* See Page 5 for additional developed frequencies.
Check with factory for availability of frequencies not listed.
Description
CTS Model 407 incorporates a high Q quartz resonator and is ideal for supporting a wide range of commercial and
industrial applications.
Ordering Information
Model
407
Mode of
Oscillation
F
Tolerance
@ +25°C
3
Temperature Stability/Temperature Range
5
Load
Capacitance
D
Frequency
[MHz]
XXXMXXXX
Mode
Code
Fundamental
F
3rd Overtone
T
Code
-20°C
1
X
2
3
5
Stability
to +70°C
±10ppm
±15ppm
±20ppm
±30ppm
±50ppm
Code
-30°C
R
Y
N
4
8
Stability
to +85°C
±10ppm
±15ppm
±20ppm
±30ppm
±50ppm
Code
-40°C
-
W
6
7
9
Stability
to +85°C
-
±15ppm
±20ppm
±30ppm
±50ppm
Code
Frequency
Frequency
1
Code
1
X
2
3
Tolerance
±10ppm
±15ppm
±20ppm
±30ppm
Code Capacitance Code Capacitance
8pF
18pF
K
D
9pF
20pF
J
E
10pF
24pF
A
F
12pF
30pF
L
G
16pF
Series
C
S
Notes:
1] Frequency is recorded with 3 leading digits before the "M" and 4 significant digits after the "M" [including zeroes]. (Ex. XXXMXXXX [016M3840], XXXMXXXX
There are frequencies that have significant digits after the "M" that exceed the 4 digits. The remaining digits will be truncated from the CTS part number,
but the factory will calibrate to the full frequency desired. Examples below; P/N Frequency = Actual Frequency
13M5537 = 13.553750MHz
14M3181 = 14.318180MHz
16M6666 = 16.666670MHz
28M6363 = 28.636360MHz
Not all performance combinations and frequencies may be available.
Contact your local CTS Representative or CTS Customer Service for availability.
This product is specified for use only in standard commercial applications. Supplier disclaims all express and implied warranties and liability in connection with any use of this
product in any non-commercial applications or in any application that may expose the product to conditions that are outside of the tolerances provided in its specification.
便携式数字数据采集系统(PDDAS)使用了LabVIEW实时模块和PXI,以控制风洞测试和采集记录来自128个不同通道的空气压力数据 "通过LabVIEW实时模块,可以在各种操作情况下获得采集空气压力数据及向风洞提供反馈控制信号所需的确定性响应时间。" – Dave Scheibenhoffer, G Systems 挑战: 用一个可采集、分析和存储来自下一代喷气式战斗机引擎设计的动...[详细]