Space Crystal Oscillator
TE 100
For this product, a full detailed specification can also be delivered on request.
Specific request can be addressed to RAKON
info@rakon.fr
XO Series 100
Product Description
This SMD Space XO is designed for space clock applications and is based on hybrid technology.
The reference is resistant to shock and vibration environment.
Key advantages of this frequency source are its compact size (14x9x3.8mm), low weight (2g) and
low power consumption of 0,1W.
This XO is manufactured in accordance with MIL-PRF-55310 (Class 2, type 1, level S) and EMs can
be delivered with a very short lead time.
Features
Frequency Range : 10 MHz to 100 MHz
Low consumption: 20 mA
Supply Voltage : +3.3V or +5V
Overall Frequency Stability over 15 years ± 100ppm
Output Wave Form : square CMOS compatible
Manufacturing in accordance with:
o
MIL-PRF-55310 (Class 2, type 1, level S or B)
o
MIL-PRF-38534
Applications
Digital cards
FPGA clock
Specifications
1.
Environmental conditions
Parameter
Operating Temperature
Conditions/remarks
Option A
Option B
TSo
Min
-20
-55
-55
Nom
25
25
Max
70
125
125
Unit
°C
°C
°C
Switch-on Temperature
Non-Operating
Temperature
TNOp
-55
125
°C
Random Vibration
Level as per MIL-STD-202, Method 214, Condition I-F (20 Grms)
Sine Vibration
Level as per MIL-STD-202, Method 204, Condition D (20G)
Mechanical shock as per MIL-STD-202, Method 213, (half sine
Shocks
with a peak acceleration of 1500g for duration of 0.5 msec)
Acceleration as per MIL-STD-883, Method 2001, condition A
Acceleration
(5000g, during 60s in Y1)
TID : 100 kRad, low dose rate
Radiation
No SEL up to LET = 100 MeV/mg/cm²
Januaryr 30th, 2013
Shortform, 51000648.110, Issue A6
1/5
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Space Crystal Oscillator
TE 100
2.
Electrical interface
Parameters
Power supply
Conditions/remarks
Option 1
Option 2
In parallel with 1 kΩ
Power supply option 2
10 MHz ≤Freq < 80 MHz
Load In parallel with 1 kΩ
Power supply option 1
80 MHz≤Frequency ≤ 100 MHz,
In parallel with 1 kΩ
Power supply option 1
Min
3.13
4.5
13
13
Nom
3.3
5
15
15
Max
3.465
5.5
18
18
XO Series 100
Unit
V
V
pF
Load Impedance
pF
9.1
10
11
pF
3.
Performances
Parameters
Nominal Frequency
Steady state input
current power
Global Frequency
stability (1)
Initial frequency
accuracy
Frequency-temperature
stability
Frequency variation vs.
supply voltage
Frequency variation vs.
load
Frequency ageing
Start up time
Output waveform
Conditions/Remarks
10 MHz≤Freq< 20 MHz
20 MHz≤Freq < 50 MHz
50 MHz≤Freq ≤ 100 MHz
Temperature option A
Temperature option B
Min
10
Typ
Max
100
20
25
30
± 70
± 100
± 15
± 15
± 50
±3
±5
± 15
10
Square
0.4
2.4
0.5
4.5
45
55
5
5
Unit
MHz
mA
mA
mA
ppm
ppm
ppm
ppm
ppm
ppm
ppm
ppm
ms
V
V
%
ns
ns
± 50
± 80
± 10
± 10
± 35
Temperature option A
Temperature option B
Over Operating Temperature
Over Operating Temperature
Over 15 years
AHCMOS compatible
Option 1
VOL
VOH
VOL
VOH
Output level
Duty cycle
Rise time
Fall time
Option 2
10%-90% of Vcc
90%-10% of Vcc
Note 1 : Including initial accuracy + freq temp stability + power supply stab + ageing over 15 years
Januaryr 30th, 2013
Shortform, 51000648.110, Issue A6
2/5
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Space Crystal Oscillator
TE 100
4.
Mechanical features
Weight : 2 grams
XO Series 100
5.
Pin description
Pin number
1
2
3
4
Name
GND
Fout
Vcc
Description
Not connected
Electrical & Mechanical ground
Frequency output
Supply voltage
Januaryr 30th, 2013
Shortform, 51000648.110, Issue A6
3/5
www.rakon.com
Space Crystal Oscillator
TE 100
6.
Model philosophy
Representativeness
Engineering
Model
A
Passive
commercial parts,
Active parts from
the same
manufacturer of
HiRel parts
Swept quartz
stabilized
Flight
representative in
form-fit-function
Flight design
Acceptance
testing
IPC610
Engineering
Qualification
Model
B, C
Mil Grade parts
procured from the
same
manufacturer of
HiRel parts
Swept quartz
stabilized
Flight
representative in
form-fit-function
Flight design
Qualification
testing
ECSS-Q-ST-70-08 &
70-38
Qualification
Model
D
XO Series 100
Flight Model
Options
E, G
Components
HiRel Parts
HiRel Parts
Crystal material
ESCC3501
Swept quartz
stabilized
Flight design
Flight design
Qualification
testing
(including
screening)
ECSS-Q-ST-70-08
& 70-38
ESCC3501
Swept quartz
stabilized
Flight design
Flight design
Acceptance testing
(including
screening)
ECSS-Q-ST-70-08 &
70-38
Mechanical
interface
Electrical interface
Tests
Workmanship
7.
Flight Model Screening according to MIL-PRF-55310
Full Level S (option E)
Full Level B (option G)
Lot Acceptance test could be performed on all screening options
8.
Options for Engineering Qualification Model
Production manufacturing, qualification flow including qualification mechanical tests (option B)
Production manufacturing, electrical tests only (option C)
9.
Deliverable documentation
Test data
Full specification
Certificate of Conformity (CoC)
Januaryr 30th, 2013
Shortform, 51000648.110, Issue A6
4/5
www.rakon.com
Space Crystal Oscillator
TE 100
10.
Ordering part number definition
The part number breakdown is defined as follows:
XO Series 100
TE 100 E A 1 1 1 24M000000
RAKON
Series
Model
A = EM
B = EQM full environmental testing
C = EQM reduced environmental testing
D = QM
E = FM level S
G = FM level B
I = FM + group C
Temperature range/Overall Stability
A = –20°C to +70°C, ± 70 ppm
B = –55°C to +125°C, ± 100 ppm
Supply voltage
1 = 3.3V
2 = 5V
Wave form
1 = Square AHCMOS
Frequency adjustment
1 = internal calibration
Frequency,
fnom
A qualification flow test could follow the model “C”.
A LAT could follow the model “E”.
Januaryr 30th, 2013
Shortform, 51000648.110, Issue A6
5/5
www.rakon.com
