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MIL-C-24604(SH)
( A p p l i c a t i o n  for  copies  should  be  addressed  to  the  National
Aero-
nautics  and  Space  Administration,  Washington,  DC  20546.)
and  technical
association
specifications
and
(Technical
society
They
are
standards  are  generally  available  for  reference  from  libraries.
also  distributed  among  technical  groups  and  using  Federal  agencies.  )
REQUIREMENTS
3.
First  article  inspection.  Prior  to  beginning  production,  sample
3.1
c y l i n d e r s  snail  be  examined  and  tested  as  specified  in  4.3  (see  6.3).
Ability  of the  cylinders  to  meet  the  performance  and  environmental  require-
ments  of  this  specification  shall  be  demonstrated  by  the  first  article
M a t e r i a l s ,  design,  or  construction  shall  not  be  altered
inspection.
following  first  article  acceptance.
3.2
Design
and
construction.
3.2.1
Design.  The  cylinders  shall  consist  of  fiberglass  filaments
impregnated  with  a  thermosetting  plastic  resin  and  wound  on  a  metal  liner.
The  metal  liner  shall  not  be  stressed  above  its  elastic  limit  at  cylinder
pneumatic  pressure  up  to  proof  pressure:  the  liner  shall  not  be  stressed
above  95  percent  of  its  compressive  yield  strength,  cylinder  unpressurized;
and  the  maximum  strength  in  the  glass  filaments  at  the  6300  pounds  per
operating  pressure  shall  not  exceed  30  percent
,
square inch
of  the  filament  stress  at  virgin  hydrostatic  burst  pressure  of  the
Stresses  shall  be  computed  by  the  Computer  Code  NASA  CR-72124.
cylinder.
or  other  equivalent  analytic  techniques.
Operating
characteristics
of
3.2.1.1
O p e r a t i n g  characteristics
.
the
cylinder
shall  be  as  follows:
- Normal  room  temperature  (75F
5F) -
Operating
pressure
(a)
5000
-  High  temperature  (160F)  - 6300
Low  temperature  (minus  20F)  -  3700
Proof  pressure  - 7500
(minimum)
(b)
(minimum)
Burst  pressure  -  15,000
(c)
Temperature  range  - Minus  20F  to  160F
(d)
Useful  cyclic  life  (without  liner  leakage)  -  500
fill
cycles
(e)
or  100  fill  cycles  plus  3500  temperature  cycles
from
minus
20F  to
Dynamic  fatigue  life  -  10  years
(f)
Leakage  less  than  5  percent  pressure  in  10 years
(g)
Physical
characteristics
shall
Physical
characteristics.
3.2.1.2
be
as  follows:
Port  fitting  -  302,  304  or  316  series  CRES  1-1/8  inch
(a)
12-UNF-3A  external  thread  (port  fitting  detail  shall  be
in  accordance  with  detail  "X"  of  MS26545  for  internal  and
external  dimensions).
3

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