1、 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRICAL, (CIRCULAR, ENVIRONMENT RESISTING), PLUG, THREADED COUPLING, (PUSH-PULL, QUICK-DISCONNECT WITH LANYARD), CRIMP SOCKET CONTACT, SERIES III, CLASSES A, G, M, R, T, W AND Z This specification is approved for use by all Departments and Agencies of the D
2、epartment of Defense. The requirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-83723. FIGURE 1. Plug, dimensions and configuration. AMSC N/A FSC 5935 INCH-POUND MIL-DTL-83723/69B 29 June 2009 SUPERSEDING MIL-C-83723/69A (USAF) 17 December 1991
3、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B 2 LANYARD FIGURE 1. Plug, dimensions and configuration - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B
4、 3 Shell size A B C D E F thread G H 8 .704 (17.88) .290 (7.37) .470 (11.94) .370 (9.40) .305 (7.75) .500-20 UNF-2A .437 (11.10) .294 (7.47) 10 .829 (21.06) .388 (9.86) .600 (15.24) .497 (12.62) .405 (10.29) .625-24 UNEF-2A .572 (14.53) .428 (10.87) 12 1.016 (25.81) .558 (14.17) .724 (18.39) .613 (1
5、5.57) .531 (13.49) .750-20 UNEF-2A .687 (17.45) .598 (15.19) 14 1.079 (27.41) .627 (15.93) .849 (21.56) .738 (18.75) .665 (16.89) .875-20 UNEF-2A .812 (20.62) .667 (16.94) 16 1.204 (30.58) .772 (19.61) .974 (24.74) .863 (21.92) .790 (20.07) 1.000-20 UNEF-2A .937 (23.80) .794 (20.17) 18 1.345 (34.16)
6、 .860 (21.84) 1.030 (26.16) .919 (23.34) .869 (22.07) 1.0625-18 UNEF-2A .992 (25.20) .900 (22.86) 20 1.470 (37.34) .985 (25.02) 1.154 (29.31) 1.044 (26.52) .994 (25.25) 1.1875-18 UNEF-2A 1.117 (28.37) 1.025 (26.04) 22 1.595 (40.51) 1.110 (28.19) 1.279 (32.49) 1.169 (29.69) 1.119 (28.42) 1.3125.18 UN
7、EF-2A 1.242 (31.55) 1.150 (29.21) 24 1.720 (43.69) 1.235 (31.37) 1.404 (35.66) 1.294 (32.87) 1.244 (31.60) 1.4375-18 UNEF-2A 1.367 (34.72) 1.275 (32.39) Shell size J max J min K M 8 .405 (10.29) .396 (10.06) .612 (15.54) 1.095 (27.81) 10 .526 (13.36) .517 (13.13) .737 (18.72) 1.240 (31.50) 12 .696 (
8、17.68) .687 (17.45) .925 (23.50) 1.432 (36.37) 14 .765 (19.43) .756 (19.20) .987 (25.07) 1.490 (37.85) 16 .892 (22.66) .883 (22.43) 1.112 (28.24) 1.711 (43.46) 18 .998 (25.35) .989 (25.12) 1.237 (31.42) 1.815 (46.10) 20 1.123 (28.52) 1.114 (28.30) 1.362 (34.59) 1.962 (49.83) 22 1.248 (31.70) 1.239 (
9、31.47) 1.487 (37.77) 2.070 (52.58) 24 1.373 (34.87) 1.364 (34.65) 1.612 (40.94) 2.195 (55.75) FIGURE 1. Plug, dimensions and configuration - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B 4 Inches mm Inches mm Inches mm
10、Inches mm .031 .79 .092 2.34 .210 5.33 7.00 177.80 .045 1.14 .096 2.44 .290 7.37 .046 1.17 .107 2.72 .309 7.85 .048 1.22 .114 2.90 .320 8.13 .054 1.37 .118 3.00 .330 8.38 .062 1.57 .125 3.18 .400 10.16 .068 1.73 .146 3.71 .500 12.70 .070 1.78 .150 3.81 .510 12.95 .076 1.93 .206 5.23 1.18 29.97 NOTES
11、 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Unless otherwise specified, tolerances shall be .005 (.13 mm) for three place decimals, .01 (0.25 mm) for two place decimals, and 1oand 30 for angular dimensions. 4. The dimensions showing the relationship of the
12、 coupling ring to the shell apply only when the coupling ring is in the full forward position. 5. The quick-disconnect connector plug is intended to be used with series III threaded coupling receptacles (MIL-DTL-83723/82 and MIL-DTL-83723/84), and with the adapter (MIL-DTL-83723/70) permanently atta
13、ched to the receptacle. 6. Coupling of the quick-disconnect plug connector is to be accomplished by a straight axial push with no cocking of the coupling mechanism. 7. Uncoupling of the quick-disconnect plug connector is to be accomplished by a straight axial pull on the outer coupling ring. FIGURE
14、1. Plug, dimensions and configuration - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B 5 Shell size P P1 P2 P3 P4 R R1 8 1.457 (37.01) 1.869 (47.47) 2.018 (51.26) 5.838 (148.29) 1.848 (46.94) .830 (21.08) 4.585 (116.46)
15、10 1.457 (37.01) 1.979 (50.27) 2.100 (53.34) 6.528 (165.81) 1.888 (47.96) .880 (22.35) 5.390 (136.91) 12 1.457 (37.01) 2.124 (53.95) 2.293 (58.24) 7.348 (186.64) 1.928 (48.97) .950 (24.13) 6.330 (160.78) 14 1.457 (37.01) 2.124 (53.95) 2.353 (59.77) 7.348 (186.64) 1.928 (48.97) 1.010 (25.65) 6.330 (1
16、60.78) 16 1.457 (37.01) 2.229 (56.62) 2.502 (63.55) 8.068 (204.93) 2.028 (51.51) 1.070 (27.18) 6.710 (170.43) 18 1.457 (37.01) 2.474 (62.84) 2.614 (66.40) 8.068 (204.93) 2.028 (51.51) 1.130 (28.70) 6.710 (170.43) 20 1.457 (37.01) 2.604 (66.14) 2.739 (69.57) 9.068 (230.33) 2.148 (54.56) 1.190 (30.23)
17、 7.740 (196.60) 22 1.457 (37.01) 2.729 (69.32) 2.864 (72.75) 9.068 (230.33) 2.148 (54.56) 1.260 (32.00) 7.740 (196.60) 24 1.457 (37.01) 2.854 (72.49) 2.989 (75.92) 9.068 (230.33) 2.228 (56.59) 1.320 (33.53) 8.030 (203.96) FIGURE 2. Plug and backshell assembly, dimensions and configuration. Provided
18、by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B 6 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Unless otherwise specified, tolerances shall be .005 (.13 mm) for three place decimals, .01 (0.25
19、mm) for two place decimals, and 1oand 30 for angular dimensions. FIGURE 2. Plug and backshell assembly, dimensions and configuration - Continued. REQUIREMENTS: Dimensions and configurations: See figures 1 and 2. For insert arrangements, see MIL-STD-1554 and table I. TABLE I. Inserts requiring reduce
20、d diameters for lead-in chamfers on contact cavities. Shell size Insert arrangements Contact cavities 8 03 1, 2, 3 10 06 1, 2, 3, 4, 5, 6 For connector accessories: See SAE-AS85049 and MIL-C-83723/16. Unless otherwise specified in the purchase order, the following components shall be furnished with
21、the connector: a. Contacts in accordance with SAE-AS39029 shall be furnished with the connector. Spare contacts are required for each size contact. The total quantity of spare contacts shall be 10 percent or 1, whichever is greater, of the total number of each size contact required. b. Grommet seal
22、plugs in accordance with MS27488 shall be furnished with the connector. Total quantity shall be 15 percent of each contact size or 3, whichever is greater. c. Contact extraction tools in accordance with MIL-I-81969 shall be included in the connector package. Connector assembly shall include a backsh
23、ell to ensure compliance with moisture sealing requirements. See SAE-AS85049 and MIL-C-83723/16. The coupling mechanism of the connector plug shall withstand a minimum tensile load of 100 lb (45.36 kg) minimum. Load shall be applied to the rear accessory hardware in a straight axial direction. The q
24、uick-disconnect connector plug shall meet the vibration and shock requirements in accordance with MIL-DTL-83723. The coupling mechanism shall maintain the plug and receptacle in the locked position during testing. The tensile force required to unlock the coupling mechanism shall be 5 lb minimum and
25、20 lb maximum. The locking mechanism shall meet the performance requirements of MIL-DTL-83723. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/69B 7 Part or Identifying Number (PIN) example: M83723/ 69 W 22 55 N Military designator Spec
26、ification sheet number Class Shell size Insert arrangement Polarizing position Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes. Referenced documents. In addition to MIL-DTL-83723, th
27、is document references the following: MIL-STD-1554 MS27488 MIL-I-81969 MIL-C-83723/16 MIL-DTL-83723/70 MIL-DTL-83723/82 MIL-DTL-83723/84 SAE-AS39029 SAE-AS85049 CONCLUDING MATERIAL Custodians: Preparing activity: Army - CR DLA - CC Navy - AS Air Force - 85 DLA - CC Review activities: (Project 5935-2
28、008-105) Air Force 70, 99 NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
