1、 MIL-DTL-39030/3E 17 July 2013 SUPERSEDING MIL-DTL-39030/3D 9 April 2004 DETAIL SPECIFICATION SHEET DUMMY LOADS, ELECTRICAL, COAXIAL, TYPE I (SMA), LOW POWER This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the produc
2、t described herein shall consist of this specification sheet and MIL-DTL-39030. NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Series SMA pin contact interface in accordance with MIL-STD-348. 4. Part or Identifying Number (PIN). FIGURE 1. Dimensions and
3、configuration, PINs M39030/3-01, -02, -11, -15, -16, -17, -22, and 26 (both N and S). AMSC N/A FSC 5985 Inches mm .005 .27 .28 .312 .43 .56 .73 0.13 6.9 7.1 7.92 10.9 14.2 18.5 Dash number A max B max -01, -16 .73 .28 -02, -17 .73 .28 -11, -22 .43 .27 -15, -26 .56 .28 INCH-POUND Provided by IHSNot f
4、or ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 2 Inches mm .005 .120 .140 .25 .312 .36 .85 2.00 0.13 3.05 3.56 6.4 7.92 9.1 21.6 50.8 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Series SMA pin contact in
5、terface in accordance with MIL-STD-348. FIGURE 2. Dimensions and configuration, PINs M39030/3-03, -04, -18 and -19 (both N and S). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 3 Inches mm .005 .312 .72 0.13 7.92 18.3 NOTES: 1. Dim
6、ensions are in inches. 2. Metric equivalents are given for information only. 3. Series SMA socket contact interface in accordance with MIL-STD-348. FIGURE 3. Dimensions and configuration, PINs M39030/3-05 and -06 (both N and S). Provided by IHSNot for ResaleNo reproduction or networking permitted wi
7、thout license from IHS-,-,-MIL-DTL-39030/3E 4 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Series SMA socket contact interface in accordance with MIL-STD-348. FIGURE 4. Dimensions and configuration, PINs M39030/3-07 and -08 (both N and S). Inches mm .0
8、05 .120 .140 .25 .312 .80 2.00 0.13 3.05 3.56 6.4 7.92 20.3 50.8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 5 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Series SMA pin contact in
9、terface in accordance with MIL-STD-348. FIGURE 5. Dimensions and configuration, PINs M39030/3-09, -10, -12, -14, -20, -21, -23, and -25 (both N and S). Dash number A max -09, -20 .84 -10, -21 .55 -12, -23 .55 -14, -25 .55 Inches mm .005 .01 .26 .312 .33 .55 .84 0.13 0.3 6.6 7.92 8.4 14.0 21.3 Provid
10、ed by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 6 Inches mm .005 .01 .130 .25 .26 .312 .33 .61 2.00 0.13 0.3 3.30 6.4 6.6 7.92 8.4 15.5 50.8 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Serie
11、s SMA pin contact interface in accordance with MIL-STD-348. FIGURE 6. Dimensions and configuration, PINs M39030/3-13 and -24 (both N and S). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 7 TABLE I. Dash numbers and characteristics.
12、 Dash number both N and S Operating frequency (GHz) VSWR (max) Power handling capability (max) Nominal characteristic impedance (ohms) Weight (max) (oz) Finish Figure numbers Average (watts) Peak 1/ (watts) 01, 16 6/ DC to 18 (1.05 +.010f ):1 2/.5 3/ 50 3/ 50 0.25 4/ 1 02, 17 6/ DC to 18 (1.05 +.010
13、f ):1 2/ .5 3/ 50 3/ 50 0.25 5/ 1 03, 18 6/ DC to 18 (1.05 +.010f ):1 2/ .5 3/ 50 3/ 50 0.25 4/ 2 04, 19 6/ DC to 18 (1.05 +.010f ):1 2/ .5 3/ 50 3/ 50 0.25 5/ 2 05 DC to 18 (1.05 +.010f ):1 2/ .5 3/ 50 3/ 50 0.25 4/ 3 06 DC to 18 (1.05 +.010f ):1 2/ .5 3/ 50 3/ 50 0.25 5/ 3 07 DC to 18 (1.05 +.010f
14、 ):1 2/ .5 3/ 50 3/ 50 0.25 4/ 4 08 DC to 18 (1.05 +.010f ):1 2/ .5 3/ 50 3/ 50 0.25 5/ 4 09, 20 6/ DC to 10 1.10:1 1.0 100 50 0.25 4/ 5 10, 21 6/ DC to 10 2.10:1 2.0 200 95 0.25 4/ 5 11, 22 6/ DC to 18 1.15:1 1.0 100 50 0.25 4/ 1 12, 23 6/ 2 to 19 1.30:1 1.0 100 50 0.25 4/ 5 13, 24 6/ 2 to 19 1.30:
15、1 .5 50 50 0.25 4/ 6 14, 25 6/ 2 to 19 1.30:1 1.0 100 75 0.40 4/ 5 15, 26 6/ 4.4 to 5.0 (1.025 +.005f ):1 2/ .5 50 50 0.25 4/ 1 1/ Peak power is specified with a 1 percent duty cycle. 2/ “f” is the frequency in GHz. 3/ Power input is derated linearly from 100 percent at +25C to 25 percent at specifi
16、ed maximum ambient operating temperature. 4/ Gold plated in accordance with ASTM B488, type II, grade C, class 1.27, over copper flash. 5/ Passivated in accordance with ASTM A967 or SAE-AMS2700. 6/ Furnished with safety wire holes (for high vibration areas). Three holes .016-inch (0.41 mm) minimum d
17、iameter, equally spaced, are required for safety wiring after mating. Location on coupling nut is optional. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 8 REQUIREMENTS: Dimensions and configurations: See figures 1 thru 6. Electric
18、al characteristics: See table I. Materials: Body and connector: Corrosion-resistant steel in accordance with SAE-AMS-QQ-S-763 or ASTM A484/A484M and ASTM A582/A852M. Finish: See table I. Contact pin and contact socket: Beryllium copper in accordance with ASTM B194, ASTM B196/B196M, or ASTM B197/B197
19、M. Finish: The male pin shall be plated to a minimum gold thickness of 50 micro inches (1.27m) in accordance with ASTM B488, type ll, code C, class 1.27, over 50 micro inches (1.27 m) minimum of nickel in accordance with SAE-AMS-QQ-N-290, class 1, measured anywhere along the mating surface, for all
20、series. The socket contact shall be plated to a minimum of 50 micro inches (1.27m) of gold in accordance with ASTM B488, type ll, code C, class 1.27, over 50 micro inches (1.27 m) minimum of nickel in accordance with SAE-AMS-QQ-N-290, class 1, including the I.D., measured at a depth of .040 inch min
21、imum. The plating on non-significant surfaces in the I.D. shall be of sufficient thickness to ensure plating continuity and uniform utility and protection. This plating may consist of an underplate only. A silver underplate shall not be permitted. Bead chain and lug: Corrosion-resistant steel or pla
22、stic. Weight: See table I. Ambient temperature range: Operating: Dash numbers 01 thru 08, 11, 15, 16 thru 19, 22 and 26: -55C to +125C. Dash numbers 09, 10, 12, 13, 14, 20, 21, 23, 24 and 25: -65C to +125C. Nonoperating (storage): -65C to +165C. Connector tests: The following tests shall, be perform
23、ed after visual and mechanical examination in the qualification inspection. Force to engage and disengage: Torque 2 inch-pounds, maximum. Coupling proof torque (for plug male type only): 15 inch-pounds, minimum. Threaded coupling connector: For each test of threaded coupling connector where the test
24、 is performed on mated pairs, the pairs shall be torque to 7 to 10 inch-pounds. Connector durability: 500 cycles at 12 cycles per minute, maximum. After this test, the connector shall meet the engage and disengage requirement. Vibration: Method 204 of MIL-STD-202, test condition D. Shock: Method 213
25、 of MIL-STD-202, test condition I. Barometric pressure: Method 105 of MIL-STD-202, test condition C. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-39030/3E 9 PIN: M39030/3-(dash number from table I) (S = screened or N = not screened). Margi
26、nal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes. In addition to MIL-DTL-39030, this specification sheet references the following documents: ASTM A484/A484M MIL-STD-202 ASTM A582/A582M MIL-STD-348 ASTM A967 SAE-AMS-QQ
27、-N-290 ASTM B194 SAE-AMS2700 ASTM B196/B196M SAE-AMS-QQ-S-763 ASTM B197/B197M ASTM B488 CONCLUDING MATERIAL Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force - 85 (Project 5985-2013-024) DLA - CC Review activities: Army - AV, MI Navy - AS, OS, SH Air Force - 19 NOTE: The activit
28、ies 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-,-,-
