DLA MIL-PRF-1 296 E-2009 ELECTRON TUBE REFERENCE CAVITY TYPES 1Q22 1Q23 1Q24 5846 6040 6041.pdf

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1、AMSC N/A FSC 5960 INCH POUND MIL-PRF-1/296E 1 October 2009 SUPERSEDING MIL-PRF-1/296D 29 JUNE 1998 PERFORMANCE SPECIFICATION SHEET ELECTRON TUBE REFERENCE CAVITY TYPES 1Q22, 1Q23, 1Q24, 5846, 6040, 6041 The requirements for acquiring the electron tube described herein shall consist of this document

2、and the latest issue of MIL-PRF-1. This specification is mandatory for use by all Depart- ments and Agencies of the Department of Defense. DESCRIPTION: Reference cavity stabilizer, X-Band, Waveguide mounted. ABSOLUTE RATINGS: Resonant frequency (MHz) 1Q22 1Q23 1Q24 5846 6040 6041 Altitude Minimum: 9

3、249.5 9279.5 9309.5 9279.5 9307.5 9311.3 - - - Maximum: 9250.5 9280.5 9310.5 9280.5 9308.5 9312.5 50,000 ft. PHYSICAL CHARACTERISTICS: Dimensions: See outline drawing. Weight: 8 ounces (approximately). Mounting Position: Any. TEST CONDITIONS: See note 1. _ GENERAL: Qualification: Required. Provided

4、by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/296E 2TABLE I. Testing and inspection. Inspection Method MIL-STD-1311 Conditions Symbols Limits Min Limits Max Unit Conformance inspection, part 1 Insertion loss Loaded Q Temperature cycle (1) RF glow

5、test - - - - - - - - - - - - At resonant frequenciesT = 40C to 100C t = 30 minutes see note 3 see note 5 Li QL 1Q22Fo 1Q23Fo 1Q24Fo 5846Fo 6040Fo 6041Fo - - - 4.0 1,900 9249.7 9279.7 9309.7 9279.7 9307.7 9311.7 - - - 6.0 2,400 9250.3 9280.3 9310.3 9280.3 9308.3 9312.3 - - - dB - - - MHz MHz MHz MHz

6、MHz MHz - - - Conformance inspection, part 2 Vibration Shock Temperature cycle (2) Temperature compensation (1) Off resonance insertion loss Pressurizing 1031 1042B - - - - - - - - - 4003 10 G see note 2 50 G, 6 ms half-sine T = 40C to 100C t = 12 hours see note 3 Room temperature to 100C, see note

7、4 F = 9,800 100 MHz F = 8,850 100 MHz 45 Psi absolute see note 8 Fo Fo 1Q22Fo 1Q23Fo 1Q24Fo 5846Fo 6040Fo 6041Fo Fo Li Li - - - - - - - - - 9249.7 9279.7 9309.7 9279.7 9307.7 9311.7 - - - 30 30 - - - .15 .15 9250.3 9280.3 9310.3 9280.3 9308.3 9312.3 10.0 - - - - - - - - - MHz MHz MHz MHz MHz MHz MHz

8、 MHz MHz dB dB - - - Conformance inspection, part 3 Life test Life test end points - - - - - - Group B, t = 30 minutesT = 55C to 100C see note 6 Cycles 25 - - - - - - See footnotes at end of table I. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MI

9、L-PRF-1/296E 3TABLE I. Testing and inspection - Continued. Inspection Method MIL-STD-1311 Conditions Symbols Limits Min Limits Max Units Conformance inspection, part 3 -Continued RF glow test Resonant frequency Qualification Temperature cycle (3) Temperature compensation (2) Atmospheric pressure tes

10、t - - - - - - - - - - - - - - - - - - see note 5 T = 55C to 100C t = 30 minutes see note 3 Room temperature to 0C Room temperature to -25C Room temperature to -40C Room temperature to -55C see notes 4 and 7 P = Atmospheric to 45 psi P = Atmospheric to 5 in. Hg - - - 1Q22Fo 1Q23Fo 1Q24Fo 5846Fo 6040F

11、o 6041Fo 1Q22Fo 1Q23Fo 1Q24Fo 5846Fo 6040Fo 6041Fo Fo Fo Fo Fo Fo Fo - - - 9249.5 9279.5 9309.5 9279.6 9307.5 9311.5 9249.7 9279.7 9309.7 9279.7 9307.7 9311.7 - - - - - - - - - - - - - - - - - - - - - 9250.5 9280.5 9310.5 9280.4 9308.5 9312.5 9250.3 9280.3 9310.3 9280.3 9308.3 9312.3 0.3 0.7 1.0 1.2

12、 0.15 0.15 - - - MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz NOTES: 1. Electrical measurements are to be made with a standard frequency source having an absolute accuracy of the order of 1 part in 500,000. The cavities shall be tested mounted between UG-40/U chokes in RG-

13、52/U waveguide and with a voltage standing wave ratio less than 1.05 due to resistive match looking into each of the chokes between which the cavity is mounted. 2. The difference in resonant frequency before and after vibration shall not exceed the limits specified. 3. The cavity shall be subjected

14、to three complete cycles between the specified temperature extremes. The cavity may be allowed to come to equilibrium at room temperature in passing from one extreme to the other. The cavity shall be maintained at the extreme temperatures for the specified time during each cycle. When the tube has c

15、ome to equilibrium at room temperature at the conclusion of the last two half cycles, the resonant frequency shall be measured and shall be within the specified limits. 4. After temperature cycling described in note 3, the cavity shall be brought to equilibrium at the specified extreme temperature f

16、or 30 minutes and then returned to equilibrium at room temperature. Then it shall be brought to the specified extreme temperature again and allowed to return to room temperature. Resonant frequency measurements shall be made at approximately 20C temperature intervals while returning to room temperat

17、ure. At no temperature shall the resonant frequency differ from the value at room temperature by more than the specified amount. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/296E 4NOTES: Table I. - Continued. 5. The tube shall show a typ

18、ical diffuse low-pressure glow discharge when placed in an rf field. 6. The cavity may be allowed to come to equilibrium at room temperature in passing from one extreme to the other. The cavity shall be maintained at the extreme temperature for the specified time during each cycle. When the tube has

19、 come to equilibrium at room temperature, at the conclusion of the last two half cycles, the resonant frequency shall be measured and shall be within the specified limits. 7. Fo at -55C may be obtained by extrapolation of the data obtained at higher temperatures. 8. This test is not applicable to ty

20、pe 5846. 9. This specification sheet uses accept on zero defect sampling in accordance with MIL-PRF-1, table III. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/296E 5Dimensions Inches Millimeters Ltr Min Max Min Max Conformance inspection

21、, part 1 J 1.744 1.756 44.30 44.60 M 1.218 Nom 30.94 Nom P 0.061 0.065 1.55 1.65 Q 0.400 0.402 10.16 10.21 Conformance inspection, part 2 A - - - 2.187 - - - 55.55 B 0.608 0.612 15.44 15.54 C - - - 1.375 34. 34.93 These Dimensions apply to 5846 only. Dimensions Inches Millimeters Ltr Min Max Min Max

22、 D 0.859 0.891 21.82 22.63 E 1.000 REF 25.4 REF G 0.638 0.642 16.21 16.31 H - - - 0.828 - - - 21.03 K - - - 0.875 - - - 22.23 L 0.609 Nom 15.47 Nom N 0.020 0.030 0.51 0.76 R 0.028 0.030 0.71 0.76 S 8-32 UNC-28 THD FIGURE 1. Outline drawing of tube types 1Q22, 1Q23, 1Q24, 5846, 6040, and 6041. Provid

23、ed by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/296E 6Referenced documents. In addition to MIL-PRF-1, this document references the following: MIL-STD-1311 Marginal notations are not used in this revision to identify changes with respect to the pr

24、evious issue due to the extent of the changes. Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force - 85 (Project 5960-2009-006) DLA- CC Review activities: Army AR Navy - SH 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-,-,-