DLA MIL-PRF-1 825 E-2008 ELECTRON TUBE RECEIVING TYPE 5651WA.pdf

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1、 AMSC N/A FSC 5960 MIL-PRF-1/825E 16 October 2008 SUPERSEDINGMIL-E-1/825D 14 January 1972 PERFORMANCE SPECIFICATION SHEET ELECTRON TUBE, RECEIVING TYPE 5651WA The requirements for acquiring the electron tube described herein shall consist of this document and MIL-PRF-1. This specification is mandato

2、ry for use by all Depart- ments and Agencies of the Department of Defense. DESCRIPTION: Diode, miniature, voltage reference. Outline - 5-2 (EIA). Base - E7-1. Envelope - T5-1/2. Cathode - Glow discharge. Base connections: ABSOLUTE-MAXIMUM RATINGS: Parameter: Total darkness ionization voltage Ambient

3、 light ionization voltage Operating voltage Operating current TE TA Alt Unit: V dc V dc V dc mA dc C C ft Maximum: - - 90 (approx) 3.5 +155 +150 Note 2 Minimum: 115 115 82 1.5 - -55 - TEST CONDITIONS: - - - - - 255 - GENERAL: Qualification Not Required. Reliable tube. INCH-POUND Pin No. - 1 2 3 4 5

4、6 7 Element - a k Note 1 k a Note 1 k Inactive for new design after 30 April 1997. Provided by IHSNot for Resale-,-,-MIL-PRF-1/825E 2 TABLE I. Testing and inspection. Limits MIL-STD- 1311 Method Requirement or test Notes Conditions Acceptance level Symbol Min Max UNIT 3347 3337 3337 3337 3335 3345 1

5、201 Conformance inspection, part 1 Ionization voltage (1) Voltage drop (1) Voltage drop (2) Voltage drop (3) Regulation Voltage jump Short and discontinuity detection - - - - - 3 - Ebb/Ib = 1.5 to 3.5 mAdc; illumination = 5 to 50 ft candles Ebb/Ib = 3.5 mAdc Ebb/Ib = 1.5 mAdc Ebb/Ib = 2.5 mAdc Etd(1

6、) minus Etd(2) 0.4 0.4 0.4 0.4 0.4 0.4 0.4 Ez Etd Etd Etd Reg Jump - - 82.0 82.0 83.5 - - - 110 88.0 88.0 86.5 2.0 5.0 - Vdc Vdc Vdc Vdc Vdc mVdc - 3278 3347 3305 - 1031 1041 1031 - 3347 3337 3337 3335 1121 2126 1105 Conformance inspection, part 2 Noise Ionization voltage (2) Leakage current Voltage

7、 repeatability Low-frequency vibration Shock Vibration fatigue Post-shock and vibration fatigue test end points: Ionization voltage (1) Voltage drop (1) Voltage drop (2) Regulation Base strain Glass strain Permanence of marking - 4 - 5 - - 6 - - - - - - - Ebb/Ib = 3.5 mAdc Eb = 50 Vdc; Rp = 3,000 oh

8、ms Ebb/Ib = 2.5 mAdc F = 40 Hz; 15 G; Rp = 10,000 ohms; Ebb/Ib = 2.5 mAdc 450 G 2.5 G; fixed frequency; F = 25Hz (min), 60 Hz (max) 1.0 6.5 6.5 6.5 6.5 - 6.5 - - - - - 2.5 - Eb Ez LIb Etd Ep - - Ez Etd Etd Reg - - - - - - - - - - - 82 82 - - - - 5.0 115 5 100 5.0 - - 115 90 90 3.0 - - - mVac Vdc Adc

9、 mVdc mVac - - Vdc Vdc Vdc Vdc - - - See notes at end of table. Provided by IHSNot for Resale-,-,-MIL-PRF-1/825E 3 TABLE I. Testing and inspection - Continued. Allowable defectives per characteristic Limits MIL-STD- 1311 method Requirement or test Notes Conditions AcceptanceLevel 8/ First sample Com

10、bined samples Symbol Min MaxUnit 1516 - - 1521 - - - 1501 - - 3335 3337 3337 3337 3347 - - - - 3335 3337 3337 3337 3347 - Conformance inspection, part 3 Stability life Stability life-test end point: Change in voltage drop (3) of individual tubes Survival-rate life Survival-rate-life test end points

11、(100 hours): Inoperatives Change in voltage drop (3) of individual tubes Intermittent life Intermittent life-test end points (500 hrs) Inoperatives Regulation Voltage drop (1) Voltage drop (2) Voltage drop (3) Ionization voltage (1) Change in voltage drop (3) of individual tubes Total defectives Int

12、ermittent life-test end points (1,000hrs) Inoperatives Regulation Voltage drop (1) Voltage drop (2) Voltage drop (3) Ionization voltage (1) Total defectives - - - - - - 7 - - - - - - - - - - - Ebb/Ib = 2.5mA dc; TA = room Stability life-test conditions Stability life-test conditions, or equivalent;

13、TA=150C (min) - 2.5 - - 2.5 - - - - - - - - - - - - - - - - - - - - - - 1 1 1 1 1 1 1 3 2 2 2 2 2 2 5 - - - - - - 3 3 3 3 3 3 3 6 5 5 5 5 5 5 10 - Etd t - - Etd t - - Reg Etd Etd Etd Ez Etd t - - Reg Etd Etd Etd Ez - - - - - - - - - 82 82 82 - - - - - 82 82 82 - - - 200- - 500- - 3.090 87.588.51151.

14、5 - - 3.291 88 90 115- - mVdc- - mVdc- - Vdc Vdc Vdc Vdc Vdc Vdc - - Vdc Vdc Vdc Vdc Vdc - See notes at top of next page. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHSMIL-PRF-1/825E 4 NOTES: 1. Internal connections, do not use. 2. See “Reduced pressure

15、 (altitude) rating”, and altitude, maximum peak voltage in the basic document. 3. Cycle (or vary) the tube current between 1.5 and 3.5 mA. 4. Conditions for this test shall be those of ionization voltage (1), except testing shall be done in total darkness, and the tube shall not have conducted or ha

16、ve been exposed to light for at least 24 hours prior to testing. 5. Repeatability shall be defined as the maximum shift in tube voltage drop between successive firings of the tubs. The tube shall be tested in the following manner: (a) The voltage drop shall be read at, 2.5 mAdc drain. (b) The tube s

17、hall be turned off for 1 minute. (c) The tube shall be restarted and operated at the same current. (d) The voltage drop shall be read after 1 minute of operation. (e) The “on-off” cycle shall be repeated a minimum of five times. The maximum difference in tube voltage drop shall be taken as the measu

18、re of repeatability. 6. This test shall be conducted on the initial lot and thereafter on a lot approximately every 6-months. When one lot has passed, the 6-month rule shall apply. 7. Envelope temperature (TE) requirements, when measured in accordance with the temperature by conduction-band measurem

19、ent (method 1226), will be satisfied if a tube having bogey tube drop (Etd = 3 percent) under normal test conditions, is determined to operate at minimum specified temperature at any position in the life-test rack. 8. This specification sheet utilizes accept on zero defect sampling plan in accordanc

20、e with MIL-PRF-1, table III. Referenced documents. In addition to MIL-PRF-1 this document references MIL-STD-1311. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes. Custodians: Preparing activity: Army - CR DLA-C

21、C Navy - EC Air Force - 85 (Project 5960-2008-067) DLA - CC Review activities: Army - AR Navy - AS, CG, MC, OS, SH 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 http:/assist.daps.dla.mil/. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS