DLA MIL-PRF-1 1105A-1999 ELECTRON TUBE GAS SWITCHING TYPE 6564.pdf

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1、I INCH-POUND I 27 Auqust 1999 SUPERSEDING 7 June 1957 MIL-PRF-I/I 105A MIL-E-l/1105(SigC) Unit: PERFORMANCE SPECIFICATION SHEET Kw V dc R ELECTRON TUBE, GAS SWITCHING TYPE 6564 This specification is approved for use by all Depart- ments and Agencies of the Department of Defense. The requirements for

2、 acquiring the electron tube described herein shall consist of this document and the latest issue of MIL-PRF-I. DESCRIPTION: Dual T. R. tube (band pass). Pack in sealed water-vapor-proof bag. If opaque bag is used, the tube type number shall be stamped thereon. APPLICATION: Used with short-slot hybr

3、id couplers. DIMENSIONS: See figures 1 and 2. ABSOLUTE RATINGS: Open circuit Parameter: I Transmitter Po I ignitorvoltage I Altitude I I -700 Maxim um : I Minimum. GENERAL: The Preproduction sample approval requirements in Signal Corps Drawing SC-A-46600 hereby replace any qualification requirements

4、 existing in or otherwise referable to the data in this specification sheet. (Copies of Signal Corps Drawing SC-A-46600, “Preproduction Sample Approval in Lieu of Qualification Requirements in Specifications,“ may be obtained from the acquiring activity or as directed by the contracting officer. AMS

5、C N/A 1 of6 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited FSC 5960 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-111105A TABLE I. Testinci and inspection. Inspection Qualification Dielectric material Degra

6、dation due to vi bration Low level VSWR Insertion loss Transmitter - receiver Isolation Ignitor Interaction Ignitor Ignition time Ignitor voltage drop Flat leakage power Spike leakage energy Arc loss Temperature cycle Temperature cycling life Method 41 O1 4021 4473 441 6 4491 4421 4401 4406 4452 445

7、2 4488 1027 1027 Conditions G=10 11 F = 8,500 MHz f 0.1% F = 8,800 MHz f 0.1% F = 9,000 MHz f 0.1% F = 9,300 MHz f 0.1% F = 9,600 MHz f 0.1% F = 8,500 MHz f 0.1% F = 8,800 MHz f 0.1% F = 9,000 MHz f 0.1% F = 9,300 MHz f 0.1% F = 9,600 MHz f 0.1% li = 1 O0 pA dc on each ignitor F = 8,500 MHz f 0.1% F

8、 = 8,800 MHz f 0.1% F = 9,000 MHz f 0.1% F = 9,300 MHz f 0.1% F = 9,600 MHz f 0.1% li = 1 O0 pA dc on each ignitor li = 1 O0 pA dc on each ignitor 21 Ebb = -700 V dc; R = 4.0 Meg 31 li = 100 pA dc on each ignitor 41 F = 9000 MHz f 0.5 %o; PO = 40 kw f 10%; prr = 1,000; tpl = l.OfO.l ps; tp2 = 0.5 f

9、0.05 ps; li = 1 O0 pA dc on each ignitor F = 9,000 MHz f 0.5%; PO = 40 kw f 10%; prr = 1,000; tpl = l.OfO.l ps; tp2 = 0.5 f 0.05 ps; li = 1 O0 pA dc on each ignitor F = 9,000 MHz f 0.5%; PO = 40 kw f 10%; Drr = 1,000; tp = 1 .o f 0.1 5 ps c Max _ _ 1.2 1.2 1.2 1.2 1.2 1 .o 0.8 0.8 0.8 1 .o _ _ _ _ _

10、 _ _ 0.1 5.0 -375 20 O. 1 0.8 _ _ Unit _ _ _ _ _ _ _ dB dB dB dB dB _ dB dB dB dB dB _ dB sec V dc mw erg dB _ _ See footnotes at end of table 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1 105A TABLE I. Testinci and inspection - Conti

11、nued Inspection Recovery time (1) Recovery time (2) High level VSWR Life test Life test end point: Recovery time (1) Recovery time (2) Flat leakage power Spike leakage energy Insertion loss Method 4471 4471 4474 _ _ 4471 4471 4452 4452 4116 Conditions F = 9,000 MHz f 0.5%; PO = 200 kw f 10%; tp = 1

12、.O p f 0.05 p; prr = 1,000; li = 1 O0 pA dc on each ignitor F = 9,000 MHz f 0.5%; PO = 65 kw f 10%; tp = 1 .O p f 0.05 p; prr = 1,000; li = 1 O0 pA dc on each ignitor F = 9,000 MHz f 0.1%; PO = 40 kw f 10%; tp = 1 .O p f 0.05 p; prr = 1,000; li = 1 O0 pA dc on each ignitor F = 9,000 MHz f 5%; li = 1

13、 O0 pA dc on each ignitor PO = 200 kw f 10%; tp = 1 .O p f .O5 p; prr = 1,000; Group D F = 9.000 MHz f 0.1% Symbol t t 6 t t t ws Pf _ Max 7.0 3.0 1.2 _ 10 5 20 .I5 1 .o - I/ There shall be no evidence of shorts of the ignitor electrodes as indicated by a short indicator during vibration. - 2/ Ignit

14、or interaction is measured with the specified ignitor current adjusted on both ignitor electrodes. - 3/ Ignitor ignition time shall be measured separately for each ignitor electrode. - 4/ Ignitor voltage drop shall be measured separately for each ignitor electrode. - 5/ All measurements that include

15、 short-slot hybrids shall be made with gaskets bolted between input and output flanges of tube and mating flanges. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1 105A W X MATING FLANGE v Il Il GASKET Dimensions Dimensions FIGURE I. Mat

16、inci flancie and ciasket. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-1/1 105A A A- l- E 5 OUTPUT FLANGE INPUT FLANGE l / t- NOTE: Exhaust stem not to extend beyond flange. 4 FGH FIGURE 2. Input and output flancies. 5 Provided by IHSNot

17、 for ResaleNo reproduction or networking permitted without license from IHS-,-,-Custodians: Army - CR Air Force - 11 DLA - CC Review activities: Army - MI Preparing activity: DLA - CC (Project 5960-A252) 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-