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MIL-L- 23822C(AS)
4.4.4 (Cont'd)
Failure of one or more engines to comply with any of these re-
quirements shall be cause for rejection of the preproduction
test sample.
Quality conformance tests and examinations.
4.5
Each sample, selected in accordance with 4.3.2, shall be sub-
jected to examinations and tests as follows:
Requirement
*
Examinations
4.5.1
3.3.1
a. C onstruction and dimen-
sions
3.3.2
b. Materials
3.3.3
c.  Moisture, fungus and
corrosion
d.  Protective coatings and
3.3.4
surface treatments
e,  Marking
3.3.5
3.3.6
f.  Threads
3.3.7
g. Interchangeability
3.3.8
h. Weight
3.8
i.  Cleanliness
3.9
j.  Workmanship
*
4.5.2
Tests.
a.
Rocket engine performance 4. 5.4.1
4.5.4.2
b.
Ablation
4.5.4.3
c.
Smoke emission
4.5.4.4
d.
Thrust build-up
4.5.4.5
e.
Thrust tail-off
4.5.4.6
f.
Thrust variation
4.5.4.7
g.
Operating range
4.5.5
h.
Leakage
*
4.5.2.1
Test conditions. Tests of the rocket engine, unless
otherwise Specified, shall be conducted under the following ambinet
conditions:
18

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