TE300 RAKON | Alldatasheet
Document overview
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- PDF pages: 5
Technical content
Features
° — ITAR-Free ¢ Output Wave Form : sine 50 Ohms Frequency Range : 10MHz to 100 MHz © Output Level : from 0 to 8 dBm © — Supply Voltage : +5V or +12V ° Hermetic case e Low Consumption : 30 mA max. e Component selected as per ECSS-Q-ST-60C e Frequency Stability vs. Operating e Materials selected as per ECSS-Q-70 Temperature : from + 0.5ppm to + Sppm e 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 e Synthesizers ° Converters e FGU ° Board calculators Specifications
1.0 Environmental conditions
Parameter Conditions/remarks Min Nom Max Unit Operating Temperature |_ontin | ao | os | mc | Switch-on Temperature | So | to | Tt |e Non-Operating Temperature TNOp 125 be Level as per MIL-STD-202, Method 214, Condition I-k (46,3 Grms) Level as per MIL-STD-202, Method 204, Condition D (206) Mechanical shock as per MIL-STD-202, Method 213, Condition E (half sine with a Shocks peak acceleration of 1000g for duration of 0.5 msec) TID : 100 kRad, low dose rate Radiation No SEL up to LET = 60 MeV/mg/cm? December 23rd, 2011 Shortform, 51000654.110, Issue A4 1/5 www.rakon.com
fa kon Space Temperature Compensated Xtal Oscillator TE300 TCXO Series 300
2.0 Electrical interface
Parameters _—Conditions/remarks == Min. ~=—sNom Max Unit seeowapely Option Loadimpedance | | ts ss | Radj / Calibration option | 0 _|_ RadjNom* Note: RadjNom will be indicated on final test report
3.0 Performances
Parameters Conditions/Remarks Min Typ Max Unit NominalFrequency | | to] 00S Steady state power supply 0.2 Ww Calibration option 1/ Frequency adjustment negative slope 5 5 Frequency-temperature Temperature option A Po tt. | ppm _| stability Temperature optionB | | | ppm | Temperature optionc | | |S ppm | Frequency variation vs. supply voltage Over Operating Temperature +01 Frequency variation vs. load Over Operating Temperature +0.2 Startuptime [ts Frequency ageing | —__oversyear | | | ttm | Overasyears | | | ts pm | |__ Output waveform [Sine output level Supply votage option | 0 | | | am | Supplyvottage option2 | 7 | | am | |__Harmonicstevel [| P80 Spurious level 1ooHztorooKHz | || 80 ae @1ookzoffset| | | 805 | Bc Static Phase noise @iktzoftset| | | 130 | BH (noise floor) @ 10kHzoffset| | || Bc Allan Variance [ts | December 23rd, 2011 Shortform, 51000654.110, Issue A4 2/5 www.rakon.com
fa kon Space Temperature Compensated Xtal Oscillator TE300 TCXO Series 300
4.0 Mechanical features
Maximum package height under atmospheric pressure 12.8 [0.504] max Maximum package height under underpressure 13 [0.511] max Zz Number of lead : 13 Leads on 2 sides |.D bead: Pins #: _|Grounds pins : Pins #: P =, 4 Coupe A-A F x sas ° a 12.4130 20,60 max 42.41,30 pals’ Ss oa ast e 2 2a] ) ss : [0,01] 0,38. [0,02 max.] 0.60 max. DETAILC q (Seale 10:1) S& DETAIL D BP DETAIL3:1 150.Plan diencombrement GEN.TOL. | UNITS: | SCALE BOCUNENT: 150-Oscillator outline =O +1-0.1 mm finch} 3:2
5.0 Pin description
Pin number Name Description 1,3,7,12,14 | GND | _ Electrical & Mechanical ground Supply voltage 45,8900 [6 | Radj | Frequency adjustment option 1 December 23rd, 2011 Shortform, 51000654.110, Issue A4 3/5 www.rakon.com
6.0 Model philosophy
Representativeness Engineering Engineering Qualification Flight Model Flight Model + Model Qualification Model Lot Acceptance Model test Options A B,C D E,F,G,H 1 Passive commercial parts, Mil Grade parts Active parts from | procured from the Components the same same HiRel Parts HiRel Parts HiRel Parts manufacturer of | manufacturer of HiRel parts HiRel parts ESCC3501 ESCC3501 ESCC3501 Crystal material Swept quartz Swept quartz Swept quartz Swept quartz Swept quartz stabilized stabilized stabilized stabilized stabilized Flight Flight Mechanical representative in | representative in Flight design Flight design Flight design interface form-fit-function | form-fit-function Electrical interface Flight design Flight design Flight design Flight design Flight design Qualification Acceptance Acceptance Tests Acceptance Qualification testing testing testing (including testing testing (including (including screening)+ LAT screening) screening) IPC610 ECSS-Q-ST-70-08 & | ECSS-Q-ST-70- | ECSS-Q-ST-70- | ECSS-Q-ST-70-08 70-38 08 & 70-38 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
© Certificate of Conformity (CoC) December 23rd, 2011 Shortform, 51000654.110, Issue A4 4/5 www.rakon.com
10.0 Ordering part number definition
The part number breakdown is defined as follows: TE 300 E A114 1 40M000000 RAKON-TEMEX a 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= OTC to +50T, + 0.5 ppm B =-20T to +70T, + 1 ppm C =-40T to +85T, + 5 ppm Supply voltage 1= SV 2=12V Wave form 1 = Sine Frequency adjustment 1=+45ppm Frequency, fnom December 23rd, 2011 Shortform, 51000654.110, Issue A4 5/5 www.rakon.com