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|  MIL-P-82691A(OS)
test.
The
4.7.1.3
Ballistic
ballistic
properties
shall be
determined when the grain is installed as an igniter assembly for
static testing in accordance with drawing SA DL 2785411 less the
nozzle assembly.
The samples shall be conditioned at 105deg. F
and 1205 deg. F as, applicable (see 4.5.1), , for a minimum of
one hour prior to testing.
5.1 Packaging and packing. Unless otherwise specified in the
contract the packaging and packing shall be in accordance with
49
CFR 100-177 and MIL-P-116,
method
IIb (see 6.2).
5.2 Harking. Unless otherwise specified in the contract (see 6.2)
and in addition to any special marking required by such contract,
unit packages and shipping containers shall be marked in accorda-
nce With
requirements of MIL STD-129 and 49CFR 100-177 and CFR
178-199.
Marking shall include, but not be limited to the follo-
wing:
(a)
Manufacturer `s name
(b)
Material
trade
name
(c)
Gross
and
net
weights
(d)
Lot
number,
serial
numbers,
and
date
of
manufacture
(e)
Number and
revision letter
of
this
specification
and
acceptance
drawings
(f)
Hazard
notice
(g)
Unusual
storage
requirements
6.
NOTES
(This section contains information of a general or
explanatory
nature that may be helpful , but is nor mandatory. )
6,1 Intended use. The propellant covered by this specification
is intended for use in the Mark 272 Mod 0 Igniter for the Mark 30
Rocket Motor in accordance with MIL-R-23481.
6.2
Acquisition requirements.
should d
Acquisition
documents
specify the following:
Title,
number,
revision
letter
of
this
specification
a.
Issue
b.
of DODISS to be cited in the solicitation and,
if required, the specific issue of individual documents
referenced (see 2.1 and 2.2).
Whether a
first
article
sample
is
required
(see
3.1,
4.4
c.
and 6.3)
7
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