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ACT4489DF

Description
DATACOM, MIL-STD-1553 DATA BUS TRANSCEIVER, DFP36, DFP-36
CategoryWireless rf/communication    Telecom circuit   
File Size545KB,7 Pages
ManufacturerCobham Semiconductor Solutions
Download Datasheet Parametric View All

ACT4489DF Overview

DATACOM, MIL-STD-1553 DATA BUS TRANSCEIVER, DFP36, DFP-36

ACT4489DF Parametric

Parameter NameAttribute value
MakerCobham Semiconductor Solutions
Parts packaging codeDFP
package instructionDFP,
Contacts36
Reach Compliance Codeunknown
Is SamacsysN
JESD-30 codeR-XDFP-F36
Negative supply voltage rating-12 V
Number of functions1
Number of terminals36
Maximum operating temperature125 °C
Minimum operating temperature-55 °C
Package body materialUNSPECIFIED
encapsulated codeDFP
Package shapeRECTANGULAR
Package formFLATPACK
Certification statusNot Qualified
Maximum seat height4.445 mm
Nominal supply voltage12 V
surface mountYES
Telecom integrated circuit typesMIL-STD-1553 DATA BUS TRANSCEIVER
Temperature levelMILITARY
Terminal formFLAT
Terminal pitch2.54 mm
Terminal locationDUAL
Base Number Matches1
Standard Products
ACT4489 Dual Transceiver
for MIL-STD-1553A/B, MIL-STD-1760 & SAE-AS15531
www.aeroflex.com/Avionics
February 24, 2005
FEATURES
Small size, light weight and low power dissipation dual transceiver
+5V / ±12V DC power supply operation
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
DSCC Standard Microcircuit Drawing (SMD): Pending
GENERAL 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 the smallest
package with lower pin count for those designs with less board space. 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.
Each channel of the dual transceiver is completely separate from the other and fully independent. This includes
power leads as well as signal lines. Hence, each channel may be connected to a different data bus with no interaction.
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 Volts 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 Volts P-P and reject signals less than 0.6
Volts 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. If unused, a 2K pull-up to +5 Volts
is recommended.
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