TE310 RAKON | Alldatasheet
Document overview
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Technical content
Features
Frequency Range : 10MHz to 100 MHz « Output Wave Form :; square CMOS e Supply Voltage : +5V or +12V compatible * Low Consumption : 30 mA max ® Hermetic case © Frequency Stability vs. Operating © Component selected as per ECSS-Q-ST-60C Temperature : from +/- 0.5ppm to +/— Materials selected as per ECSS-Q-70 Sppm Manufacturing in accordance with: e Ageing : +/- Sppm over 15 years © MIL-PRF-55310 (Class 1, type 3, level S,B) o ECSS-Q-ST-70-08C and ECSS-Q-ST-70-38C
Applications
© — GPS receivers Synthesizers * Converters © FGU ¢ Board calculators Specifications
1.0 Environmental conditions
Line Parameters Conditions/remarks Min Nom Max Unit Temperature option A 0 25 50 °C
11 Operating Temperature Temperature option B -20 25 70 36
Temperature option C -40 25 85 °c
1.2 Switch-on Temperature TSo -40 85 5
13 Non-Operating Temperature TNOp -55 125 °c
1.4 Random Vibration Level as per MIL-STD-202), Method 214, Condition I-K (46,3 Grms)
15 Sine Vibration Level as per MIL-STD-202), Method 204, Condition D (20G)
Mechanical shock as per MIL-STD-202, Method 213, Condition E 1.6 Shocks (half sine with a peak acceleration of 1000g for duration of 0.5 msec) te TID : 100 kRad, low dose rate ar Radiation No SEL up to LET=60 MeV/mg/cm? March, 11th 2012 OO “Specifications subject to change without notice _ _ Shortform, 51000655.110, Issue A3 1/5 www.rakon.com
2.0 Electrical interface
Line Parameters Conditions/remarks Min Nom Max Unit 4 Power supply Supply option 1 475 5.0 5.25 Vv Supply option 2 11.4 12.0 12.6
10 MHz < Frequency < 30 MHz, In parallel with 1 kQ 13 15 18 pF
22 Load Impedance 30 MHz < Frequency <50 MHz, In parallel withikQ 62 7 7.5 pF
50 MHzsFrequency < 100 Mk, In parallel with 1 kQ 42 47 Sit pF
2.3 Adjustment Resistor Radj Calibration option 1 (e) 10 kQ
3.0 Performances
Line Parameters Conditions/Remarks Min Typ Max — Unit
3.1 Nominal Frequency 10 100 MHz
3.2 Steady state supply power (Rnom) 30 mA
33: Initial frequency accuracy uae Rnom +1 = ppm Negative slope
3.4 Frequency adjustment Calibration option 1 RadjMin +5 ppm
3.5 Calibration option 2 NA
Temperature option A +0.5 ppm
3.6 Frequency stability vs temperature Temperature option B ait ppm
Temperature option C +5 ppm 3.7. Frequency variation vs. supply voltage Over Operating Temperature +0.1 ppm 3.8 Frequency variation vs. load Over Operating Temperature +0.2 ppm 3.9 pisducneraene Over 1 year #1 ppm
3.10 Over 15 years +5 ppm
3.11 Output waveform AHCMOS compatible Square
3.12 Output level VOL 0.4 Vv 3.13 VOH 2.4 Vv
3.14 Duty cycle 45 55 %
3.15 Rise time 10%-90% of Vcc 5 ns
3.16 Fall time 90%-10% of Vcc Ks ns
Shortform, 51000655.110, Issue A3 2/5 www.rakon.com
fa kon Space Temperature Compensated Crystal Oscillator TE310 TCXO Series 310
4.0 Mechanical features Weight 25 grams
Maximum package height under atmospheric pressure 12.8 [0.504] max Maximum package height under underpressure 13.2 [0.519] max Zz Number of lead : 13 Leads on 2 sides Y. x |.D bead : Pins #: _|Grounds pins : Pins # : COUPE A-A 8 A = 3 | _ H Ej 13,30 £1,30 25,60 Max 13,30 £430 = 1 4 1 x CT a FS a] | a ae Eg] ool sa | —— sy far | Ps = = Cc [0,02 max.] 0,01 toot] _ 9,60 max eS ¢ Se) DETAILC ts ECHELLE3 :1 DETAILB So ECHELLE 10:1 ~ 150.Plan dencombrement oA GEN. TOL. SCALE DOCUMENT: 150-Oscillator outline | =} -6- | +04 3:2
5.0 Pin description
Line Pin number Name Function 5.1 1-3-7-12-14 GND Electrical & Mechanical Ground 5.2 2 Vee Supply Voltage 5.3 4-5-8-9-10-11 NC Do not connect 5.4 6 Radj Calibration option 1 Resistor Adjustment 5.5 13 Fout Frequency Output ‘March, 11th 2012 - OO ~~ Specifications subject to change without notice 7 Shortform, 51000655.110, Issue A3 3/5 www.rakon.com
6.0 Model philosophy
Representativeness Engineering Engineering Qualification Flight Flight Model Model Qualification Model Model + Model Lot Acceptance test (option A) (options B, C) (option D) (options £, (option!) F,G, H) Component Passive Mil Grade parts HiRel Parts HiRel Parts HiRel Parts commercial procured from parts the same Active parts manufacturer of from the same HiRel parts manufacturer of HiRel parts Crystal material Swept quartz Swept quartz Swept quartz Swept Swept ESCC3501 quartz quartz Stabilized Stabilized Stabilized ESCC3501 ESCC3501 Stabilized Stabilized Mechanical Flight Flight Flight design Flight design Flight design interface representative representative in in form-fit- form-fit-function function Electrical interface Flight Flight Flight design Flight design Flight design design design Tests Acceptance Qualification Qualification Acceptance Acceptance testing testing testing testing testing (including (including (including screening) screening) screening)+ LAT Workmanship IPC610 ECSS-Q-ST-70-08 — ECSS-Q-ST-70-08 ECSS-Q-ST- ECSS-Q-ST- 38 38
7.0 Flight Model Screening according to MIL-PRF-55310
Full Level S (option E) Level S with combined burn in aging of 480 hours (option F) Full Level B (option G) Level B with combined burn in aging of 480 hours (option H) Lot Acceptance test could be performed on all screening options
8.0 Options for Engineering Qualification Model
Production manufacturing, qualification flow including qualification mechanical tests (option B) © Production manufacturing, electrical tests only (option C)
9.0 Deliverable documentation
© Certificate of Conformity (CoC) March, iith20i2.-—~=~=~*”:S*«S cations subject to change without notice Shortform, 51000655.110, Issue A3 4/5 www.rakon.com
10.0 Ordering part number definition
The part number breakdown is defined as follows: TE 310 EA1 1 14 40M000000 Series | Model A=EM B = EQM full environmental testing C = EQM reduced environmental testing D=QM E=FM level S F = FM level S with combined Bl-aging G=FM level B H = FM level B with combined Bl-aging | = FM + group C Temperature range/Stability A= OT to +50T, +0.5 ppm B =-20T to +70T, + 1 ppm C=-40T to +85T, + 5 ppm Supply voltage 1= 5V 2=12V Wave form 1 = Square AHCMOS Frequency adjustment 1:45 ppm Frequency, fnom Shortform, 51000655.110, Issue A3 5/5 www.rakon.com