DLA MIL-DTL-55041 10 B-2010 SWITCH WAVEGUIDE ELECTROMECHANICAL LATCHING FREQUENCY RANGE 8 6 TO 10 3 GHz.pdf

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1、AMSC N/A FSC 5985 MIL-DTL-55041/10B 27 July 2010 SUPERSEDING MIL-DTL-55041/10A 2 February 2000 DETAIL SPECIFICATION SHEET SWITCH, WAVEGUIDE, ELECTROMECHANICAL, LATCHING, FREQUENCY RANGE 8.6 TO 10.3 GHz This specification is approved for use by all Departments and Agencies of the Department of Defens

2、e. The requirements for acquiring the switch described herein shall consist of this specification sheet and MIL-DTL-55041. FIGURE 1. Switch configuration and schematic, PIN M55041/10-001. INCH-POUND Dimensions Ltr Inches MillimetersMin Max Min MaxA .53 .83 13.46 21.08B 2.22 square 2.58 square 56.39

3、square 65.53square C 4.50 5.50 114.30 139.70D 2.43 2.60 61.72 66.04E - 1.250 - 31.75F - 2.000 - 50.80G - 1.000 - 25.40H - 1.000 - 25.40J - 1.750 - 44.45K .190-32 UNF-2BHole depth .370 Min 4.83-32 UNF-2BHole depth 9.40 Min L 1.794 1.806 45.57 45.87M - 2.62 square - 66.55square N .164-32 UNC-2BFull th

4、read depth .370 Min 4.17-32 UNC-2BFull thread depth 9.40 Min Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55041/10B 2 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for general information only and are based upon 1.00

5、inch = 25.4 mm. 3. Unless otherwise specified, tolerances are .02 (0.5 mm) for two place decimals and .005 (0.13 mm) for three place decimals. 4. Rotor sequence: When the circuit A-E is energized, the RF energy path is from port A to C. When circuit B-E is energized, the RF energy path is from port

6、A to B. 5. Interlock switch operation sequence: When circuit A-E is energized, the circuit C-D must open prior to circuit F-D being closed. When circuit B-E is energized, circuit F-D must open prior to circuit C-D being closed. All normally closed contacts and normally open contacts must open and cl

7、ose respectively within or before the first .03 inch (0.8 mm) of rotor travel and within or after the last .03 inch (0.8 mm) of rotor travel. The rotor shall come to a stop in its end position without visible bounce and shall not operate the interlock switch during such an oscillation. 6. Drive asse

8、mbly operation: The switch shall not require any holding current. The drive assembly shall be automatically deenergized when the rotor is latched. The direction of drive assembly moving the rotor shall be as specified in the pictorial view. Case 1: After circuit A-E is energized, if the actuation vo

9、ltage is removed from it and the rotor is stopped at some point after its first .03 inch (0.8 mm) of travel and before its last .03 inch (0.8 mm) of travel, the rotor shall continue to its new position (open energy path from port A to port C) by reapplying voltage to circuit A-E. However, the rotor

10、shall return to its original position (open energy path from port A to port B) if the reapplied voltage is applied to circuit B-E. Case 2: After circuit B-E is energized, if the actuation voltage is removed from it and the rotor is stopped at some .03 inch (0.8 mm) of travel, the rotor shall continu

11、e to its new position (open energy path from port A to port B) by reapplying voltage to circuit B-E. However, the rotor shall return to its original position (open energy path from port A to port C) if the reapplied voltage is applied to circuit A-E. 7. Helical thread inserts may be used. 8. The sha

12、pe of the can is optional. FIGURE 1. Switch configuration and schematic, PIN M55041/10-001 - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55041/10B 3 REQUIREMENTS: Dimensions and configuration: See figure 1. Exterior surface: Bl

13、ack finish in accordance with MIL-DTL-14072. Weight: 2.5 pounds (1.13 kg), maximum. Operation: 1P2T latching, break before make. Rotor operation: See figure 1, note 4. Connector: The power connector shall mate with connector MS3116E10-6S. Drive assembly operation: See figure 1, note 6. Drive assembl

14、y operating voltage: 21 V dc to 29 V dc. Drive assembly starting current: 4 amperes, maximum, at 27 V dc. RF power handling capability: Peak 400 kW, average 400 W. Temperature altitude: The temperature altitude must be as recommended for class 2 equipment designed for 21.28 Km (70,000 feet) altitude

15、 and continuous sea level operation over the temperature range of -62C to +90C (+95 C intermittent operation). Frequency range: 8.6 GHz to 10.3 GHz. Isolation: 80 dB, minimum. VSWR: 1.1:1, maximum. Insertion loss: 0.10 dB, maximum. Switching time (see figure 2): 1 second, maximum, 21 V dc at 20C 10C

16、; 2 seconds, maximum, 21 V dc at -54C 5C. Pressure: With 30 lbf/in2(gage) applied, the pressure drop shall not exceed 5 lbf/in2(gage) in 1 hour. Pressure equilibrium: 1 lbf/in2, tested as follows: a. Seal one active (open) waveguide port by means of an O-ring and flat plate and attach a compressed a

17、ir (15 lbf/in2(gage) input to the other active (open) waveguide port. b. Adjust flow rate of compressed air to 100 cubic inches per minute. c. Measure the pressure differential between the air input port to which the compressed air is attached and the inactive (closed) waveguide port. The pressure d

18、ifferential shall not exceed the value specified. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55041/10B 4 Interlock switching current: 5 amperes, maximum, at 27 V dc; 2 amperes, maximum, at 24 V dc. Cycle life: 50,000 cycles; rate of cycl

19、ing shall be 10 per minute, maximum. Part or Identifying Number (PIN): M55041/10-001. Material: Lubricants shall comply, as a minimum, to the requirements of MIL-PRF-83261. The test set-ups specified in Figures 2, 3, and 4 of MIL-DTL-55041 may be modified to reflect current industry practice. Explos

20、ion: Applicable. The test need not be done with full RF power applied if the switch is designed so that the switching mechanism is completely isolated from the RF energy path. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55041/10B 5 FIGURE

21、 2. Switching time. NOTE: Switching time: The switch shall be mounted in the position shown; the long axis of the switch shall be vertical. The switching time shall be taken and recorded. The switch shall be rotated in 45 increments and switching time recorded at each position through 360. The switc

22、hing time shall not vary more than 10 percent from the time recorded at 0 (the original position). NOTE: The switch covered by this specification sheet is NSN 5985-01-040-4182 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-55041/10B 6 Refere

23、nced documents: In addition to MIL-DTL-55041, this document references the following: MIL-PRF-83261 MIL-DTL-14072 The margins of this specification 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 assum

24、es no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous issue. Custodians: Preparing activity: Air

25、Force - 85 DLA - CC DLA - CC (Project 5985-2010-009) Review activity 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.daps.dla.mil/. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-