DLA MIL-PRF-1 1386 F-2008 ELECTRON TUBE CATHODE RAY TYPE 4QP2 [Refer To DLA MIL-STD-1311 C VALID NOTICE 1 DLA MIL-STD-1311 C DLA MIL-STD-1311 B CHG NOTICE 4 DLA MIL-STD-1311 B NOTI.pdf

1、AMSC N/A FSC 5960 INCH-POUND MIL-PRF-1/1386F 2 December 2008 SUPERSEDING MIL-E-1/1386 E 20 July 1976 PERFORMANCE SPECIFICATION SHEET ELECTRON TUBE, CATHODE RAY TYPE 4QP2 This specification is approved for use by all Depart- ments and Agencies of the Department of Defense. The requirements for acquir

2、ing the electron tube described herein shall consist of this document and the latest issue of MIL-PRF-1. DESCRIPTION: Flat face, rectangular, electrostatic deflection and focus, post accelerator. DIMENSIONS AND PIN CONNECTORS:- See figure 1. ABSOLUTE RATING: Parameter: Ef Ec1 Eb1 Eb2 Eb3 Ed Rg Unit:

3、 V Vdc Vdc Vdc Vdc V Meg Maximum 6.9 0 160 650 3,400 200 1.5 Minimum: 5.67 -200 - TEST CONDITIONS: (Cathode reference ) (Notes 1 and 2) 6.3 Adjust Focus 575 3,000 - - TEST CONDITIONS: (Oscilloscope use) (Ground reference) ( Notes 1 and 2) 6.3 Adjust Focus - - - - ABSOLUTE RATINGS: Parameter: Zd Ehk

4、Eb3/Eb2 Ek Egeom Esd East Escn Unit: Meg (Note 2) Vdc Ration Vdc Vdc Vdc Vdc Vdc Maximum - +180 5.2 - - - - - Minimum: 1.0 -180 - - - - - - TEST CONDITIONS: Cathode reference ) (Notes 1 and 2) - - - - - - - - TEST CONDITIONS: (Oscilloscope use) (Ground reference) ( Notes 1 and 2) - - - -575 Adjust A

5、djust Adjust 2,425 GENERAL: Qualification - Required Inactive for new design after 5 December 1997 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 2TABLE I. Testing and inspection. Limits Inspection MIL-STD-1311 Method Notes Condition

6、s Symbol Minimum Maximum Unit Conformance inspection, Part 1 Temperature cycling Pressure ( implosion) Barometric pressure, reduced Low-temperature operation Vibration Cathode illumination Direct-interelectrode capacitance Neck and bulb alinement (electrostatic types) Face tilt Deflection-factor uni

7、formity Magnetization Shock 1027 1141 1002 1026 5111 5216 1331 5101 5101 5248 5256 - - - - - - - - - - 8 - 0 Cathode to all Grid No. 1 to all D1 to D2 D3 to D4 D1 to all D2 to all D3 to all D4 to all - 1D2 3D4 - - - - - - Ck Cg1 C1D2 C3D4 CD1 CD2 CD3 CD4 - DFU DFU - - 5 - - -55 - - - - - - - - - - -

8、 - - - - - - - - 1 - 5.3 6.8 2.8 1.0 6.3 6.7 3.8 3.8 - 0.080 3 3 - - Cycles - - C mm - pF pF pF pF pF pF pF pF - Inch % % - - Conformance inspection, part 1 Electrode current (anode No. 3) Voltage breakdown Voltage breakdown (electrostatic types) Gas “cross” Angle between traces Screen and faceplate

9、 blemishes Modulation 5201 5201 5201 5206 5101 5106 5223 12 3 - - 13 - - - Ib3-15A Ib3 = 10 A - - - - Ec1 - - - - 89 - - 15 - - - 91 - 30 Adc - - - Degrees - Vdc Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 3TABLE I. Testing and in

10、spection. Continued Limits Requirement or Test MIL-STD-1311 Method Notes Conditions Symbol Minimum Maximum Unit Conformance inspection, Part 1 Continued Line with “A” (electrostatic deflection) Line width “B” (electrostatic deflection) Spot postion (electrostatic deflection) Spot displacement (leaka

11、ge) Grid cutoff voltage Focusing voltage at cutoff Deflection factor Grid No. 1 leakage current Anode No 1 leakage current Anode No. 2 leakage current Geometry adjust Deflection plate shield Astigmatism adjust Useful scan Pattern distortion 5226 5226 5231 5241 5241 5246 5248 5251 5251 5251 - - - - 5

12、 4 - - - - - - - - - 6, 10 7, 10 10 - Ib3 = 10 A Ib3 = 10 A ID2 3D4 3D4 1D2 3D4 - - - - - Ec1 Eb1 DF DF - - - - - - - - - - - - - - -40 - 22.5 13.5 520 520 520 - - - 0.75 0.80 6 8 10 -20 180 27.5 16.5 3 5 5 595 595 595 2.50 2.25 - mm mm mm mm mm Vdc Vdc Vdc/in.Vdc/in.Adc Adc Adc Vdc Vdc Vdc Inch Inc

13、h - Conformance inspection, Part 2 Heater current Electrode current (anode No. 1) Electrode current (cathode) Base alinement (electrostatic types) Side terminal and base alinement (electrostatic types) 1301 5201 5201 5101 5101 - - - - - Ec1 = 2 Vdc Ib3 = 15A +ID2,Pin No. 4 +ID2 If Ik - - 540 -15 - -

14、 660 +10 0.500 - mA Adc mAdc - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 4TABLE I. Testing and inspection. Continued Limits Requirement or Test MIL-STD-1132 Method Notes Conditions Symbol Minimum Maximum Unit Conformance inspect

15、ion, Part 2 Continued Side terminal and base alinement High-temperature operation Neck and base alignment (electrostatic types) Stray light emission (conventional types) Screen Focusing voltage, zero-bins Heater-cathode leackage current Secureness of base, cap, or insert Permanence of marking 5101 1

16、026 5101 5216 5221 5246 5251 1101 1105 - 11 - - - - - - - Pin No. 4 Eb2 = 600 Vdc; Eb3 = 3,400 Vdc - - - - Eb1 Ihk - - - - - - - 360 40 - - - +70 - - - - - 10 - - C - - cb Vdc Adc - - Conformance inspection, Part 3 Life test Life-test end points: Line width “A” Line width “B Modulation 5226 5226 522

17、3 - - - Group C; Ib3 = 10 Adc; Eb2 = 575 Vdc; Eb3 = 3,000 Vdc Ib3 = 10A Ib3 = 10A Ib3 = 10A T - - Ec1 500 - - - - 0.75 0.80 30 hrs mm mm Vdc NOTES: 1. All readings of beam current (Ib3) shall be in addition to the reading obtained for method 5201, anode No. 3 current. For oscilloscope use, the mean

18、potentials of 1D2 and 3D4 with respect to ground shall be zero. 2. It is recommended that the deflecting electrode circuit resistance be approximately equal. Higher resistance values up to 5.0 megohms may be used for low-beam current operation. 3. With the beam cutoff, the post-accelecrator anode (A

19、3) shall draw 15 Adc maximum. 4. Spot adjusted for least astigmatism. 5. With a 2.5-by 2-inch rectangular raster centered on the face of the tube, the raster edge shall not deviate form straight parallel lines by more than 0.040 inch on the left and right edges nor by more than 0.0515 inch at the to

20、p and bottom. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 56. The post-accelerator spiral band lower end and the geometry adjust are connected internally. By adjusting the potential on this electrode combination, pin cushion and b

21、arrel distortions are minimized. 7. Normally operated at accelerator potential, linearity improvements can be obtained in the vertical trace by proper adjustment of deflection plate shield voltage. 8. For the 102 direction: Divide the axis into five successive 1/2 inch intervals symmetrically locate

22、d with respect to the geometric center of the tube face. The percentage difference (DFU)between deflection factors of the center interval and any other interval shall not exceed the limit specified. 9. A hammer-drop shock testing machine shall be used, consistent with MIL-PRF-28800. The tube may be

23、clamped as in the vibration test or mounted directly on the shock machine. With test potentials applied, display a circle or raster. Using a hammer-drop height of 6 inches, apply three blows each in directions 1D2, 3D4, and base-to face. Momentary failure of operation during shock is permissible pro

24、vided normal operation is deflection factor, spot position, and grid cutoff voltage. In addition, there shall be no evidence of damage to the internal structure. 10. Range for oscilloscope use: -55 to +20 Vdc. 11. Following temperature stabilization, the tube shall meet requirements under pattern di

25、stortion, line-width, and anode No. 3 current; all voltages and settings being those obtained at room temperature with 25 K resistors in series with geometry, shield and astigmatism adjust electrodes. 12. An accept on zero defect sampling plan (see MIL-PRF-1, table III) shall be used for conformance

26、 inspection, part 1. 13. This test to be performed at the conclusion of the holding period. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 6FIGURE 1. Outline drawing of electron tube types 4QP2 PIN NO. ELEMENT 1 HEATER 2 CATHODE 3 GR

27、ID4 N.C. 5 AI 6 N.C. 7 AZ 8 N.C. 9 V SHELD 10 N.C. 11 N.C. 12 HEATER Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1386F 7Dimensions are in inches with metric equivalents (mm) in parentheses. Ltr Mimimum Maximum Conformance inspection, pa

28、rt 2 A 13.312 (338.12) 13.688 (347.68) B - - - - - - - - 3.765 (95.63) C 1.969 (50.01) 2.031 (51.59) D 2.250 (57.15) - - - - - - - E 10.000 (254.00) 10.250 (260.35) H 1.250 (31.75) 1.500 (38.10) J 3.219 (81.76) 3.281 (83.34) K 2.719 (69.06) 2.781 (70.64) L - - - - - - - .500 (12.70) P 2.719 (69.06)

29、2.781 (70.64) Reference dimensions (see note 3) F 8.500 (215.90) G 3.125 (79.38) M .625 (15.88) R 5.500 (139.70) Rad. S 3.000 (76.20) Rad. NOTES: 1. +1D2 towards pin No. 4. 2. +3D4 towards pin No. 1. 3. These dimensions are for information only and are not required for inspection purposes. FIGURE 1.

30、 Outline drawing of electron tube types 4QP2 - Continued Referenced documents. In addition to MIL-PRF-1, this document references the following: MIL-PRF-28800 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

31、 changes. Custodians: Preparing activity: Navy EC DLA- CC DLA CC Project number (5960-2008-071) Review activities: Navy AS, CG, MC, OS 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-,-,-