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HI-8596PSTF
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FabricantHolt circuits intégrés
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Pièce fabricant #HI-8596PSTF
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Fiche technique HI-8596PSTF DataSheet
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En stock17776
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Spécifications
| Attribut | Valeur |
| EU RoHS | Compliant |
| ECCN (US) | 7A994 |
| Part Status | Active |
| HTS | COMPONENTS |
| Automotive | No |
| PPAP | No |
| Minimum Operating Temperature (°C) | -55 |
| Maximum Operating Temperature (°C) | 125 |
| Mounting | Surface Mount |
| Package Height | 1.25 |
| Package Width | 3.9 |
| Package Length | 9.9 |
| PCB changed | 16 |
| Standard Package Name | SO |
| Supplier Package | SOIC N |
| Pin Count | 16 |
| Lead Shape | Gull-wing |
| Maximum Supply Current (mA) | 40 |
| Number of Transceivers | 1 |
| Power Supply Type | Single |
| Supplier Temperature Grade | Extended |
| Function | Line Transmitter |
| Receiver Signal Type | Differential |
| Minimum Single Supply Voltage (V) | 3 |
| Typical Single Supply Voltage (V) | 3.3 |
| Maximum Single Supply Voltage (V) | 3.6 |
| Number of Transmitters | 1 |
| Transmitter Signal Type | Differential |
| Number of Drivers per Line | 1 |
| Number of Transmitter Enables | 1 |
| Data Transmission Topology | Point-to-Point |
| Process Technology | CMOS |
| Driving Mode | 3-State |
Présentation
Description
Equivalent
1. DDC BU-63133: Offers similar MIL-STD-1553 transceiver functionality.
2. Holt HI-1585: Another transceiver option for MIL-STD-1553 applications.
3. Aeroflex UT63M125: Provides comparable transceiver features for MIL-STD-1553.
These alternatives are suitable for applications requiring MIL-STD-1553 communication capabilities. Always verify specific requirements and compatibility with your application before selecting a replacement.
Features
1. ARINC 429 Compliance: It meets the ARINC 429 standards for avionic data transmission, ensuring reliability in data communication.
2. Dual-Channel Operation: The device supports dual-channel output, allowing for simultaneous data transmission on two channels.
3. High Output Driver: It is equipped with high output drive capability to meet the demands of ARINC 429 bus systems.
4. Built-in Test Functionality: The device includes self-test features to ensure proper operation and easy troubleshooting.
5. Wide Temperature Range: It operates efficiently across a broad temperature range, making it suitable for various aerospace environments.
6. Supply Voltage Flexibility: The IC supports a range of supply voltages, providing flexibility in system design.
7. Rugged Design: Designed for the harsh conditions of aviation applications, offering reliability and durability.
These features make it ideal for applications requiring robust data communication in aerospace systems.
Pinout
Functions of each pin include:
1. V+: Positive supply voltage.
2. GND: Ground connection.
3. TXA: Transmitter input A.
4. TXB: Transmitter input B.
5. V-: Negative supply voltage.
6. OUTA: Differential output A.
7. OUTB: Differential output B.
8. N/C: Not connected or used for additional functions in some configurations.
This IC ensures proper signal levels and timing for ARINC 429 communication, crucial for reliable data transmission in avionics systems.