Space Voltage Controlled Crystal Oscillator
TE 200
VCXO Series 200
For this product, full and detailed specifications can be delivered on request. Specific request can be addressed to RAKON
[email protected]
Product Description
This ITAR free Space Flat Pack VCXO is featured by excellent pulling range of +/70ppm, good ageing characteristics of +/- 1 ppm per year, low power consumption of 0.15W, compact package size (20x20x13mm), and weight of 20g. The main applications are space synthesizers and transponders. These Space Flat Pack VCXOs are manufactured in accordance with MIL-PRF-55310 (Class 1, type 2, level S).
Features
• Frequency Range : 10MHz to 40 MHz • Supply Voltage : +5V or +12V • Low Consumption : 30 mA max • Frequency Stability vs. Operating
Temperature : from +/- 10ppm to +/15ppm • Ageing : +/– 5ppm over 15 years • Output Wave Form : sine 50 Ohms
• Output Level : from 0 to 8 dBm • Component selected as per ECSS-Q-ST-60C • Materials selected as per ECSS-Q-70 • Manufacturing in accordance with:
o MIL-PRF-55310 (Class 1, type 2, level S)
o ECSS-Q-ST-70-08C and ECSS-Q-ST-70-38C
Applications
• GPS receivers • Converters • Board calculators
• Synthesizers • FGU
Specifications
1.0 Environmental conditions
Line
Parameters
Conditions/remarks
Min Nom Max
Unit
Temperature option A
0 25 50
°C
1.1
Operating Temperature
Temperature option B
-20 25
70
°C
Temperature option C
-40 25
85
°C
1.2 Switch-on Temperature TSo -40 85 °C
1.3
Non-Operating Temperature
TNOp - 55 125 °C
1.4
Random Vibration
Level as per MIL-STD-202), Method 214, Condition I-K (47,60 Grms)
1.5
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)
1.7
Radiation
TID : 100 kRad, low dose rate No SEL up to LET=60 MeV/mg/cm²
March, 11th 2012 Shortform, 51000652.110, Issue A4
Specifications subject to change without notice
1/5 www.rakon.com
Space Voltage Controlled Crystal Oscillator
TE 200
VCXO Series 200
2.0
Line 2.1
2.2 2.3 2.4
Electrical interface
Parameters Power supply
Load Impedance Control voltage Adjustment Resistor
Conditions/remarks Supply option 1 Supply option 2
Radj Calibration option A Calibration option B
Min Nom Max Unit 4.75 5.0 5.25 V 11.4 12.0 12.6 V 45 50 55 Ω
0 5V 0 10 kΩ NA NA NA
3.0
Line 3.1 3.2 3.3
3.4
3.5
3.6
3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14
Performances
Parameters Nominal Frequency Steady state input current
power Initial frequency accuracy
Frequency adjustment
Frequency control
Frequency stability vs temperature
Frequency variation vs. supply voltage
Conditions/Remarks
Min Typ Max 10 40
(Rnom)
30
Calibration option A
Rnom
Calibration option A
Negative slope
RadjMin +5
RadjMax
Control voltage option A
±40
Control voltage option B
±70
Temperature option A
± 10
Temperature option B
± 10
Temperature option C
± 15
±1 -5
Over Operating Temperature
± 0.5
Unit MHz mA ppm
ppm ppm ppm ppm ppm
ppm
Frequency variation vs. load Over Operating Temperature
± 0.5
ppm
Frequency ageing Output waveform
Output level Harmonics level
Over 1 years
Sine 0
± 1 ppm
dBm – 30 dBc
Spurious level Phase noise
noisefloor
– 80 dBc – 145 dBc/Hz
March, 11th 2012 Shortform, 51000652.110, Issue A4
Specifications subject to change without notice
2/5 www.rakon.com
Space Voltage Controlled Crystal Oscillator
TE 200
VCXO Series 200
4.0 Mechanical features
Weight 20 grams
5.0 Pin description
Line Pin number 5.1 1-3-7-12-14 5.2 2 5.3 4
5.4 6 5.5 5-9-10-11 5.6 13
March, 11th 2012 Shortform, 51000652.110, Issue A4
Name GND Vcc Radj NC Vc NC Fout
3/5
Function Electrical & Mechanical Ground
Supply Voltage Calibration option A Resistor Adjustment Calibration option B Do not connect
Control voltage input Do not connect
Frequency Output
Specifications subject to change without notice
www.rakon.com
Space Voltage Controlled Crystal Oscillator
TE 200
VCXO Series 200
6.0 Model philosophy
Representativeness Engineering Model
(option A)
Engineering Qualification Model
(options B, C)
Qualification Model
(option D)
Flight Model
Flight Model + Lot Acceptance test
(options (option I) E, F, G, H)
Component Crystal material
Passive commercial
parts Active parts from the same manufacturer of HiRel parts Swept quartz
Mil Grade parts procured from
the same manufacturer of
HiRel parts
Swept quartz
Stabilized
Stabilized
Mechanical interface
Electrical interface Tests
Flight representative
in form-fitfunction Flight design
Acceptance testing
Flight representative in form-fit-function
Flight design Qualification testing
Workmanship
IPC610
ECSS-Q-ST-70-08 & 70-38
HiRel Parts
Swept quartz ESCC3501 Stabilized
Flight design
Flight design Qualification
testing (including screening) ECSS-Q-ST-7008 & 70-38
HiRel Parts
HiRel Parts
Swept quartz ESCC3501 Stabilized Flight design
Swept quartz ESCC3501 Stabilized
Fligh.