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|  MIL-L-23822C(AS)
Intended use. The Liquid Propellant Rocket Engine
6.1
LR64 covered by this specification is intended for use in the AQM-
37A missile target.
Procurement documents should
Ordering data.
6.2
specify the following:
a.
Title, number and date of this specification.
b.
The number of rocket engines to be provided.
c.
The number of preproduction rocket engines
to be provided (see 3.2).
d.
Technical data, if any, specified in the contract
or purchase order.
All options or deviations (see 3.2.1).
e.
f.
Test plans, methods, and procedures (see 4.9).
Preproduction test data report (see 4.4.2.1).
g.
h.
Quality Verification Test Data Reports
(see 4.3.2.1).
Three copies of the Quality Verification Test
Data Report (QVT ) shall be forwarded to
NAVAIRSYSCOM/AIR-53512 after each static
firing.
i.
QVT performance rejection analysis (see 4.7.1.1).
Corrective action proposals (see 4.8.1).
j.
k.
Selection of levels of packaging and packing (see
5.1, 5.2).
l. Preservation methods (see 5.1.1.1, 5.1.2.1).
m. Source of GFE containers if required.
n. Request for use of substitute parts or materials
(see 3.3.2.1).
Conflicting requirements
Conflicting requirements.
6.3
between this specification and any specifications, publications or
drawings listed herein should be referred in writing to the procuring
activity or its designated agent for interpretation or clarification.
Definitions. Definitions concerning ballistic nomen-
6.4
clature as contained in MIL-STD-292 are applicable.
24
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