen-end,
lash-
vented,
nd
closed-end.
E Q U A L
E C T I O NH A R G E :ropelling
charge
m a d e
up
of a
u m b e rf
harges
q u a l
n
size.h e
u m b e r
f
ections
sed
eter-
mines
h e
uzzle
velocitynd
ange
f
th e
projectile.
E Q U A T I O N
FT A T E :n
quat i on
elating
th eolume,
emperature,nd
pressuref
system.
E R O S I O N :
eari ng
w a yfbored u e
to
com-
bi ned
ffect
f
as
ashing,couring,
nd
mechanicalbrasion.
u e
o
h eig hem-
peraturesnd
velocities,
ndhemicalc-
tion, th e
ore
iameter
ecomesnlarged.
E X P E L L I N GH A R G E :uantityf
ropellant
used
n
pecial
urposehell
o
eject
he
contents
fth ehell.
E X P L O S I V E :
ubstance
hi ch,
h enubjected
toeat,mpact,
riction,
rtheruitable
initial
mpulse,
ndergoes
n
explosionthat
is
ery
apid
hemical
ransformation,
forming
ther
more
stable
products
entirely
or
argely
aseous,
hose
ombined
ol-
u m e
s
uch
reater
ha nthatf
th e
origi-
na l
ubstance.xplosivesre
lassified
as
high-explosive
r
ow-explosive,ccording
to
he
atefth etransformation.
Sec
H I G H
E X P L O S I V E
ndLO W
E X P L O S I V E . )
E X P L O S I V EH A R G E :
redetermined
quantity
of
xplosive
equiredoroduce
specific
effect.See
U R S T I N GH A R G E ;
XPEL-
LI N G
C H A R G E ;P R O P E L L I N G
C H A R G E . )
E X P L O S I V E
:
m m o n i u m
icrate,
igh-
explosive
harge
h a ts
ot
easilyetffn
transportation,
r
n
andl i ng,
tc.ome-
timest
s
se dsurstinghargen
armor-piercingprojectiles.
E X P L O S I V E
R A I N :
h a tortion
f
fuzeor
fuze
ystem
onsistingf
xplosive
om-
ponents,
u c h
as
primer,
otonutor ,
booster,
etc.,ecessary
oause
unctioning
f
w a r h e a d
or
destructor.
E X T E R I O R
AL L I STI CS:
T h e
r an c h
f
ballis-
tics
hi ch
eals
it h
the
motion
oi
he
pro-
jectileafter
eaving
h e
gun.
F I N :ight
etal
ortion
f
ortarhell,
b o m b ,nd
ome
ockets,
esigned
or
ta-
bilizing
nd
ontrolling
themwhile
n
flight.
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FIN
TABILIZATION:
Method
f
tabilizing
projectilejomb,
r
missileuring,flight
by
the
fitting
of
fins.
FIXED
AMMUNITION:
Ammunition
with
primer
and
ropellent
owder
ontainedncar-
tridge
ase
ermanentlyrimpedrt-
tached
o
projectile,
hat
soaded
nto
a
weapon
as
a
unit.
FIXED ROUND:Round
f
ixed
mmunition.
FLAME
EMPERATURE.See
DIABATIC
FLAME
TEMPERATURE.)
FLASH
EDUCER:Any
material
foruse
with
a
propelling'
harge
oeduce
tsuzzle
flash.
r
'
:/
>
-
-
FLAT
RAJECTORY:
rajectory
ith
ittle
curvature,
roducedy
projectile
ith
highvelocity.
:w-
FLECHETTE:
Stabilized
fragment
pointednoseand
finned
tail;
dart.
having'-a?'
FORCE:
erm,
onvenientininterior
ballis-
tics
heory,
hich
s
efinedas
the
product-
ofhe
umberfmols
f
aserrmof
propellantrid
he
diabatic-constant-vol-
ume
flametemperature.
FORCING
ONE:
apered
eginning
fhe
lands
t
he
rigin
fhe
ifling
f
gun
tube.
heorcing
one
llows
he
otating
bandf
he
rojectile
o
be
gradually
n-
gagedyhe
ifling
hereby
entering
he
projectile
in
the
bore.
FORMOEFFICIENT:actorsed
n
orm
functions
o
escribeheatiofurning
surface
to
fraction
burned.
FORM
UNCTION:
athematical
xpression
relating
urning
ateo
ropellantrain
geometry.
FRAGMENTATION:
hereaking
nd
cat-
tering
n
ll
irections
fheiecesf
projectile,bomb,
or
grenade.
FULMINATE
OF
MERCURY:
S e e
MERCURY
FULMINATE.
FUZE: Device
used
tonitiateaetonation
undertheconditionsdesired.
GILDINGETAL:opper-zinc
lloy
brass)
usedforrotatingbands.
GRANULATION: Sizeand
shape
of
grain
of
propellant.
GRAVIMETRICENSITY:eight
fhe
ro-
pellant
inlb
pern.3)
divided
by
the
volume
occupied
by
he
ropellant
includes
the
air
space in an d
around
propellant
grains).
G-SERIES
AR
ASES:
roup
f
ersistent
blood
nd
erveoisons
hich
re
ighly
toxic
nd
racticallydorless.A,
B,
an d
GD
are
members
of
the
G-series.
GUNCOTTON:
itrocellulose
ontaining
3
percent
ormoreofnitrogen.
"
H
HANGFIRE:
emporary
failure
rdelayn
the
action
f
,primer,gniter,
r
ropelling
charge.
or ewecondst
annote
distinguished
romompleteailure,
r
misfire.
HANGFIRE
EST:
est
o
determine
uniform-
ity
nd
romptness
ffire
f
atype
of
am-
munition.
HC
IXTURE:
olid,
onpersistent
creening
smoke
hat,
when
burning,
produces
agray-
ish
s
whitemokeaving
harp,
crid
odor,hich
stoxicfreleasednsufficient
quantitiesn
nclosedlaces;sedn
bombs,
hell,
renades,
ndmokeots.
The
moke
s
ool
urning
s
ontrasted
with
hite
hosphorous,
nd
ends
o
ling
to
the
earth.
H E A T
F
OMBUSTION:
eat
volved
n
he
completexidation
f
ubstance
ton-
stantressure
nd25C.The
test
s
usually
accomplishedalorimetrically
yurning
a
gram
f
ample
n
combustion
bomb
con-
tainingnec
f
aterunder
a
pressure
of
30
atmospheres
of
pureoxygen.
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IGNITING
IXTURE:
xplosive
mixturesed
as
a
fuze
n
pyrotechnic
signals.
IGNITING
RIMER:
rimer
esigned
o
e
initiated
y
lame
rom
notherrimer.
Sometimessedn
ubcaliber
uns
o
s
topermitdrill
r
ractice
with
theregular
primer.
IGNITION
ARTRIDGE:
gniter
n
artridge
form
hich
ayesed
lonerithad-
ditional
ropellant
ncrementss ro-
pelling
harge
or
ertain
mortar
ammuni-
tion.
ILLUMINATINGHELL:
Projectile
witha
time
fuzehat
ets
ffarachutelaretny
desired
eight;sed
for
lighting
upanarea.
INTERIOR
ALLISTICS:
ubdivision
fballis-
tics
hich
eals
ith
that
art
f
hehe-
nomenaithin
hehamberndoref
weapon
ssociated
ithmpartinginetic
energyomissiles.See
BALLISTICS.)
ISOBARIC
DIABATICLAME
EMPERA-
TURE:
Adiabatic
flame
temperature
attained
in
onstant
ressure
ystem.
See
ADIABATIC
FLAMETEMPERATURE.)
ISOCHORIC
DIABATIC
LAME
EMPERA-
TURE:
Adiabatic
flame
temperature
attained
in
onstant
olume
ystem.
SeeD I-
ABATICFLAMETEMPERATURE.)
IMPACTUZE:
uzeesigned
o
functionon
impact.
INCENDIARY:
1)
hemicalgent
sed
ri-
marily
or
gniting
ombustible
ubstances
with
hich
ts
n
ontactyenerating
sufficient
eat
o
ausegnition.2)
Filling
forncendiaryunitionsuch
s
hells,
bombs,
renades,
nd
lame
hrowers.
3)
Munition
ith
flammableilling
nd
means
ofreleaseand/orgnition.
INCREMENT:
package
ofpropellant,
forming
partofthe
full
propellingcharge,which
may
be
emoved
oreducethevelocityor
range.
(See
MULTISECTION
CHARGE.)
JOLTND
UMBLE
ESTS:
ests
ntended
to
simulate
hehocks
arious
omponents
of
mmunition
re
ubjected
o
n
trans-
portationandhandling.
JUMP:
he
ovement
hich
heube
f
he
gunescribesnderhe
hock
f
iring,
but
eforehe
rojectile
leaves
themuzzle.
Usuallyexpressedasan
angle.
K
KINETICNERGYMMUNITION:
mmuni-
tion
hose
ffectivenesss
ependent
pon
its
high
density
(mass)
an digh
elocity.
INITIAL
IRSPACE:
olumef
unhamber
no t
ccupiedy
ropellant
hen
un
s
loaded
for
firing.
INITIAL VELOCITY:
LOCITY.)
(See MUZZLE VE-
INITIATOR:mall
uantityfery
ensitive
andowerfulxplosivesedotarthe
detonation
fnother
ess
ensitive
x-
plosive.
Mercury
ulminate,
ead
azide,
and
tetryl
re
theprinciplehighexplosivesused
asinitiators.
INSTANTANEOUS
UZE:
ne
hichwillburst
the
rojectile
nhe
utside
f
a
hard
sur-
face
such
s
concrete
mplacement)
be-
fore
enetration
r
icochet.
his
fuze
will
give
ome
ratern
ard
round.
See
SUPERQUICKFUZE.)
LANDS:
aisedortionetween
grooves
boreofa
rifled
gun.
n
the
LATERAL
EVIATION:
orizontal
istance
betweentheointfmpact
rurstnd
thegun-target
line.
LEAD
ZIDE:
ery
ensitiveighxplosive
used
n
mall
uantities
o
nitiate
ther
less
sensitivehighexplosives.
LEAFLET
HELL:
sually
onsistsf
tand-
ard-base
jectionmokehell,
f
an y
cali-
ber,ithmoke
anisters
emoved
nd
propaganda
substituted
therefor.
LIFTING
LUG:
hreadedyebolthich
its
into
the
uze
cavity,permittingheavyshells
to
behandled
bymeans
of
awinch.
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LINEARURNINGRATE:The
distancenormal
to
ny
urning
urface
f
he
ropellant
grain
urned
hroughn
nit
ime.
his
propertyependsponhe
hemical
om-
position,
nd
s
otafunction
of
geometry.
LINER:1)Inner
tube,
n
acannon,
which
bears
the
ifling
nd
hich
may
be
replaced
when
worn
ut.
2)
one
f
material
sed
sn
integralpart
of
shapedchargeliner.
LIVE
MMUNITION:mmunition
ontaining
explosives.
his
s
n
ontrast
to
drill
am-
munition
dummymmunition),
hich
on-
tains
oexplosives
nd
s
sedintraining.
LOADING
ENSITY:atio
feight
f
ro-
pellant
in
lb
perin.3)
to
available
chamber
volume.
LONG-DELAY
UZE:
ne
which
willburstthe
projectile
fter
omplete
enetration
nto
hard
round.heres ariation
nhe
time
lement
n
ong-delay
uzes
equired
for
ifferent
ses.
This
s
a
question
to
be
determined
by
the
Ordnance
Dept.)
LO WXPLOSIVE:
xplosive
hich
ndergoes
a
elativelylow
hemical
ransformation,
therebyroducing
deflagration
r
n
x-
plosion,
he
ffect
anging
rom
hat
f
rapid
ombustiono
hat
f ow
rder
detonation.
t
s
uitable
for
se
n
igniter
trains
nd
ertaintypes
of
propellants.
See
PROPELLANT.)
LOW
ORDER
ETONATION:
ncomplete
eto-
nation
f
he
xplosive
harge
n
bomb,
projectile,
r
ther
imilar
igh
explosive.
(See
DETONATION.)
LOWERCCEPTABLEEAN
AXIMUM
PRESSURE:
or
ny
ype
un,thatvalueof
themaximumpressure
which
sspecified
in
theropellantpecification
s
heower
limit
for
he
average
of
the
maximum
pres-
sureshat
reeveloped
y
n
acceptable
smokeless
ropellant
n
propelling
harges
which
ill
mpart
hepecified
muzzle
ve-
locity
othespecified
projectile.
Smokeless
propellant
n
ropelling
harges
hich
n
acceptance
ests
evelops
an
averagemaxi-
mumpressure
owerthanthisvalue
scon-
sideredas
having
failedto
pass
heest.
M
MACH
UMBER:atio
fhe
elocityf
body
o
hat
found
n
he
ame
medium.
MACHWAVE:Supersonicshock
wave.
MAGNUS FORCE: (1)
Forcenormal
to
the
plane
f
aw,aused
y
hespin.
2)
Force
arising
fromnteraction
fpinningbody
an d
the
windstream
when
the
body
s
yawing.
MAGNUS
ORCE,ENTER
F:
anishing
point
of
Magnus
moment.
MAXIMUM
RESSURE:
he
maximum
value
of
the
pressure
exerted
by
thepropellant
gases
onhe
alls
f
gu n
uring
he
iring
of
the
round.
MAXIMUM
KY
RIGHTNESS:
Worst
ossible
sky
ondition
for
observing
pyrotechnic
sig-
nals; usuallyuniform
clouds
or
vercast.
MEPLAT:
Flatnose.
MERCURYULMINATE:
ensitive
xplosive
that
s
etff
y
riction,
mpact,
r
heat,
and
etonates.
ercury
ulminate
s
sed
to
et
ffther
xplosivesn
rojectiles,
mines,
or
bombs.
METAL
OULING:
epositf
etal,
hich
collectsn
he
ore
f
gun,
hat
omes
from
he
ackets
r
otating
ands
f
ro-
jectiles.
MISFIRE:
1)
ailure
ofirerexplodeprop-
erly.
2)
ailurefaprimeror
the
propel-
lingharge
f
rojectile
ounction,
wholly
or
n
part.
Misfire
may
be
contrasted
with
hangfire,
hich
s
elay
n
an y
part
of
afiringcharge.
MULTISECTION
H ARGE:
ropelling
harge
in
eparate-loading
remifixed
mmuni-
tionthat
soaded
ntoanumberofpowder
bags.
ange
djustments
an
e
ade
y
increasing
reducing
he
umberf
ags
used,
s
ontrasted
ith
ingle-section
charge,
n
hich
the
size
ofthechargecan-
not
be
changed.
MUZZLE
LAST:udden
airpressure
exerted
in
he
icinityfhemuzzle
of
aweaponby
the
rush of
ho t
gases
and
air onfiring.
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MUZZLE
RAK E
also
alledECOIL
BRAKE):
evice
ttachedto
the
muzzleof
a
gunhichtilizes
scaping
gasesoreduce
the
ffective
ecoil
orce
f
the
guntubeon
thearriage
r
mount.
nsome
esigns
t
eliminatesorreducesmuzzle
flash.
MUZZLE
LASH:
ndesirable
uminous
gni-
tion
f
nburned
ropellant
ases
ssuing
from
he
muzzle
fgun.
Thegases
gnite
uponmixture
with
atmospheric
oxygen.
MUZZLEELOCITY:
peed
f
projectile
at
the
instant
itleaves
he
muzzle
f
gun.
MUZZLEAVE:
ompression
avereac-
tion
fheir
n
frontf
he
muzzleof
a
weapon
mmediately
after
firing.
N
NERVE GAS: (See
G-SERIES WAR
ASES.)
NONDELAY
UZE:
uzehatunctions
s
result
f
nertia
f
iring
in
or
rimer)
as
issile
s
etarded
uring
enetration
ofarget.
he
nertia
auseshe
iring
pin
totrike
he
rimeror
rimerhe
iring
pin),
nitiating
uzeaction.Thistypeoffuze
isnherentlylowernctionhanhe
superquick
r
nstantaneous
uze,
ince
ts
actionepends
pon
eceleration
retarda-
tion)
f
he
issileuring
enetration
f
thetarget.
NORMALHARG E:
Propelling
chargeemploy-
in g
standard
amount
of
propellant
tofire
a
gun
nder
rdinary
conditions,
as
compared
with
educedhargerupercharge
usedinspecial
circumstances.
NORMAL
ORCE:
1)
Componentofair
resist-
ance
erpendicular
o
he
xisf
he
ro-
jectile
n
he
lane
f
aw
(exterior
ballis-
tics).
2)
ny
force
perpendicular
o
a
given
line
or
surface
(general).
NITROCELLULOSE:
xplosive
ubstance
formed
b y
he
itration
f
otton,r
ome
other
orm
f
cellulose.
Usedasthebase
of
most..
ropellants.
pecificrades
f
nitrocellulosesee
YROCELLULOSE
nd
GUNCOTTON)dependonthedegreeto
which
the
cellulose
isnitrated.
NITROCOTTON:
See
GUNCOTTON.)
N ORM AL
MPACT:
trikingfrojectile
againsturfacehat
serpendicular
o
thelineofflightof
the
projectile.
NOSE
SPRAY:
(See
SPRAY.)
N UTATION :
mall
periodicoscillationabout
themotionofprecession.
N1TROGUANIDINE
nitrated
minomethanami-
dine):
seds
nadditionalbaseofpropel-
lant,
seds"cool
propellant"
becauseof
its
ow
lameemperaturehich
does
ot
erode
un
boresnorproduceasmuchlumi-
nous
lash
s
ingle
ase
nitrocellulose)
propellants.
NITROGLYCERINE:
itrated
ster
fglycerol
in
hichheH
adicals
reeplaced
y
NO2;
sed
s
rimary
ase
f
Britishpro-
pellants
nd
s
elatinizing
gent
f
.
.
propellants,
ut
ot
sed
srimary
ase
of
.
.ropellantsecausets
igh
flame
temperature
acceleratesboreerosion.
NITROGEN
USTARDGASES:
Group
ofblister
gases
imilar
o
mustard
as
ith
arying
chemical
ropertiesndittle
r
o
dor;
gases
affecteyes,nose,
and
lungs.
OBTURATION:
ny
rocesshat
revents
he
escape
f
ases
rom
he
ube
fweapon
during
the
firing
of
aprojectile.
OBTURATOR:
evice
or
makingthetubeof
a
eapon
as-tight,
reventingnyscape
of
as
ntil
he
rojectilehas
leftthe
muz-
zle.
OGIVE:
he
shape
of
the
head
of
the
projectile,
often
onvex
olidofrevolution
generated
by
n
rc
firclehoseenter
ies
on
the
ide
fhe
xisf
evolution
pposite
tothearc.
OPTIMUMCHARG E:
Web
andpropellant
weight
combination
hich
roducesmaximum
e-
locityat
a
specifiedpressure.
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OVERTURNING
O M E N T
of
rojectilen
flight):ouple
bout
n
xis
hrough
he
center
fravity,
perpendicular
to
theplane
of
yaw.
OXYGENALANCE:
atio
f
elf-contained
oxygeno
uel
n
propellant
or
explosive.
PARASHEET:
arachute-likeevice
ade
from
ingle
lat
iece
fmaterial,
r
as
fe w
ieces
s
ts
ize
illpermit;voids
costf
omplex
ore
onstructionfpara-
chute.
PEAKRESSURE:nstantaneousaximum
pressureevelopednheun
chamber
by
burningropellant;
ressuremmediately
preceding
anexpanding
shock
wave.
PERCUSSION
COMPOSITION:
igh-explosive
powder
that is
ignited inome
types
of
firearms by the blow of
he firingpin
against
theprimer
cap.
PERCUSSION
FUZE:
(See IMPACT FUZE.)
PERCUSSION
RIMER:
ap
r
ylinderon-
tainingmallhargefig h
xplosive
that
ayeet
ff
byablow.
Apercussion
primers
sed
n
ll
ixedndemifixed
ammunitionndn
ertai
ypes
f
epa-
rate-loading
mmunitionognite
hemain
propelling
charge.
PERFORATION:assagef issileom-
pletely
throughanobject.
PERMISSIBLE
NDIVIDUALAXIMUMPRES-
SURE:
or
ny
ype
un ,
hatalue
hich
should
ot
exceededyheaximum
pressureevelopedy
ny
ndividualround
underan y
service
condition.
PERMISSIBLEEAN
AXIMUM
RESSURE:
For
ny
ype
un,
hat
alue
hich
hould
no t
e
xceeded
y
he
verage
f
he
maximumressures
eveloped
neries
of
ounds
ired
nderny
ervice
ondi-
tions.
PHOSGENE:olorlesshoking
as
aving
n
odorofnew-mownha y
or
freshcorn;
causes
chokingndoughing,ndnjuriesohe
lungs.
PICRIC
CID
trinitrophenol):ig hxplosive,
more
owerfulhanrinitrotoluene,sed
widelynhe
orm
f
mixtures
ith
ther
nitro
compounds.
PIEZOELECTRICRYSTAL:rystalline
ma-
terialossessing
he
roperty
hat,
when
t
isecahnicallyompressedr
tretched
in
certain
directions,
lectrical
harges
n
direct
roportion
o
hemechanical
train
appear
onthe
crystal
surfaces.
PITCH
of
ifling):eciprocalf
he
wist.
(See
TWIST.)
PLANFORM:Shapeofplan
viewoffins.
PLASTIC
XPLOSIVE:Explosivewhich,within
normal
angesf
atmospheric
temperature,
is
apable
f
eing
olded
nto
esired
shapes.
PLUNGING
FIRE:
Gunfire
that
strikes
earth'ssurfaceat
a
highangle.
the
POINT-BLANK
ANGE:istance,otarget,
that
s
ohorthathe
rajectoryf
bullet
rprojectile
spracticallyastraight,
ratherhanurved,
ine.
oint-blank
range
sne
or
hichnosuperelevations
needed.
POINT
DETONATING
UZE:
uze,
ocatedn
theose
f
rojectile,
hich
s
nitiated
upon
mpact.
POWDER:
ermometimes
ooselysed
or
"propellant"
or
"propellingcharge."
POWDER
RAIN:
1)
rain,
sually
fom-
pressed
lack
owder,
sed
o
btainime
action
n
lder
uzeypes.
2)
rain
of
ex-
plosives
aid
ut
fordestruction
by
burning.
PRACTICE
MMUNITION:mmunitionsed
for
argetractice,mmunitionwithapro-
pellingharge,utith
ithernnert
filler
r
ow-explosive
iller
o
erve
as
a
spotting
charge.
PRECISION:
heuality
f
aving
mall
is-
persionaboutthe
mean.
PRECESSION:
hangen
he
directionofthe
axis
f
otating
ody.
nhis
andbook,
precessioneans
he
low
motion
ithout
nutation.
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P R E S S U R E ,
E N T E R
O F:
h epoint
where
th e
resultant
orceausedby
air
resistancen-
tersects
th eaxis
f
th e
projectile.
P R I M A C O R D :
lexibleabric
tube
containinga
filler
f
high-explosive
E T N
pentareyth-
ritetetranitrate)
hats
used
oransmit
detonation
rom
a
detonator
o
a
booster
or
bursting
harge.
rimacordsh erade
nameor
h e
ype
f
etonat i ng
cord
cur-
rently
in
use.
P R I M E R :
Device
usedto
initiate
th e
functioning
of
nexplosive
r
gniter
rain.
t
m a ye
actuated
y
riction,
l o w ,
eat,
ressure,
orelectricity.
P R I M E R - D E T O N A T O R :
Assemblyconsisting
of
a
rimer
nd
detonator.t
a y
lso
n-
clude
delay
element.
P R I M E R
E A T :
hamber
n
h e
breech
mech-
anism
f
u n
h a t
uses
eparate-loading
ammunition,
into
hi chh erimerset.
P R O B A B L E
R R O R :
n
errorfsuchmagni-
t u d e
h a th erobability
fm ak in gnerror
greater
h a n
t
n
ny
ivenbservation
s
just
qualoh erobability
f
aki ngne
less
h a n
t,
oth
probabilities
eing
ne-
half.
P R O C E D U R E ,E S I G N :
utl ine
of
steps
tofol-
lo windesigning
a n
item.
P R O G R E S S I V E
R A N U L A T I O N :
ropellant
grainhichurnsit h
ontinually
n-
creasing
urface
ntilherainsom-
pletely
consumed.
P R O J E C T I L E :bject,uchsullet
r
shell,
h a t
s
ropelled
romw e a p o ny
anexplosivepropelling
charge.
P R O O F
M M U N I T I O N :
A m m u n i t i o n
incorpora-
ting
olid,
lunt-nosed,
teel
or
ast
ron
shot
f
nexpensive
anufacture;sedn
proof
iring
funs;sedoimulate
h e
weight
f
projectile
designedorh e
gu n
in
adjusting
th e
charge
weight
ofropellant.
PROPAGANDA
HELL:
S e e
EAFLET
SHELL.
P R O P E L L A N T :xplosiveaterial
whose
rate
of
ombustion
s
ow
n o u g h ,
ndts
ther
propertiesuitable,
opermit
tsses
propellingcharge.
P R O P E L L I N G
H A R G E :
xplosive
charge
that
isu r n e dnaw e a p o nto
propel
aprojectile
therefrom
see
R O P E L L A N T ) .urning
f
th eonfinedropelling
harge
roduces
gases
hose
ressure
orces
h e
projectile
out.
P R O X I M I T YU Z E :uze
designed
o
detonate
a
rojectile,
o m b ,
ine,
rcharge
h en
activated
y
nxternal
nfluence
nh e
close
vicinityf
a
target.
P Y R O C E L L U L O S E :itrocellulose
ontai ni ng
12.60
percentnitrogen.
PYROCOTTON:
S e e PYROCELLULOSE.
P Y R OO W D E R :
traight
itrocellulose
ow-
d e r ;
mokeless
propelling
chargeconsisting
of
itrocelluloset h at
has
smaller
nitro-
gen
ontent
h a nuncotton;
ingle-base
propellant.
P Y R O T E C H N I C S :mmunitionontaining
chemicals
h a tproduce
a
smoke
or
brilliant
lightnurni ng,sed
or
signalling,
mark-
ing,potting,
lluminating,etc.
P Y R O X Y L I N
( coUodi on) :
Nitrocellulose
taining8-12percent
nitrogen.
con-
Q U A L I T Y
S S U R A N C E :ystemf
ssuring
t h ataterial
ccepted
s
n
ccordance
w i thequirements,
ncluding
nspection
and
test
procedures,
acceptance
criteria,
etc.
Q U I C K N E S S
propellant
urning):
a tef
c h a n g e
f
pressure
w i thi nth eclose
chamber
wit h
respect
to
time.
R A M :1 )
o
u shntoposition.2)
o
eat
a
projectile
inthe
bore
of
a
gun.
R A M M E R :
1 )
evice
orrivingprojectile
into
osition
n
u n.
t
a ye
a n d -or
power-operatedra rt
f
h e
eceiver
mechanism.
2)
ool
sed
o
emove
ive
projectiles
from
th ebore
of
a
gun.
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R A T E D
A X I M U M
R E S S U R E :ornyyp e
g u n ,
h a t
aluefheaximum
pressure
w h i c h
s
pecified
n
hepropellantpeci-
ficationash e
pper
limitofaverage
pres-
surehicha ybe
developedb ya n
accept-
able
ropellantnheorm
fropelling
charges
hichill
mpart
h epecified
muzzle
velocity
o
hepecified
projectile.
T h e
mokeless
ropellant
n
ropelling
chargeshich,nh ecceptanceest,e-
velopsn
verageaximumpressure
ex-
ceeding
hisvalue
s
considered
as
avi ng
failed
topass
the
test.
R E L A T I V EO R C E :
atio
ofobserved
axi-
m u m
ressure
eveloped
y
ropellant
u n d e r
est
oheaximum
ressure
de-
velopedy
tandard
ropellantn d er
identical
test
conditions.
R E L A T I V E
Q U I C K N E S S :
Ratio
of
the
quickness
(dP/dt)fa
est
propellant
tothequickness
of
tandardropellant,
easured
athe
same
initial
temperature
a nd
loadingdensity
in th esameclosed
chamber.
R E M A I N I N GE L O C I T Y :peedfprojectile
a t
ny
pointalongits
pat h
of
flight.Remain-
in gvelocity
s
usually
measuredinfeet
per
second.
R I C O C H E T :
lancing
after
impact.
r eb o u n dfprojectile
RIFLE:
1 )
nyirearmhat
has
riflinginthe
bore
esignedo
ive
pinohe
pro-
>
ectileorreater
ccuracy
fire
nd
longer
ange
notxtensivelysedn
his
manner,xcept
orhoulderarms).
2)Cu t
spiralgrooves
rifling)
n
he
bore
of
a
gu n
in
ordero
giveapino
heprojectileso
t h at
t
will
avea
greater
ccuracyoffire
and
longer
range.
R I F L I N G :
Spiralgrooves
nth e
bore
ofaweap-
on
designed
o
give
a
pin
o
the
projectile
for
reater
ccuracy
nd
carrying
ower.
Riflingncludes
othh erooves
nd
he
ridges
between,
called
lands.
bycentering
h e
rojectile,
h u spreventing
escapefgas,nd
giving
herojectilets
spinas
tengagesinth e
rifling.
R O U N D :1 )llheartsh a t
a k e
ph e
ammunition
ecessary
n
iring
n e
hot
(also
alled
O M P L E T E R O U N D ) .
2)
ne
shot
fired
b y
a
w e a p o n .
R O U N DO FA M M U N I T I O N :SeeR O U N D . )
S
S A B O T :1 )ightweightarriern
h ic h
subcaliber
projectile
s
entered
o
permit
firing
he
rojectilen
he
arger
caliber
w e a p o n .h e
arrier
ills
he
bore
of
he
w e a p o n
rom
whichhe
projectile
s
ired;
and
ts
ight
weight
permitst
obesafely
fired
at
very
ig h
velocities.
tisnormally
discarded
hort
distance
rom
he
uz-
zle,
nwhich
case
it
is
k n o w nasa
discard-
in g