DLA MIL-PRF-1 609 G-2009 ELECTRON TUBE GAS SWITCHING TYPE 1B24A.pdf

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1、 INCH-POUND MIL-PRF-1/609G 30 September 2009SUPERSEDING MIL-PRF-1/609F 31 March 1999 PERFORMANCE SPECIFICATION SHEET ELECTRON TUBE, GAS SWITCHING TYPE 1B24A This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the electro

2、n tube described herein shall consist of this document and the latest issue of MIL-PRF-1. DESCRIPTION: TR, tunable, internal cavity, incident power 30 kw, frequency range 8,490 to 9,600 MHz. ABSOLUTE RATINGS: Parameter: Incident power Ii Ebb Alt Unit: kw A dc V dc ft Maximum: 30 200 -1,000 10,000 Mi

3、nimum: - - - 100 -750 - - - PHYSICAL CHARACTERISTICS: Dimensions: See figure 1. TEST CONDITIONS: Parameter: Incident power Ii tp prr Ebb Ri Frequency Unit: kw A dc s pps V dc Meg F MHz Test condition 1: 10 100 0.5 1,000 - - - - - - F1 8,490 0.1% Test condition 2: 30 - - - 1.0 1,000 -800 2.3 F2 8,600

4、 0.1% F3 9,000 0.1% F4 9,375 0.1% F5 9,375 0.2% F6 9,375 0.5% F7 9,500 0.1% F8 9,600 0.1% GENERAL: Qualification - Required. AMSC N/A FSC 5960 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/609G 2 TABLE I. Testing and inspection. Requireme

5、nt or test Method MIL-STD-1311 Notes Test Conditions Symbol Limits Min Limits Max Units Qualification Insertion loss (integral cavity) Loaded Q Temperature coefficient of frequency 4416 4461 4466 2 2 3 - - - - - - - - - F = F2 to F7 F = F2 to F7 F = F4 Li QL F - - - 160 - - - 2.0 350 -20 dB - - - MH

6、z Conformance inspection, part 1 Ignitor ignition time Ignitor voltage drop Insertion loss (integral cavity) Ignitor interaction (insertion loss) Tuning range Flat leakage power Temperature cycling (nonoperating) 4401 4406 4416 4421 4426 4452 1027 1 - - - - - - - - - - - - - - - - - - - - - - - - -

7、- - - - - - - - - - - - - - 1 - - - Ebb = -800 V dc; Ri = 2.3 Meg 1 percent Ii = 100 A dc F = F1 Ii = 100 A dc 5 turns F = F6; T = 25C 5C t Eid Li Li F pf - - - - - - 325 - - - - - - 8,490 - - - - - - 5.0 450 2.0 0.2 9,600 30 - - - sec V dc dB dB MHz mw - - - Conformance inspection, part 2 Dielectri

8、c material strain Degradation due to vibration Ignitor oscillation Insertion loss (integral cavity) Loaded Q Recovery time Vibration detuning 4101 4021 4411 4416 4461 4471 4016 - - - - - - - - - - - - - - - - - - 4 - - - - - - - - - - - - - - - 1 - - - F = F3, F4 and F8 F = F1 and F8 F = F4 2G; F =

9、F4; t = 12 hours - - - - - - Ii Li QL t F - - - - - - - - - - - - 160 - - - - - - - - - - - - 60 2.0 350 4.0 3 - - - - - - A dc dB - - - s MHz See footnotes at end of table. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/609G 3 TABLE I. Te

10、sting and inspection -Continued. Requirement or test Method MIL-STD-1311 Notes Test Conditions Symbol Limits Min Limits Max Units Conformance inspection, part 3 Life test Life-test end points: Flat leakage power Insertion loss (integral cavity) Ignitor interaction (insertion loss) Ignitor voltage dr

11、op Degradation due to vibration Recovery time Temperature cycling life test - - - - - - 4452 4416 4421 4406 4021 4471 1027 5 6 - - - - - - - - - - - - - - - - - - - - - 2 - - - 1 - - - - - - - - - - - - 1 - - - Group B; F = F5 F = F6; T = 25 5 C F = F4 Ii = 100 A dc Ii = 100 A dc F = F4 Group B t -

12、- - pf Li Li Eid - - - t Cycles500 - - - - - - - - - - - - - - - - - - - - - 10 - - - - - - 30 2.0 0.5 650 - - - 6 - - - hrs - - - mw dB dB V dc - - - s - - - NOTES: 1. This specification sheet uses accept on zero defect sampling plan in accordance with MIL-PRF-1, table III. 2. This test shall be pe

13、rformed at intervals of 100 MHz. 3. The frequency drift shall be measured with no adjustment of the tuning mechanism. 4. The tube shall be tuned to the specified frequency and then vibrated in the direction of ignitor axis. At the conclusion of this test, the tube shall satisfy all electrical tests

14、of this specification. 5. The ignitor current shall not be adjusted during life test. 6. Life-test end points shall be measured by using a fixed voltage and resistor. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/609G 4 NOTES: 1. Exhaust

15、tubulation shall not extend beyond periphery. 2. Applies to area between periphery of this section of tube and concentric circle of 5/16 radius. 3. No part of iris assembly shall extend beyond body surface. 4. Reservoir shall be glass, or approved equivalent. 5. Maximum projection of reservoir shall

16、 lie within a cylinder of 1.250 diameter with axis colinear with tube axis. 6. A force of 200 pounds shall be applied to the face of the tube within the area indicated by shading. Dimension M shall not be permanently changed by more than 0.001. Qualification inspection required. 7. Body faces shall

17、be cadmium plated 0.0003 minimum, or shall be made entirely of monel, bright nickel or equivalent. If nickel Is required, it is recommended that it be used only when other metals can not meet the performance requirements. 8. Solder fillets permissible on peripheral surface near exhaust tubulation an

18、d electrode terminal. Slots shall be free from solder. FIGURE 1. Outline drawing of electron type 1B24A. Dimensions Ltr Inches Millimeter Min Max Min Max Qualification inspection C 2.875 73.03 E 1.275 1.285 32.39 32.64 F 1.215 1.225 30.86 31.12 L CAP: C1-2 (EIA) Conformance inspection, part 1 (see n

19、ote 1) G .031 .063 0.79 1.60 K .637 .643 16.18 16.33 M .609 .615 15.47 15.62 Q .607 .613 15.42 15.57 R .086 .094 2.18 2.39 Conformance inspection, part 2 A 3.250 82.55 B 1.760 44.70 D 1.422 36.12 H .527 .533 13.39 13.54 J .938 23.83 N 1.188 30.18 Reference dimension P .563 Flat 14.30 Flat Provided b

20、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/609G 5 Referenced documents. In addition to MIL-PRF-1, this document references the following: MIL-STD-1311 The margins of this specification are marked with vertical lines to indicate where changes fro

21、m 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 this document based on the entire content irrespective of the marginal

22、 notations and relationship to the last previous issue. Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force - 85 (Project 5960-2009-036) DLA - CC Review activities: Army - MI Navy - AS, CG, MC, OS Air Force - 19, 99 NOTE: The activities listed above were interested in this documen

23、t 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-,-,-