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|  MIL-P-82691A(OS)
s o l i c i t a t i o n Unless otherwise specified, the issues of documents
not listed in the DODISS shall be the issues of documents cited
in the solicitation (see 6.2).
AMERICAN
SOCIETY
FOR
TESTING
AND
MATERIALS
ASTM
D412
Method of Tensile Testing
of Vulcanized Rubber
(Application
for copies should be addressed to American
Society
for Testing and Materials, 1916 Race Street, Philadelphia, PA
19103. )
2.3 Order of precedence. in the event of l conflict between the
text of this document and the references cited herein, the text
of this document tales precedence. Nothing in this document, how-
ever , superesedes applicable laws and regulations unless a speci-
fic exemption has been obtained.
3.
REQUIREMENTS
3.1
First l rticle. When specified (see 6.2) ,
a sample shall be
furnished
for first article inspection and approval (see 4.4 and
6 .3).
The grain shall
conform
with
the
3.2 Grain configuration.
requ-
irements of the drawings
cited herein.
3.3 Chemical composition. The propellant
shall
have
the
composi-
tion specified in MIL-P-23482.
The
physical
properties
shall
conform
to
3.4 Physical
properties.
Table I.
Table I.
Physical
properties
requirements.
examination. The igniter propellant grain shall
3.5
Radiographic
foreign
fissures or
no evidence of porosity,
cracks ,
exhibit
largest
and shall contain no more than one hole whose
material
whose
inch and no more than two holes
exceeds
1/16
dimension
There shall be no more than
largest dimension exceeds 1/32 inch.
inch.
l xceeds 1/16
dimension
two high density areas whose largest
3.6 Ballistic properties . The igniter as shown on DL SA 2785411
shall demonstrate the ball istic characteristics shown in Table II
when tested at 10 deg. and 120 deg. F.
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