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ACT4489

Description
MIL-STD-1553 Data Bus Transceiver, PLUG IN-24
CategoryWireless rf/communication    Telecom circuit   
File Size154KB,7 Pages
ManufacturerCobham PLC
Download Datasheet Parametric View All

ACT4489 Overview

MIL-STD-1553 Data Bus Transceiver, PLUG IN-24

ACT4489 Parametric

Parameter NameAttribute value
MakerCobham PLC
package instructionDIP,
Reach Compliance Codeunknown
JESD-30 codeR-XDIP-P24
Negative supply voltage rating-12 V
Number of functions1
Number of terminals24
Maximum operating temperature125 °C
Minimum operating temperature-55 °C
Package body materialUNSPECIFIED
encapsulated codeDIP
Package shapeRECTANGULAR
Package formIN-LINE
Certification statusNot Qualified
Filter levelMIL-STD-883
Maximum seat height5.08 mm
Nominal supply voltage12 V
surface mountNO
Telecom integrated circuit typesMIL-STD-1553 DATA BUS TRANSCEIVER
Temperature levelMILITARY
Terminal formPIN/PEG
Terminal pitch2.54 mm
Terminal locationDUAL
width15.24 mm
Base Number Matches1
Standard Products
ACT4489 Single Transceiver
for MIL-STD-1553A/B, MIL-STD-1760 & SAE-AS15531
www.aeroflex.com/Avionics
May 16, 2005
FEATURES
Small size, light weight and low power dissipation single transceiver
Bipolar supply ±12V, logic supply +5V
Outstanding MIL-STD-1553 / SAE-AS15531 performance
Monolithic construction
Input and output TTL compatible design
Designed for commercial, industrial and aerospace applications
MIL-PRF-38534 compliant devices available
Aeroflex-Plainview is a Class H & K MIL-PRF-38534 manufacturer
DESCRIPTION
The Aeroflex-Plainview ACT4489 is the next generation monolithic transceiver design which provides full
compliance with MIL-STD-1553A/B, MIL-STD-1760 and meets SAE-AS15531 requirements in a small package
with low power consumption. The series performs the front-end analog function of inputting and outputting data
through a transformer to the MIL-STD-1553 data bus.
Design of these transceivers reflects particular attention to active filter performance. This results in low bit and word
error rate with superior waveform purity and minimal zero crossover distortion. Efficient transmitter electrical and
thermal design provides low internal power dissipation and heat rise at high as well as low duty cycles.
TRANSMITTER
The transmitter section accepts bi-phase TTL data at the input and when coupled to the data bus with a 1:1 ratio
transformer the data bus signal is typically 7.0 V
P
-
P
at Point A (See Figure 5). When both DATA and DATA inputs
are held low or high, the transmitter output becomes a high impedance and is “removed” from the line. In addition,
an overriding “INHIBIT input provides for the removal of the transmitter output from the line. A logic “1” applied to
the “INHIBIT” takes priority over the condition of the data inputs and disables the transmitter (See Figure 1
Transmitter Logic Waveform). The Transmitter may be safely operated for an indefinite period with the bus (Point
A) short circuited at 100% duty cycle.
RECEIVER
The Receiver section accepts bi-phase differential data at the input and produces two TTL signals at the output. The
outputs are DATA and DATA, and represent positive and negative excursions of the input beyond a pre-determined
threshold (See Figure 2 Receiver Logic Waveform).
The pre-set internal thresholds will detect data bus signals exceeding 1.20 V
P
-
P
and reject signals less than 0.6 V
P
-
P
when used with a transformer (See Figure 5 for transformer data and typical connections).
A low level at the RX STROBE IN input inhibits the DATA and DATA outputs.
SCD4489 Rev B

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Datasheet   0 1 2 3 4 5 6 7 8 9 A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
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