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MIL-PRF-29504-5D-2010

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MIL-PRF-29504-5D-2010 MIL-PRF-29504/5D w/Amendment 1 1 July 2010 SUPERSEDING MIL-PRF-29504/5D 20 December 2006 PERFORMANCE SPECIFICATION SHEET TERMINI, FIBER OPTIC, CONNECTOR, REMOVABLE, ENVIRONMENT RESISTING, SOCKET TERMINUS, SIZE 16, REAR RELEASE, MIL-DTL-38999, S...
MIL-PRF-29504-5D-2010
MIL-PRF-29504/5D w/Amendment 1 1 July 2010 SUPERSEDING MIL-PRF-29504/5D 20 December 2006 PERFORMANCE SPECIFICATION SHEET TERMINI, FIBER OPTIC, CONNECTOR, REMOVABLE, ENVIRONMENT RESISTING, SOCKET TERMINUS, SIZE 16, REAR RELEASE, MIL-DTL-38999, SERIES III This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product described herein shall consist of this specification and MIL-PRF-29504. FIGURE 1. Socket terminus AMSC N/A FSC 6060 INCH-POUND The documentation and process conversion measures necessary to comply with this amendment shall be completed by 3 January 2011. MIL-PRF-29504/5D w/AMENDMENT 1 2 NOTES: 1. Dimensions are in inches, except diameter "A" which is dimensioned in metric (microns). 2. Metric equivalents are given for general information only. 3. Unless otherwise indicated, all diameters are to be concentric with respect to datum A within .003 inch (0.08 mm). 4. Dimensions apply after plating when applicable. 5. Free length prior to installation in the connector. 6. Alignment sleeve and body design optional, not to exceed maximum envelope dimensions. 7. For alignment sleeve design, engagement force shall be less than preload force of the spring. For solid alignment sleeve design, the inside diameter (I.D.) shall be .06251 to .06270 inch (1.588 to 1.593 mm). For split alignment sleeve design, the (I.D.) tolerance does not apply. 8. Hole circular run-out in table I is relative to datum A. 9. Ferrule end face may be flat or have a radius that does not exceed a curvature of .39 inch (10 mm). Recommend inspection documentation advises that an end face curvature of .98 inch (25 mm) falls between that of a flat end face and one with a curvature of .39 inch (10 mm). 10. Hole "A" diameter and tolerance are specified in table I. 11. Manufacturer’s symbol or trademark location is in front of the first TICC band (see figure 1 of MIL- PRF-29504). As an alternative to TICC bands, each digit of the TICC may be designated by the number which corresponds to the color band. An alternate location of the marking shall be allowed only in the case of insufficient surface area and only if approved by the qualifying activity. 12. Ferrule surface shown to have either a chamfer within 25o to 65o angle X .010 minimum or a .010 R minimum. 13. Optional dimension: Maximum allowable edge break is .015 inch (0.38 mm) 14. Alignment sleeve surface shown to be either .003 R minimum or chamfer within 25o to 65o angle X .003 minimum. 15. Alignment sleeve cover is optional for a non-ceramic alignment sleeve. For use with ceramic ferrules, ceramic alignment sleeves are preferred for new design. 16. Termini qualified to this specification sheet shall meet the performance requirements when inserted into a connector with clip-to-clip dimensions of .756 to .808 inch (19.20 to 20.52 mm). 17. Terminus design shall accommodate a single fiber cable with a maximum diameter of .087 inch (2.2 mm). 18. Ferrule diameter for ceramic: .06246 to .06250 inches (1.5865 to 1.5875 mm), ferrule diameter for metal: .06230 to .06248 inches (1.5824 to 1.5870 mm). 19. For interoperability with a standardized polishing puck, the length of exposed ferrule or the length of ferrule protrusion from the ferrule end face to the terminus first face of barrel (body) shall be .158 inches (4.01 mm) minimum. FIGURE 1. Socket terminus - Continued. Inches mm Inches mm .002 0.05 .117 2.97 .003 0.08 .127 3.23 .006 0.15 .130 3.30 .029 0.74 .225 5.72 .033 0.84 .528 13.41 .072 1.83 .546 13.87 .092 2.34 .735 18.67 .101 2.57 1.223 31.06 .103 2.62 1.500 38.10 .110 2.79 MIL-PRF-29504/5D w/AMENDMENT 1 3 20. Termini qualified to this specification sheet shall meet the performance requirements when inserted into a connector with clip-to-clip dimensions of .756 to .808 inch (19.20 to 20.52 mm). 21. For style 1 and 3 terminus only, reduction of the .225 inch (5.72 mm) minimum length to .025 inch (0.63 mm) is allowed. Additionally there shall be a smooth ramp transition on the terminus between the terminus barrel and the crimp sleeve/heat shrink so as not to restrict the function of the insertion and removal tool during the removal operation. 22. Terminus compression spring shall withstand an applied force of 8 pounds minimum with no damage. FIGURE 1. Socket terminus - Continued. Part or identifying number (PIN): See table I of this document and 6.6 of MIL-PRF-29504. M 29504 / 05 -XXXX Military designator Basic specification Specification sheet TICC code (see table I) Usage: Termini compliant with this specification sheet are intended to be used in MIL-DTL-38999 connectors as applicable, and may be used in connectors other than MIL-DTL-38999 at the discretion of the acquiring activity. Termini compliant with this specification may not meet all requirements of MIL-DTL- 38999 if not used in a series III connectors. REQUIREMENTS: Temperature ranges: Operating -67°F to 329°F (-55°C to +165oC) Non-operating -40°F to 185°F (- 40°C to + 85oC) Storage -40°F to 185°F (- 40°C to + 85oC) Fabrication procedure. Standard fabrication procedure (for terminus placement/termination onto the end of an optical fiber), including epoxy specified in the procedure, shall be used for test sample terminations. Test sample configurations and fabrication shall be performed as specified in NAVSEA Drawing 8283255. A copy of this document can be obtained at Web Site: https://fiberoptics.nswc.navy.mil/ in the NAVSEA Drawing section under Component Information. MIL-PRF-29504/5D w/AMENDMENT 1 4 Design and construction: Dimensions and configuration: See figure 1 and table I. Pre-polished termini may have either flat or radiused end faces. Regardless of the end face geometry, the terminus shall meet the requirements of this specification when terminated using the procedures specified. Weight: 1.0 gram maximum. TABLE I. TICC numbers and "A" (ferrule hole) diameter for specified optical fiber sizes. 1/ Applicable to any single mode core size. Also applicable to any multimode core size when enhanced performance is required and cladding tolerances permit. 2/ Circular run-out of 0.5 microns preferred, as it becomes more standard in industry. 3/ Termini with metal ferrules are intended primarily for legacy systems. Fiber size (core/cladding) µm Ferrule hole diameter µm Ferrule material Circular run-out µm TICC style 1 TICC style 2 TICC style 3 Single mode < 9/125 1/ 125 +1, -0 Ceramic 1 2/ 4309 4312 4315 Single mode < 9/125 1/ 125.5 +1, -0 Ceramic 1 2/ 4310 4313 4316 Single mode < 9/125 1/ 126 +1, -0 Ceramic 1 2/ 4311 4314 4317 Single mode 9/125 1/ 125 +1, -0 Ceramic 1 2/ 4236 4246 4279 Single mode 9/125 1/ 125.5 +1, -0 Ceramic 1 2/ 4237 4247 4280 Single mode 9/125 1/ 126 +1, -0 Ceramic 1 2/ 4238 4248 4281 50/125, 62.5/125 126 +2, -0 Ceramic 2 4239 4249 4282 50/125, 62.5/125 127 +2, -0 Ceramic 2 4046 4250 4283 62.5/125/153 156 +3, -0 Ceramic 3 4240 4251 4284 62.5/125/155 157 +3, -0 Ceramic 3 4241 4252 4285 100/140 142 +3, -0 Ceramic 4 4049 4253 4286 100/140 145 +3, -0 Ceramic 4 4050 4254 4287 100/140/172 173 +1, -0 Ceramic 2 4296 4297 4298 100/140/172 173 +3, -0 Ceramic 4 4088 4255 4288 100/140/172 175 +3, -0 Ceramic 4 4242 4256 4289 200/230 236 +4, -0 Ceramic 8 4243 4257 4290 200/280 286 +4, -0 Ceramic 8 4244 4258 4291 400/440 448 +4, -0 Ceramic 8 4245 4259 4292 50/125, 62.5/125 127 +3, -0 Metal 3/ 3 4260 62.5/125/155 157 +3, -0 Metal 3/ 3 4261 100/140 142 +3, -0 Metal 3/ 4 4262 100/140/172 175 +3, -0 Metal 3/ 4 4263 200/230 236 +4, -0 Metal 3/ 8 4264 - - ` ` , ` ` ` , ` , , , , ` ` , , ` , ` , , , , , , ` , - ` - ` , , ` , , ` , ` , , ` - - - MIL-PRF-29504/5D w/AMENDMENT 1 5 Cable strain relief capture mechanism. Three styles for a capture mechanism are specified for this terminus design (see table I). Cable strain relief capture mechanism shall not interfere with intended sealing performance of wire grommet seal, a component in the MIL-DTL-38999 connector, or with the functionality of the insertion and removal tools (see table II). Style 1: Captive strength member outside barrel (body) with shrink sleeve. Style 2: Captive strength member inside terminus barrel (body). Style 3: Captive strength member outside terminus barrel (body) with crimp sleeve. The terminus shall meet all the requirements when the crimp sleeve is assembled to the terminus using a crimp die with flats measuring .088 ± .001 inch (2.235 ± .025 mm) across and .150 inch (3.81 mm) maximum long. The crimp die shall not contain an optional protrusion on either upper or lower die. Tools: See table II. TABLE II. Tools Tool PIN Insertion tool M81969/14-03 Removal tool M81969/14-03 Mating terminus: MIL-PRF-29504/4. Circular run-out: Not greater than the value specified in table I. Frequency of terminus end face cleaning. Unless otherwise specified, terminus may be cleaned before or after each test if the connector is demated. Cleaning shall not be performed during the ten successive mates for the insertion loss test. Unless otherwise specified, cleaning may be performed during mating durability before each optical transmittance measurement. Terminus end face cleaning shall be performed for the post optical transmittance measurement after the salt spray test. The optical transmittance measurement is performed after the general cleaning and inspection for corrosion. Cleaning may be performed at other times when degradation in optical performance occurs. Cleaning performed as a corrective action for degraded optical performance shall be noted on the data sheet. Unless otherwise specified, cleaning of the optical end faces is to occur without removal of termini from the connector. Qualification inspection. Inspections and sequence shall be performed as listed in table III. - - ` ` , ` ` ` , ` , , , , ` ` , , ` , ` , , , , , , ` , - ` - ` , , ` , , ` , ` , , ` - - - MIL-PRF-29504/5D w/AMENDMENT 1 6 TABLE III Qualification inspections. Test procedure Sample size Unterminated termini 1/ Size Weight Identification markings Workmanship Circular run-out Terminus retention Terminus engagement and separation forces Terminus cleaning Termini as part of single fiber cable 2/ Cable pullout force 3/ Salt spray Termini in multiple termini connector 4/ Group 1 5/ Interoperability 6/ Insertion loss (initial) Return loss (single mode only) Group 2 7/ Mating durability Terminus cleaning Return loss (single mode only) Mechanical tests Shock Vibration Insertion loss (verification) Return loss (single mode only) Group 3 7/ Environmental tests Thermal shock Temperature life Insertion loss (verification) Return loss (single mode only) 1/ Sample size shall be sufficient to ensure quantity of termini for inspections as part of a single fiber cable and inspections as an integral part of a multiple fiber connector. 2/ A minimum sample size of 16 socket termini shall be used. 3/ Cable pullout force shall be performed when mated to M29504/04 pin termini. Change in optical transmittance shall be measured after the test only. Minimum of 16 socket termini shall be used for salt spray. 4/ Six (6) test samples (mated connector assemblies, fully populated with termini, consisting of MIL-DTL-38999 shell size 17 series III connectors with inserts containing 8 cavities) shall be used in accordance with test sample configuration in NAVSEA Drawing 8283255. 5/ Four (4) test samples from those in 3/ shall be used for group I inspections except for interoperability. - - ` ` , ` ` ` , ` , , , , ` ` , , ` , ` , , , , , , ` , - ` - ` , , ` , , ` , ` , , ` - - - MIL-PRF-29504/5D w/AMENDMENT 1 7 TABLE III Qualification inspections - Continued. 6/ Two (2) separately designated test samples (instead of 3/) shall be used for interoperability testing per NAVSEA drawing 8283255. 7/ Two (2) sets of test samples from group I (see 4/) shall be used for groups II and III testing. Inspections for un-terminated termini: Test sample configuration. Test fixture for this test shall include MIL-DTL-38999 shell size 11, 13, or 17, series III connectors, utilizing both plug and receptacle for retaining the termini during testing. A minimum sample size shall be used to ensure sufficient quantity for termini inspections as part of a single fiber cable and for termini inspections as an integral part of a multiple fiber connector. Identification markings. The Termini Identification Color Coding (TICC) bands shall be marked on the barrel of the termini or use of the allowed alternative markings as stated in 11/ of figure 1. Manufacturer’s symbol or trademark shall be in accordance with 11/ of figure 1. The manufacturer shall list the symbol or trademark with SAE in accordance with SAE AIR 1351. Terminus retention. Terminus displacement measurement is not applicable. Test may be used as one operational means to verify acceptable shoulder construction. Terminus engagement and separation force. Test is not applicable for socket terminus with solid alignment sleeves. For socket terminus with split alignment sleeves, maximum engagement force shall be 30 ounces (8.3 N) using a .0625 inch (1.588 mm) diameter gauge pin. The separation force is not applicable. Maintenance aging. Not applicable. Fungus resistance. Not applicable. Inspections for the terminus as part of a single fiber cable: Test sample configuration. Each terminus is to be terminated on one end of a single fiber cable. Cable used is to have provisions compatible with termini strain relief, as applicable. Termini, selected from the group that passed inspections for un-terminated termini (group 1), shall be used. A minimum sample size of 16 pin termini and 16 of the applicable counterpart socket termini, selected from the group that underwent inspections for un-terminated termini, shall be used. Fiber pull out force. Not applicable (This test is used for terminus configurations with no type of cable strain relief). Cable pull out force. Applicable for terminus configurations with any mechanism for cable strain relief. The change in optical transmittance shall be measured after the test for a socket terminus. - - ` ` , ` ` ` , ` , , , , ` ` , , ` , ` , , , , , , ` , - ` - ` , , ` , , ` , ` , , ` - - - MIL-PRF-29504/5D w/AMENDMENT 1 8 Salt spray. Test samples (termini on single fiber cable) shall be tested to TIA/EIA-455-16, test condition C. Terminus ferrule may be covered up to half way from the end face to the shoulder with plastic protective (dust) covers. No corrosive effects shall be seen on the external connector parts that would be detrimental to the operation of the connector. No optical degradation shall occur as a result of this test. The criterion for insertion loss verification shall be used to determine if this optical requirement is met. Insertion loss verification, with termini inserted into a MIL-DTL-38999 shell size 17; series III connector, shall be performed both prior to and after the salt spray test. Inspections for termini as an integral part of a multiple termini connector: Test sample configuration: Four test samples (mated connector assemblies) shall be used for group I inspections except for interoperability. Two of these four mated connector assemblies shall be used for group II inspections and two for group III inspections. Each mated connector assembly shall be comprised of a cable assembly with termini placed into MIL-DTL-38999 shell size 17, series III connectors. These termini/connectors are located in the middle of the cable assembly. Termini, selected from the group that passed inspections for un-terminated termini, shall be used and inserted into MIL-DTL-38999 shell size 17 or higher, series III connectors as part of the cable assembly that comprises each test sample. Cable assembly length shall be 10 meters with the connector mated pair inserted 5 meters from the cable ends. Cable length may be longer (with added cable at the optical source end) if cut-backs are performed to verify insertion loss. Each connector shall be fully populated with termini. At least 8 randomly selected termini pairs in each cable assembly shall be monitored for optical transmittance after and when specified, during environmental and mechanical testing. Insertion loss shall be performed on all termini pairs in each cable assembly. Connectors used in the cable assembly, both the plug and receptacle types, are to include backshells. Selection of the backshell is to include assurance of proper strain relief for each single fiber cable and not cause degradation in optical performance. Test sample configurations, fabrication methods and the specific test methods and practices shall be as specified in NAVSEA Drawing 8283255. Interoperability. Applicable, except test for terminus insertion and removal forces is not required. Testing shall be performed using two separately designated cable assemblies with fully populated, MIL-DTL-38999, series III, shell size 17 connectors. Test performance and test sample configurations/fabrication shall conform to NAVSEA Drawing 8283255. As part of the interoperability inspection, terminus on the end of single fiber cable, shall be inserted and removed from the connector to verify that the strain relief is compatible with the tools listed in table II. At the discretion of the preparing activity, selected configurations may be specified to undergo inspections for shock, vibration, and mating durability. Interoperability is applicable only for termini among vendors with the same TICC such as fiber size, ferrule hole diameter, and ferrule material (see table I) with one addition. Termini shall be interoperable regardless of the style. Qualification by similarity will be given to a terminus in the same row in table I as the terminus tested for interoperability. This qualification by similarity is valid if the only difference between the terminus tested for interoperability and the terminus configuration in the same row in table I is a different cable strain relief capture mechanism and TICC markings. Optical source wavelength. Termini with single mode fiber shall be tested using an optical source at the 1,310 nm wavelength. Termini with multimode fiber can be tested using an optical source at either the 850 nm or the 1,300 nm wavelength. - - ` ` , ` ` ` , ` , , , , ` ` , , ` , ` , , , , , , ` , - ` - ` , , ` , , ` , ` , , ` - - - MIL-PRF-29504/5D w/AMENDMENT 1 9 Launch conditions shall conform to NAVSEA Drawing 8283255: Insertion loss. The initial insertion loss and the insertion loss verification for the various fiber sizes and ferrule materials shall be as specified in table IV. The insertion loss limits specified are the maximum allowed values for each measurement (each mating with respect to the pre-cut back measurement), not the average of the ten mating or other averaging schemes. TABLE IV. Optical insertion loss performance. 1/ Fiber size (um) Termini in non-tight tolerance M38999 2/ Termini in tight toleran
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