TE200 RAKON | Alldatasheet
Document overview
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- PDF pages: 5
Technical content
Features
Frequency Range : 10MHz to 40 MHz © Output Level : from 0 to 8 dBm © Supply Voltage : +5V or +12V * Component selected as per ECSS-Q-ST-60C Low Consumption : 30 mA max. Materials selected as per ECSS-Q-70 e Frequency Stability vs. Operating e Manufacturing in accordance with: Temperature : from +/- 10ppm to +/- © MIL-PRF-55310 (Class 1, type 2, level S) 15ppm oO ECSS-Q-ST-70-08C and ECSS-Q-ST-70-38C © Ageing : +/- 5ppm over 15 years © Output Wave Form : sine 50 Ohms
Applications
© GPS receivers Synthesizers * Converters e FGU * Board calculators Specifications
1.0 Environmental conditions
Line Parameters Conditions/remarks Min Nom Max Unit Temperature option A 0 25 50 "
11 Operating Temperature Temperature option B -20 25 70 %¢
Temperature option C -40 25 85 "e a2 Switch-on Temperature TSo -40 85 °c
13 Non-Operating TNOp -55 125 *c
14 Random Vibration Level as per MIL-STD-202), Method 214, Condition I-K (47,60 Grms)
- 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) cay TID : 100 kRad, low dose rate ah Radiation No SEL up to LET=60 MeV/mg/cm? March, 11th 2012 OO - Specifications subject to change without notice Shortform, 51000652.110, Issue A4 1/5 www.rakon.com
2.0 Electrical interface
Line Parameters Conditions/remarks Min) Nom Max _ Unit Supply option 1 4.75 5.0 5.25 Vv a. Power supply Supply option 2 114 12.0 12.6 Vv
2.2 Load Impedance 45 50 55 Q
23 Control voltage 0 5 v
. Radj Calibration option A (e) 10 kQ
2.4 Adjustment Resistor
Calibration option B NA NA NA
3.0 Performances
Line Parameters Conditions/Remarks Min Typ Max Unit
3.1 Nominal Frequency 10 40 MHz
32 Steady state input current (Rnom) 30 iA
3.3 Initial frequency accuracy option A Rnom #1 ppm
3.4 Frequency adjustment Calibration option A a
Pa Frequency control Control voltage option A +40 ppm Control voltage option B +70 ppm Temperature option A +10 ppm 36 Frequency stability vs . s temperature Temperature option B +10 Temperature option C #15 Frequency variation vs. . 3.7 supply voltage Over Operating Temperature +0.5 ppm 3.8 Frequency variation vs. load Over Operating Temperature +05 ppm 39) Frequency ageing Over 1 years t1 ppm
3.10 Output waveform Sine
3.11 Output level 0 dBm
3.12 Harmonics level -30 dBc
3.13 Spurious level -80 dBc
3.14 Phase noise noisefloor -145 dBc/Hz
March, 1th 2012 _ a " Specifications subject to change without notice Shortform, 51000652.110, Issue A4 2/5 www.rakon.com
fa kon Space Voltage Controlled Crystal Oscillator TE200 VCXO Series 200
4.0 Mechanical features Weight 20 grams
‘Maximum package height under atmospheric pressure 12.8 [0.504] max Maximum package height under underpressure Zz Number of lead : 13 Leads on 2 sides |.D bead : Pins #:_ |Grounds pins : Pins #: Coupe A-A 8 i Eg é | : i ° Le 12 21,30 20,60 max 12 41,30 £8/e4| Sx BS ss} u) ss : [0,01] 0.38 [0,02 max.] = | 9160 max DETAILC ( (Scale 10:1) SS DETAILD as DETAIL 3:1 150.Plan d'encombrement — aA GEN.TOL. | UNITS: SCALE
5.0 Pin description
Line Pin number Name Function 5.1 1-3-7-12-14 GND Electrical & Mechanical Ground 5.2 2 Vec Supply Voltage 53 ri Radj Calibration option A —_ Resistor Adjustment NC Calibration option B Do not connect 5.4 6 Ve Control voltage input 5.5 5-9-10-11 NC Do not connect 5.6 13 Fout Frequency Output March,1ith2012,==—s—<“<—«‘“‘<CS*: Specifications subject to change without notice Shortform, 51000652.110, Issue A4 3/5 www.rakon.com
6.0 Model philosophy
Representativeness Engineering Engineering Qualification Flight Flight Model + Model Qualification Model Model Lot Acceptance Model test (option A) (options B, C) (option D) (options —_ (option I) E, F,G, H) Component Passive Mil Grade parts HiRel Parts HiRel HiRel Parts commercial procured from Parts 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 quartz ESCC3501 quartz ESCC3501 Stabilized Stabilized Stabilized ESCC3501 Stabilized Stabilized Mechanical Flight Flight Flight design Flight Flight design interface representative representative in design in form-fit- form-fit-function function Electrical interface Flight Flight Flight design Flight Flight design design design design Tests Acceptance Qualification Qualification Acceptanc Acceptance testing testing testing etesting testing (including (including (including — screening)+ LAT screening) screening) Workmanship IPC610 ECSS-Q-ST-70-08 ECSS-Q-ST-70- ECSS-Q- —_ ECSS-Q-ST-70-08 & 70-38 08 & 70-38 ST-70-08 & 70-38 & 70-38
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
¢ Test data e Full specification © Certificate of Conformity (CoC) March, 11th 2012 Specifications subject to change without notice Shortform, 51000652.110, Issue A4 4/5 www.rakon.com
10.0 Ordering part number definition
The part number breakdown is defined as follows: TE 200 E A1 1 1 20M000000 Series | Model A=EM B = EQM full environmental testing C = EQM reduced environmental testing D=QM E=FMlevelS 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, + 10 ppm B= OCto+70T, +10 ppm C =-20T to +70T, + 15 ppm Supply voltage 1=5V 2=12V Wave form 1 = Sine Frequency pulling range 1=+40 ppm 2=+70 ppm Frequency, fnom March, 11th 2012 Specifications subject to change without notice - Shortform, 51000652.110, Issue A4 5/5 www.rakon.com