DLA MIL-DTL-55302 191 C-2011 CONNECTORS PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES PLUG PIN CONTACTS DECADE INCREMENTS 10 THRU 100 POSITIONS PRINTED WIRING BOARD ( 075 SPACING).pdf

1、AMSC N/A FSC 5935 MIL-DTL-55302/191C 21 March 2011 SUPERSEDING MIL-DTL-55302/191B 10 February 2009 DETAIL SPECIFICATION SHEET CONNECTORS, PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES: PLUG, PIN CONTACTS, DECADE INCREMENTS 10 THRU 100 POSITIONS, PRINTED WIRING BOARD (.075 SPACING) This specification i

2、s 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 sheet and MIL-DTL-55302. FIGURE 1. Connector, plug, .075 (1.91 mm) spacing. INCH-POUND Provided by IHSNot for ResaleNo repr

3、oduction or networking permitted without license from IHS-,-,-MIL-DTL-55302/191C 2 FIGURE 1. Connector, plug, .075 (1.91 mm) spacing - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55302/191C 3 FIGURE 1. Connector, plug, .075 (1.

4、91 mm) spacing - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55302/191C 4 FIGURE 1. Connector, plug, .075 (1.91 mm) spacing - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from

5、IHS-,-,-MIL-DTL-55302/191C 5 Number of contacts Dimensions A .010 BSC B BSC C BSC D E .010 10 .798 (20.27) .618 (15.70) 0.300 (7.62) .968 (24.59) 1.138 (28.91) 20 1.173 (29.79) .993 (25.22) 0.675 (17.15) 1.343 (34.11) 1.513 (38.43) 30 1.548 (39.32) 1.368 (34.75) 1.050 (26.67) 1.718 (43.64) 1.888 (47

6、.96) 40 1.923 (48.84) 1.743 (44.27) 1.425 (36.20) 2.093 (53.16) 2.263 (57.48) 50 2.298 (58.37) 2.118 (53.80) 1.800 (45.72) 2.468 (62.69) 2.638 (67.01) 60 2.673 (67.89) 2.493 (63.32) 2.175 (55.25) 2.843 (72.21) 3.013 (76.53) 70 3.048 (77.42) 2.868 (72.85) 2.550 (64.77) 3.218 (81.74) 3.388 (86.06) 80

7、3.423 (86.94) 3.243 (82.37) 2.925 (74.30) 3.593 (91.26) 3.763 (95.58) 90 3.798 (96.47) 3.618 (91.90) 3.300 (83.82) 3.968 (100.79) 4.138 (105.11) 100 4.173 (105.99) 3.993 (101.42) 3.675 (93.35) 4.343 (110.31) 4.513 (114.63) FIGURE 1. Connector, plug, .075 (1.91 mm) spacing - Continued. Provided by IH

8、SNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55302/191C 6 Inches mm Inches mm Inches mm .001 0.03 .0375 0.95 .150 3.81 .002 0.05 .0625 1.59 .156 3.96 .005 0.13 .075 1.91 .170 4.32 .006 0.15 .078 1.98 .172 4.37 .008 0.20 .080 2.03 .200 5.08 .010 0.25 .08

9、2 2.08 .300 7.62 .014 0.36 .085 2.16 .315 8.00 .020 0.51 .086 2.18 .375 9.53 .023 0.58 .100 2.54 .400 10.16 .0245 0.62 .109 2.77 .490 12.45 .0255 0.65 .110 2.79 .545 13.84 .027 0.69 .125 3.18 .700 17.78 .135 3.43 2.00 50.80 .141 3.58 3.30 83.82 NOTES: 1. Dimensions are in inches. 2. Metric equivalen

10、ts are given for information only. 3. Unless otherwise specified, tolerances are +.005 (0.13 mm). 4. These connectors mate with connectors specified in MIL-DTL-55302/190 using appropriate hardware. 5. Numbers indicating the first and last position in each row and every fourth contact position in bet

11、ween shall be marked on the side(s) of the connector. As an option to the above, numbers indicating every fourth cavity may be stamped on the side of the connector, with exception that the number one contact shall be marked. 6. Handle shape optional. FIGURE 1. Connector, plug, .075 (1.91 mm) spacing

12、 - Continued. REQUIREMENTS Dimensions and configuration: See figure 1. Material: Guide pins, type X guide sockets, jackscrews, and jacksockets shall be made of corrosion resisting stainless steel in accordance with ASTM A581/A581M or ASTM A582/A582M, passivated in accordance with SAE-AMS-2700, or sh

13、all be corrosion resistant copper nickel alloy (61 2 percent copper, 25 2 percent nickel, 2.5 percent maximum other, and the balance zinc) and shall have a brinell hardness of 145 to 175. Type Y guide sockets shall be beryllium copper in accordance with ASTM B196/B196M or ASTM B197/B197M, nickel pla

14、ted in accordance with SAE-AMS-QQ-N-290, class 02, 50 to 150 microinches. Plating: The contact plating shall be in accordance with MIL-DTL-55302, or gold in accordance with ASTM B488, type II, code C, class 1.27, over nickel plating in accordance with SAE-AMS-QQ-N-290, class 02, 50 to 150 microinche

15、s in the engaging area and gold in accordance with ASTM B488, type II, code C, class 0.51 or type III, code A, class 0.51, over nickel plating in accordance with SAE-AMS-QQ-N-290, class 02, 50 to 150 microinches in the termination area. Provided by IHSNot for ResaleNo reproduction or networking perm

16、itted without license from IHS-,-,-MIL-DTL-55302/191C 7 Contact identification: See figure 1. Jackscrews and jacksocket torque: 2 inch pounds max fully mated. Contact resistance: The average contact resistance of all contacts measured shall not exceed 0.007 ohm, and no individual contact pair shall

17、have a resistance exceeding 0.015 ohm. Dielectric withstanding voltage: Sea level: 750 volts rms. High altitude: 250 volts rms at 70,000 feet. Current rating: 3.0 amperes maximum per contact. Polarization: Type X regular, guide pin and socket, full round (see figure 1). Type Y, adjustable “D” shaped

18、 guide pin and socket (see figure 1, detail A). All connectors are supplied in the -1 polarized position. For other than OEM use, connectors may be repolarized by using M55302/57-01 spanner wrench and M55302/190-01 guide pin and guide socket kit. When guides are removed and reinstalled in another po

19、sition, apply Loctite 83-CV or equivalent on the threads. Ordering connectors in other than the -1 polarized position may be done by the OEMs by placing the desired polarized position in brackets three spaces after the Part or Identifying Number (PIN)on the purchase order. Example: M55302/191A100Y -

20、32. Polarization pins and sockets shall be adjusted to any desired configuration by spanner wrench (M55302/57-01). Ordering connectors in the -1 polarized position without Loctite 83-CV or equivalent applied may be done by placing a “-0” in brackets three spaces after the PIN on the purchase order.

21、Guide sets, as installed, shall withstand 7 ounce-inches backoff torque applied through the guide set mounting nut. M55302/190-01 kit: Consists of one type Y ”D” shaped guide socket and one type Y “D” shaped guide pin and two spanner nuts. Provided by IHSNot for ResaleNo reproduction or networking p

22、ermitted without license from IHS-,-,-MIL-DTL-55302/191C 8 Example of Part or Identifying Number (PIN): M55302/191 A 100 X Basic number of specification sheet Type of terminals (see figure 1) A = dip terminal .109 long B = dip terminal .140 long C = dip terminal .172 long Number of contacts (see fig

23、ure 1) Type of mounting hardware (see figure 1) Type X = full round Type Y = “D” shaped Type F = fixed jackset Type S = short turning hex jackset Type N = turning hex jackset Type L = turning slotted jackset Type M = short turning slotted jackset Changes from previous issue. The margins of this spec

24、ification are marked with vertical lines to indicate where changes from the previous issue were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of

25、this document based on the entire content irrespective of the marginal notations and relationship to the last previous issue. Referenced documents. In addition to MIL-DTL-55302, this document references the following: MIL-DTL-55302/190 ASTM A581/A581M ASTM A582/A582M ASTM B196/B196M ASTM B197/B197M

26、ASTM B488 SAE-AMS-QQ-N-290 SAE-AMS-2700 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55302/191C 9 CONCLUDING MATERIAL Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force 85 DLA - CC (Project 5935-2010-148) Review activit

27、ies: Army - AR, AT, AV, CR4, MI Navy - AS, MC, OS, SH Air Force - 19, 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.daps.dla.mil . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-