CK5654 RAYTHEON | Alldatasheet
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RAYTHEON) INFORMATION = RELIABLE PENTODE eee) os ave 4 ae TT eT Las Sete RRR Eee eae eT : BOSE Brae eo Emre ae ere ee TYPE —~ ‘ ° ‘ CK5654/ The CK5654 /6AKSW /6096 is a heater-cathode type, sharp cutoff, RF pentode of miniature con- 6AK5W/6096 struction for use in low power applications at high and ultra-high frequencies. It is designed for dependable operation under conditions of shock vibration ususlly found in mobile and circraft ap- plications. MECHANICAL DATA ENVELOPE: 1-5) Glass F i BASE: Miniature Button 7-Pin i TERMINAL CONNECTIONS: : 3 Pin | Grid #1 Pin Plate g z Pin 2 Cathode, Grid #3 Pin 6 Grid #2 z 3 Pin 3 Heater Pin 7 Cathode, Grid #3 ba Pin 4 Heater 4+ MECHANICAL RATINGS: UT Tt Moximum Impact Acceleration (Shock Test-Note 3) 450 G Maximum Vibrational Acceleration (96 Hour Fatigue Test- Note 4) 25 § Maximum Bulb Temperature 165 °C MOUNTING POSITION: Any (4) ELECTRICAL DATA Q aay CAUTION: To Electronic Equipment Design Engineers: Special attention should be given to the @ | TI temperature at which the tubes are to be operated. Reliability will be seriously impaired if maximum N Ca! 1] bulb temperature is exceeded, The life expectancy may be reduced if conditions other than those HT specified for life test are imposed on the tube and will be reduced appreciably if absolute max « imum ratings are exceeded. Both reliability and performance will be jeopardized if filament voltage ratings are exceeded. Life ond reliability of performance are directly related to the degree that reg- BOTTOM VIEW ulation of the heater voltage is maintained at its centered rated value. NORMAL RATINGS AND MIL-E-1B ABSOLUTE TEST NORMAL ABSOLUTE MIL-E- 1B NORMAL OP ERATION: SYMBOL MINIMUM CONDITIONS OPERATION MAXIMUM — UNITS (Note 6) (Note 5) Heater Voltage (Note 7): Ef: 5.7 6.3 63 63 69 Vv Plate Voltage : Eb: 120 120150 200 Vde Grid #1 Voltage: Eel: -2.0 0 fy Vde Grid #2 Voltage : Ec2: 120 120. 140 155 Vde Plate Dissipation : Pp: 0.9 1.05 1.65 W Grid #2 Dissipation : Pg?: 0.3 0.31 0.55 W Hester=Cathode Voltage: Ek: = 130 +130 Vde Cathode Current (Note 9) Ik: 10.0 9.2 20 mAdc Cathode Resistance: Rke 200 © 330 ohms CHARACTERISTICS AND QUALITY CONTROL TESTS (Note 1) TEST CONDITIONS AQL MIL-E-1B MIN, LAL. BOGIE UAL. MAX. ALD, MIL-E-1B % SYMBOL UNITS ACCEPTANCE TEST- GROUP C Continuity and Short: 0.4 ACCEPTANCE TESTS- GROUP D COMBINED AQL=1.0% Heater Current : 0.65 fr 160 175 190 mA Heater-Cathode Leckage Ehk= 100 Vdc, Thies 10 pAde Hecter Positive 0.65 Ehk= 100 Vdc, hk: 10 pAde Heater Negative Tentative Data — RAYTHEON MANUFACTURING COMPANY (O03) 5 RECEIVING AND CATHODE RAY PUBEM OPERATIONS 6 25% December 22, 1954 NEWTON 58, MASS. Page 1 of 6
PEAR EER ARE EAS ARAN ALUN RTS RAN ES Ce AIRES RIT SLIT VOW CHARACTERISTICS AND QUALITY CONTROL TESTS (Note 1) (cont'd) * SYMBOL UNITS: Grid Current (1): Rgl=0.1 Meg. 0.65, kel (1 y +0. pAde Transconductance (1): 0.65 Sm(1): 4000 4525 5000 $475 6250-1025 pmhos ACCEPTANCE TESTS- GROUP E Insulation of Electrodes: EF=6.3V E(gl-all )= 2.5 R(gl- 100 meg. 100 Vdc ; g! Negative all): E (g2- ail $2300 Vde; R(g2- 100 meg.
2 Negetive ail:
E(p- all }= 300 Vde R(p- 100 meg. P Negative all 5: Plate Current (2): Ecl=- 10 Vde 2.5 tb(2): 200 pAde Plate Current (3): Ecl=-5.5 Vde 2.5 Ib (3): 5.0 pAde Transconductance (2): Ef=5.7V; (Note 8) 25 aSm: 15 % Grid Current (2): fb 150 Vde; Ec2= 125 25 4c1(2): 0 +05 pAde lc; Ecl=0; Ef= 7.0 Vac; RK=130 ohms; Rgl=0.1 Meg; after 5 min, at Ef=7,0Vac; measure grid current at Ef=7.0Vac; 3 min. test not permitted. RF Noise: Ecl=0; E wale 15.0m- 25 3.0 mW Vac ;RK=200 ohms; CK=0.2 ut Noise and Microphonics: Ef= 6.3 Vac; Ebb= 25 Ep: 100 mVac Ecc2= 200 Vde ; Ecl= 0; Rk= 1000 ohms ; Rp= 0.1 meg.; Rg2= 0.5 Meg. ; Cg2= 2 uf. Ehk=0; CK= 1000pf. ACCEPTANCE TESTS- GROUP A Shock: Hammer Angle= 30° (Note 3) Fatigue : 96 Hours : (Note 4) 6.5 Post shock and Fatigue Test end Points : Vibration (2): F=25 cps; G=2.5; Ep (2): 450 mVac Rp= 10,000 ohms’ Heater- Cathode Ehk= + 100 Vde: thk(1)2 30 pAde Leakage (1): Heater - Cathode Ehk=- 100 Vde Uhk (2) 30 pAde Leakage (2): ‘Transconductance (1): Sm(1): 3500 phos Grid Current (1): fel (1): 0 +02 pAde ACCEPTANCE TEST-GROUP F Vibration (2): F=25 cps; G= 2.5; 65 Ept 150 mVac Rp= 10,000 ohms Capacitance + (Note 2) CgIP: 9.020 uut Capacitance : (Note 2) 6.5 Cin: 3.40 4.6 uuf Capacitance : (Note 2) Cout: 245 3.25 vot Low Pressure Voltage 65 500 Voc Breckdown: RAYTHEON MANUFACTURING COMPANY a 7 SEB eT Rot eu fe Cee errr Rees REMNANTS ROLLIN SH VE CL HC RR aN NDR ON aR TC December 22, 1954 NEWTON 58, MASS. Page 2 of 6
4 » TYPE CK5654/ ) GAKSW /6096 os _ RELIABLE PENTODE ; CHARACTERISTICS AND QUALITY CONTROL TESTS (Note 1) (contd) TEST CONDITIONS AQL MIL -E-1B MIN, LAL. BOGIE UAL, MAX, ALD MIL-E-1B % SYMBOL UNITS ACCEPTANCE TEST - GROUP B Glass Stroin : 25 ACCEPTANCE LIFE TEST Heater Cycling : EF=7.5V; Ehk=+ 135 2000 cycles Vde; Eel = Eb= Ec2=0 Heater Cycling Life Test End Points: Heater-Cathode Ehk=+ 100 Vde Uhke (1): 20 pAde Leakage (1): Heoter Cathode Ehk=+ 100 Vde hk (2): 20 pAde Leakage (2): I Hour Stability Life TA=Room; Ehk=+ 135 Test: Vde; Eb= 150Vde; Ecl= 0; Ee2= 125 Vde ; Rgl= O41 Meg.; Rk= 130 ohms
1 Hour Stability Life
Test End Points : Transconductance {typical sample size= 1.0 2Sm(1): 10 % (1): Change of in- 50 tubes ) dividual tube from initial :
100 Hour Survival Rate TA= Room; Ehk=+ 135
Life Test: Vde; Eb= 150Vde; Ecl= 0; Ec2= 125 Vdc; Rol=
0.1 Meg; Rk= 130 ohms
100 Hour Survival
End Points: Inoperatives : (Typical somple size= 0.65 200 tubes ) 500 and 1000 Hour = T - Bulb= 165° C; Ehk= Intermittent High + 135 Vde Temperature Life Eb= 150Vde ; Ecl=0; Test: Ec2= 125 Vde Rgl= 0.1 Meg; Rk= 130 ohms TEST CONDITIONS MIL-E-1B 0 MIN. MAX. MIL-E-1B MAX, DEFECTS SYMBOL, UNITS PER CHARACTERISTIC Ist Combined Sample Sample
500 Hour intermittent (Typical sample size
High Temperature = 20 tubes Life Test End Points: 1st sample, 40 tubes 2nd sample (Total ‘aliowable combined defects= 4 tubes Ist sample, 8 tubes Ist ond 2nd samples ) Inoperatives : 1 3 Heater Current : i 160 190 mA 1 3 Heater- Cathode Leakage the: 10 pAde 1 3 Grid Current (1): leV(1): +0.) pAde 1 3 Transconductance (1): Sm(1): 3750 6250 pumhos 1 3 Transconductance (1) ove. 0 15 % Average Change (Note 10): Sm (1): Printed in U.S.A. RAYTHEON MANUFACTURING COMPANY le sie ne nen SRE Se aes ee Oe ea cre ee mae ees ee oe Sen Ree a aeons ate PAD St xt RSE SD oe NUS December 22, 1954 NEWTON 58, MASS. Page 3 of 6
CHARACTERISTICS AND QUALITY CONTROL TESTS (Note 1) (cont'd) TEST CONDITIONS MIL-E-1B 0 MIN. MAX, MIL-E-1B MAX. DEFECTS SYMBOL UNITS PER CHARACTERISTIC Ist Combined Somple Sample Plate Current (1): tb(1): 4S 11.0 mAde 2 5 Electrode {nsulation : {at-all} Rgl-all: 50 meg. @2- all) Rg2-all: 50 meg. 2 5 (P-all) Rp-all: 50 meg. Transconductance (2) (Note 8) Sm(2): 15 % 2 5 (Typical sample
1000 Hour Inter- size= 20 tubes Ist
mittent High sample, 40 tubes Temperature 2nd sample ) Life Test End Points: Inoperatives 2 5 Heater Current : If: 160 190 mA 2 5 Heater - Cathode Leakage : thk: 10 pAdc 2 5 Grid Current (1): fel (1): 0.1 pAdc 2 5 Transconductance ys Sm(1): 3500 6250 pmhos: 2 5 Plote Current (1): tb(1): AO 11.0 mAdc 4 8 NOTES: Note | Characteristics, Quality Control Test Procedures, and Inspection Levels are made according to the appropriate paragraphs of MIL-E-1B “Inspection Instructions for Electron Tubes " and MIL-STD- 105A. Note 2 With Shield #316 connected to cathode. Note 3. Test Conditions and Acceptance criteria per Shock Test procedures of MIL-E- 1B basic specification, Note 4 Test Conditions and Acceptance criteria per Fatigue Test procedures of MIL-E- 1B basic specification. Note 5 These normal values represent conditions at which control reliability may be expected. Note 6 These normal test conditions ore used for all characteristics unless otherwise stated under the individual test item. Note 7 For most applications the performance will not be adversely affected by + 10% heater voltage variation, but when the application can provide a closer control of heater voltage, an improvement in reliability will be realized. Note 8 Change of transconductance for individual tubes from that value measured ot Ef= 6.3V to that value measured at Ef=5.7V. Note 9 Difficulty may be encountered if this tube is operated for long periods of time with very small values of cathode current. Note 10 The average percentage change shall be ascertained from the determination of the individual changes for each tube (inoperatives excluded ) from the zero hour value for the referenced characteristic. RAYTHEON MANUFACTURING COMPANY SS RECEWING AND CATHODE RAY TUBE COPERAT eee es oo December 22, 1954 NEWTON 58, MASB. Page 4 of 6
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