MIL-PRF-24623C
TIA/EIA-455-64
-
Procedure for Measuring Steady State Gamma Radiation-Induced
Attenuation in Optical Fibers and Cables (DoD adopted).
TIA/EIA-455-71
-
Procedure to Measure Temperature-Shock Effects on Fiber Optic
Components.
EIA/TIA-455-98
-
Fiber Optic Cable External Freezing Test.
EIA/TIA-455-107
-
Determination of Component Reflectance or Link/System Return
Loss Using a Loss Test Set (DoD adopted).
(Application for copies should be addressed to the Telecommunications Industry
Association/Electronic Industries Association, 2500 Wilson Boulevard, Arlington,
Virginia 22201-3834.)
(Non-Government standards and other publications are normally available from the
organizations which prepare or distribute the documents. These documents also may be
available in or through libraries or other informational services.)
2.4 Order of precedence. In the event of a conflict between the text of this
document and the references cited herein (except for related associated specifications
or specification sheets), the text of this document takes precedence. Nothing in this
document, however, supersedes applicable laws and regulations unless a specific
exemption has been obtained.
3.
REQUIREMENTS
3.1 Specification sheets. The individual item requirements shall be as specified
herein and in accordance with the applicable specification sheet. In the event of any
conflict between the requirements of this specification and the specification sheet,
the latter shall govern.
3.2 Qualification. Fiber optic splices furnished under this specification shall be
products that are authorized by the qualifying activity for listing on the applicable
qualified products list before contract award (see 4.5 and 6.3). The provisions of
4.5.4 for retention of qualification are included in this requirement.
3.3 Materials. The splice shall be constructed of materials as specified herein and
in the specification sheet (see 3.1). In all cases, materials selected for splice
usage shall meet all qualification requirements as specified, and be of a type and
quality to assure physical, chemical and optical compatibility with the requirements
of this specification. All materials used shall be nontoxic (see 3.3.1), non-nutrient
to fungus (see 3.3.8), and manufactured to good workmanship quality (see 3.8). For
space flight applications, materials shall not release in excess of 1 percent total
mass loss or 0.1 percent collected volatile condensable materials when tested in
accordance with ASTM-E-595.
3.3.1 Toxic and hazardous products and formulations. The products used in the
splice construction shall not give off toxic or explosive fumes when exposed to flame.
Materials used shall have no adverse effect on the health of personnel when used for
the intended purpose.
3.3.2 Interior parts. The materials used for splice interior parts shall provide 20
year service. No incompatibility shall exist between the materials employed such that
degradation of these materials can result from in-service use or from test exposures
as specified herein.
3.3.3 Exterior parts. Exterior parts of the assembled splice, if metallic, shall
have a passivated finish which permits the attainment of a suitable surface finish
condition in accordance with high workmanship standards and shall be compatible with
external coatings or platings of the type and color specified in the specification
sheet (see 3.1).
3.3.4 Finish. The resultant finish on all cable splice closures (see 6.4.13) shall
meet the requirements herein.
3
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business