AvioNForge1553
| Channels | 1 channel, dual-redundant Bus A / Bus B |
|---|---|
| Modes | BC / RT / BM; single- or multifunction operation |
| Data rate | MIL-STD-1553A/B · 1 Mbps |
| Host interfaces | 10/100BASE-T Ethernet + USB 2.0 High-Speed |
| Power | 5 V DC via USB-C; bus-powered |
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ALVEXIS / AvioNForge
AvioNForge
Avionics interfaces and integration test hardware
Connect MIL-STD-1553 and ARINC-429 systems to Ethernet and USB. Interface and coupling hardware for bus monitoring, protocol conversion and laboratory integration.
Choose your interface
AvioNForge429
| Channels | 2 TX + 4 RX · ARINC-429 |
|---|---|
| Data rate | 100 kbps / 12.5 kbps |
| Host interfaces | 10/100BASE-T Ethernet + USB 2.0 High-Speed |
| Power | 5 V DC via USB-C; bus-powered |
Programmable label filtering
Datasheet · English PDF ↓
AvioNForge1553 Bus Coupler
| Coupling | Two transformer-coupled stub connections |
|---|---|
| Termination at each bus end | 78.7 Ω |
| Isolation resistors | 59 Ω |
| Transformer ratio | 1:1.41 |
| Power | Passive; no external power |
AvioNForge1553 Direct Coupled Bench
| Coupling | Direct-to-transformer coupled test interface |
|---|---|
| Data rate | MIL-STD-1553A/B · 1 Mbps |
| Stub length | Direct-coupled stubs up to 30 cm; BC / RT / BM test equipment |
| Power | Passive; no USB, Ethernet or external power |
For development, monitoring and test integration. Select bus topology, coupling, termination and software for the application. These specifications do not imply aircraft airworthiness approval or completed system certification.