MIL-STD-176A
power-pwr
fastener--fastnr, fast
pressur-press
feet-ft
propellers--prop
fitting-ftg
protection--prot
forward--fwd
fuselage-fus
quantity-qty
gallons--gal
release-rel
gear--gr
retraction--retr
generator--gen
group-gr
secondary--sec, secondry
seconds-see
hydraulic--hyd
section--sect
stabilizing--stab
inboard--inbd
stiffeners--stiff
inches--in
structure--str
incidence-incid
structural--str
include-incl
supports+sup
induction--ind
surface-sur
injection--inj
synchronizing--syn
installation-instal
instrumentation--inst
temperature-temp
integral--int
theoretical--theo
intermediate-inter
variable--var
launching--launch
ventilating--vent
liquid--liq
volume-vol
location--loc
longeron--longn
longitudinal--long
weight-wt
lubricating--lub
Lubrication--lub
4. GENERAL STATEMENTS AND RE-
material--matl
QUIREMENTS
rnaximum-max
mechanism--mech
4.1 Weight control systems shall provide
miscellaneous--mist
for determination of breakdown weight data
missile-msl
required by the statements, for consistency
mounts--mts
of allocation in accordance with the item al-
locations of the Detail Weight Statement,
nacelle-nac
Part II, and the principles and intent out-
navigation--nav
lined above in paragraph 1.3. Further struc-
number--no
tural and equipment breadowns, and gener-
ous use of footnotes, are encouraged when
operating--opr
such practices will further understanding of
outboard--outbd
the tabulated data and aid in the intended
oxidizer--oxidiz
purposes.
oxygen--oxy
panels--pnl
4.2 The Detail Weight Statement lists en-
parachute--para
tries which generally apply to all missiles.
pneumatic--pneu
However, because of the varied missile con-
4
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