1、INCH-POUND MIL-DTL-32139/5 1 August 2012 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRICAL, RECTANGULAR, NANOMINIATURE, SINGLE ROW, PLUG, POLARIZED SHELL, PIN CONTACTS, VERTICAL PCB THROUGH-HOLE TYPE This specification is approved for use by all Departments and Agencies of the Department of Defense.
2、 The requirement for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-32139. FIGURE 1. Nano connector dimensions and configurations. AMSC N/A FSC 5935 A B C .150 .11 .010 TYP .025 TYP R .018 (RADIUS OPTIONAL) 4X INSULATED CAVITIES .005 C L OF #0-80 UNF-2A,
3、 2X .012 .007 D .010 SEE NOTE 6 SEE NOTE 4 .050 HEX KEY SEE ASME B18.3 .330 .105 .003 TYP (SEE NOTE 5) .003 / .005 X 45 R.005 MAX EPOXY FILLED .115 .080 .010 X C .0575 .010 X C Y .004 X Y C .010 X Y C Y .020 .001 INSULATOR CAVITIES -x- Provided by IHSNot for ResaleNo reproduction or networking permi
4、tted without license from IHS-,-,-MIL-DTL-32139/5 2 Insert arrangement A B BSC C BSC D MAX 9 .500 (12.70) .395 (10.03) .284 (7.21) .295 (7.49) 15 .650 (16.51) .545 (13.84) .434 (11.02) .445 (11.30) 21 .800 (20.32) .695 (17.65) .584 (14.83) .595 (15.11) 25 .900 (22.86) .795 (20.19) .684 (17.37) .695
5、(17.65) 31 1.050 (26.67) .945 (24.00) .834 (21.18) .845 (21.46) 37 1.200 (30.48) 1.095 (27.81) .984 (24.99) .995 (25.27) 51 1.550 (39.37) 1.445 (36.70) 1.334 (33.88) 1.345 (34.16) Inches .001 .003 .004 .005 .007 .010 .012 .018 .020 .025 .050 .0575 .080 .105 .11 .115 .150 .330 mm 0.03 0.08 0.10 0.13
6、0.18 0.25 0.30 0.46 0.51 0.64 1.27 1.46 2.03 2.67 2.8 2.92 3.81 8.38 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Unless otherwise specified tolerances are .005 inch (0.13 mm) angular tolerance 2o. 4. Surface from which the lead length is measured. 5.
7、Shell shall be flush to insulator within .004 inch (0.10 mm). 6. Tail finish is tin/lead or gold. FIGURE 1. Nano connector dimensions and configurations Continued. Inches .0015 .033 .074 .084 mm 0.038 0.84 1.88 2.13 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information
8、only. 3. Unless otherwise specified tolerances are .005 inch (.13 mm). FIGURE 2. Nano connector interface. .0015 X C INTERFACE DETAIL .084 R .033, 2X FULL R, 2X C Y .074 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32139/5 3 NOTES: 1. Enga
9、ging face of insert shown. 2. Cavity identification numbers are for reference only and do not appear on the part. FIGURE 3. Nano connector insert arrangement. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32139/5 4 NOTES: 1. Suggested hole
10、pattern shown facing board from connector insertion side specified on figure 3. 2. Dimensions are in inches. 3. Metric equivalents are given for information only. 4. Unless otherwise specified tolerances are .005 inch (.13 mm) angular tolerance 2o. FIGURE 4. Nano connector suggested PCB hole pattern
11、 Inches mm .001 0.03 .002 0.05 .013 0.33 .016 0.41 .025 0.64 .050 1.27 .0975 2.477 .105 2.67 .111 2.82 Insert arrangement B BSC E 9 .395 (10.03) .200 (5.08) 15 .545 (13.84) .350 (8.89) 21 .695 (17.65) .500 (12.70) 25 .795 (20.19) .600 (15.24) 31 .945 (24.00) .750 (19.05) 37 1.095 (27.81) .900 (22.86
12、) 51 1.445 (36.70) 1.250 (31.75) .050 .001 TYP. .025 .002 .0975 .002 E B .025 .001 TYP. .050 .001 TYP. .013/ .016 TYP. POSITION 1 .105/.111 2X Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32139/5 5 REQUIREMENTS Dimensions and configuration
13、 see figures 1, 2, and 3. This specification sheet describes the pin side of a rectangular connector. This connector uses reverse gender contacts, i.e., the live pin is recessed in the insulator with the static socket protruding from a shrouded interface. Contact connection: The pin contact, which i
14、s recessed in the insulator, is normally connected to the live side of the circuit. Pins are terminated to a printed circuit board (PCB) as specified on figure 4. Mating receptacle: Shall be in accordance with MIL-DTL-32139/6 Part or Identifying Number (PIN): M 32139/ 05- A 01 S N S Space class Shel
15、l and finish Hardware Tail Finish Insert arrangement Detailed specification sheet Basic specification number M prefix Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32139/5 6 Insert Arrangement A = 9 B = 15 C = 21 D = 25 E = 31 F = 37 G = 51
16、 Tail Finish 01 = Tin/Lead 02 = Gold Hardware 1/ S = Jackscrew captivated Shell and Finish C = Aluminum shell, cadmium finish N = Aluminum shell, electroless nickel finish 2/S = Passivated stainless steel shell T = Titanium shell A = Pure Electrodeposited Aluminum Z = Zinc Nickel F = Nickel Fluoroca
17、rbon Polymer Space class Blank for non-space applications S = Space class 1/ Supplied installed. 2/ When aluminum shells are required for space applications, electroless nickel shall be used. Cadmium finish is not acceptable (see MIL-DTL-32139). Alternate shell finishes: Pure Electrodeposited Alumin
18、um. Pure dense electrodeposited aluminum shall be in accordance with MIL-DTL-83488, type II shall withstand 48 hour salt spray. Color shall be non-reflective and shall meet the requirements as specified herein. Nickel Fluorocarbon Polymer. High phosphate nickel with fluorocarbon polymer additive ove
19、r a suitable underplate shall be able shall withstand 48 hour salt spray. Color shall be non-reflective and shall meet the requirements as specified herein. Zinc Nickel. Zinc Nickel Alloy shall be in accordance with ASTM B841, over a suitable underplate shall withstand 48 hour salt spray. Color shal
20、l be non-reflective and shall meet the requirements as specified herein. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32139/5 7 Referenced documents. In addition to MIL-DTL-32139, this document references the following: MIL-DTL-32139/6 MIL
21、-DTL-83488 ASME B18.3 ASTM B841 CONCLUDING MATERIAL Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force - 85 (Project 5935-2010-200) DLA - CC Review activities: Army - AV, MI Air Force - 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 https:/assist.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
