http://www.alliedcomponents.com/RJ45_pdf/ARA065-0402_.pdf

RoHS
Single Port RJ45 CONNECTOR
WITH INTEGRATED MAGNETICS,TAB DOWN
10/100 Base-T Ethernet Application
Meets IEEE 802.3 & ANSI X 3.263 standards
Impedance: 100OHMS
Transmit open circuit inductance (OCL): 350uH (MIN) @100KHz,0.1VRMS with 8mA DC Bias
Rise Time: 2.5 nano-seconds from 10 to 90 percent
Always EU RoHS/ELV Compliant, wave solder capable to 265°C
RJ45 jack cavity conforms to FCC rules and regulations Part 68, SUB Part F
Standard operating temp: 0ºC to +70ºC (see footnote)
Industrial operating temo: -40ºC to +85ºC (see footnote)
Electrical Specifications @ 25°C
Part
Number
OCL(uH min)
@100KHz/0.1V
wi/ 8mA DC Bias
Turns Ratio
chip: cable
(±3%)
EMI
Fingers
LED
(L/R)
ARA065-0402_
350
1CT:1CT
NO
NO
Return Loss
(dB Min)
Insertion Loss
(dB Max)
0.5-100MHz
0.5-30MHz
30.1-60MHz
60.1-80MHz
1.1
18
18-20*LOG(f/30)
12
Electrical Specifications @ 25°C
Part
Number
Cross talk
(dB Min)
CMRR
(dB Min)
0.5-40MHz
0.5-40MHz
0.5-100MHz
35
33-20*LOG(f/50)
30
ARA065-0402_
HI-Pot
(VDC)
2250
All specifications subject to change without notice.
*Complete part number by inserting “S” for Standard Temp. or “I” for Industrial Temp.
MECHANICAL
Unless otherwise specified all tolerances are: ±0.25 in mm
21.35 [0.841]
ARA065-0402_
16.00(0.630)
3.5 [0.138]
RJ8
13.5 [0.531]
RJ1
ALLIED
ARA065-0402_
YYWW
2.54 [0.100]
6.35 [0.250]
10.8 [0.425]
714-665-1140
3.05 [0.120]
ALLIED COMPONENTS INTERNATIONAL
REVISED
1501/06/11
www.alliedcomponents.com
RoHS
Single Port RJ45 CONNECTOR
WITH INTEGRATED MAGNETICS,TAB DOWN
SCHEMATICS
ARA065-0402_
1CT:1CT
1CT:1CT
Notes:
1.R1-R4=75OHMS,1/16W,5%Resistors.
2.C1=1000pF,2KV,Decouping Capacitor.
PCB LAYOUT
Unless otherwise specified all tolerances are: ±0.05 in mm
ARA065-0402_
15.75 [0.620]
8.89 [0.350]
PCB Layout
6.35 [0.250]
11.43 [0.450]
3.05 [0.120]
8.89 [0.350]
1.27 [0.050]
MATERIALS
Housing: PBT, Flammability Rating 94V-O.
Shell: C2680 Brass, 0.20mm thick, 50u" Min nickel plating.
Mod Jack Contacts: Phosphor Bronze, 0.35mm thick, 6u" Gold plated.
714-665-1140
ALLIED COMPONENTS INTERNATIONAL
15
REVISED 01/06/11
www.alliedcomponents.com