DLA MIL-PRF-1 111 G-2013 ELECTRON TUBE THYRATRON TYPE 6130.pdf

1、 MIL-PRF-1/111G 29 May 2013 SUPERSEDING MIL-PRF-1/111F 19 December 2002 PERFORMANCE SPECIFICATION SHEET ELECTRON TUBE, THYRATRON TYPE 6130 This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the electron tube described h

2、erein shall consist of this document and the latest issue of MIL-PRF-1. DESCRIPTION: Triode, hydrogen See figure 1 Mounting position: Any Weight: 3-ounces (85 grams) nominal ABSOLUTE RATINGS: Parameter: Ef epy epx Ebb Ec egx egy ib Unit: V ac kv kv V dc V dc v v a Maximum: 6.6 3.0 3.0 - - 200 - 35 M

3、inimum: 5.7 - (Note 1) - (Note 2) 800 - - - (Note 3) - Test conditions: 6.3 3.0 - - 0 - 130 - ABSOLUTE RATINGS: Parameter: Ib tk dik/dt Pb TA prr Barometric pressure, reduced Unit: mA dc sec a/s - C pps mm Hg Maximum: 45 - 750 0.3 x 109 90 - 87.0 Minimum: - 120 - - -50 - - Test conditions: - 120 - -

4、 - 2,800 - GENERAL: Qualification Not required This specification sheet uses accept on zero defect sampling in accordance with MIL-PRF-1, table III. AMSC N/A FSC 5960 INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/111G 2 TABLE I

5、. Group A inspection. Inspection MIL-STD-1311 Method Note Conditions Symbol Limits Unit Min Max Conformance inspection, part 1 Heater current Instantaneous starting DC anode voltage for conduction Operation (1) Pulse emission (method A) 3241 3267 3247 3246 3251 - 5, 7 8 5, 9, 10 - epy = 3,000 v (min

6、) epy = 4,000 v (min) ik = 35 a (min) prr = 60 10% tp = 5.0 s 10% tr = 0.5 s (max); specified time interval = 2.5 s If - Ebb egy egk 2.0 - - - - 2.5 - 300 130 150 Aac - Vdc v v Conformance inspection, part 2 Shock, Specified Pulse Anode delay time Anode delay time drift Time jitter Operation (2) 104

7、2 3256 3256 3261 3246 - 5, 9 11 5 5, 6 Operation (1); t = 120 seconds Anode delay time epy = 1,500 v (max) t = 5.0 minutes - tad tad tj egy - - - - - - 0.6 0.15 0.02 130 - s s s v Conformance inspection, part 3 Life test Life-test end points: Operation (1) DC anode voltage for conduction Time jitter

8、 Low-frequency vibration High-frequency vibration Operation at elevated temperature Operation (3) 3246 3247 3261 1031 1031 3246 3246 5 - - - 4, 12 4, 12 5, 12 5, 6, 12 Group B; t = 500 hours; t = 96 hours “on“ and one hour “off“ (tube mounted horizontally) No voltages; F = 12 to 50 Hz t = 30 seconds

9、 (min) t = 5.0 hours; TA = 90C t = 5.0 hours - egy Ebb tj - - egy egy - - - - - - - - - 140 750 0.04 - - 130 130 - v V dc s - - v v See footnotes at end of table. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/111G 3 NOTES: 1/ For instanta

10、neous starting applications where anode voltage is applied instantaneously, the power supply filter design shall be such that the maximum permissible epy is 3,000 v and shall not be attained in less than 0.04 second. 2/ In pulsed operation, the peak inverse voltage, exclusive of a spike of 0.05 s ma

11、ximum duration, shall not exceed 1,500 volts during the first 25 s after the pulse. 3/ Driver pulse, measured at tube socket with thyratron grid disconnected; egy = 175 v (min), time of rise = 0.5 s (max), grid pulse duration = 2.0 s (min). Impedance of drive circuits = 1,500 ohms (max). 4/ There sh

12、all be no pronounced resonance in the specified range. 5/ The circuit constants shall be chosen so that at epy = 3.0 kv under resonant charging conditions, dik/dt = 750 a s (min), ib = 35 a, tp = 0.5 s 10 percent, prr = 3,000. The grid pulse characteristics shall be tp = 2.0 s (max), tr = 0.5 s (min

13、), driver impedance = 1,500 ohms (min). 6/ The tube shall operate satisfactorily in an evacuated chamber in which the pressure does not exceed 70 mmHg. 7/ The tube shall operate satisfactorily on push button starting within three attempts when the anode voltage epy is applied to the tube under test

14、in such a manner as to rise from 0 to 3,000 v within 0.03 second. The filter in the rectifier shall be designed so that epy reaches at least 1,500 v within 0.015 second. 8/ This test shall be conducted within 60 seconds after the operation (1) test. 9/ The tube shall operate continuously for 5 minut

15、es without evidence of arc-back or anode heating. 10/ This test is to be the first test performed at the conclusion of the holding period. 11/ During the interval between 2 minutes and 7 minutes of the anode delay time test, the change in anode delay time (tad) relative to the tad value observed on

16、the anode delay time test shall not exceed the specified value. 12/ This test shall be performed according to the life testing schedule given in MIL-PRF-1 paragraph 4.3.8. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/111G 4 FIGURE 1. Out

17、line drawing of electron tube type 6130. Pin connections Pin No. Element 1 2 3 4 cap h k g h, k a Dimensions Ltr Minimum Maximum Inches mm Inches mm Conformance inspection, part 2 A - - 5.188 131.78 B - - 1.563 39.70 C 4.188 106.38 4.563 115.90 Conformance inspection, part 3 (see note) D - - 1.469 (

18、37.31) E Cap: C1-1 (EIA) F Base: A4-9 (EIA) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/111G 5 Referenced documents. In addition to MIL-PRF-1, this specification sheet references MIL-STD-1311. The margins of this specification are marke

19、d 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 this document based

20、 on the entire content irrespective of the marginal notations and relationship to the last previous issue. Custodians: Preparing activity: Army - CR DLA - CC Navy - EC Air Force - 85 (Project 5960-2013-009) DLA - CC Review activities: Army - AR Navy - AS, CG, MC, OS, SH Air Force - 99 NOTE: The acti

21、vities 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-,-,-