CAVU Aerospace UK

External magnetic-isolation board on OBC-Cube-Polar

The Standard version of OBC-Cube-Polar 1G Ethernet outputs is implemented as compact capacitively-coupled Ethernet interfaces from 10/100/1000 voltage-mode copper PHYs. If the satellite platform requires galvanic isolation, the clean solution is to add a small external magnetic-isolation adapter connected to J3/J4. The OBC PCB itself does not need to be enlarged or re-laid out. For this situation we have an adapter add-on card. The proposed adapter is a passive interface board. It does not require an additional active Ethernet PHY or switch IC. The active Ethernet PHY remains on the OBC; the adapter board adds the isolation magnetics and the final satellite-bus connector interface.

Existing OBC interface at J3/J4

Each of J3 and J4 carries one 1G Ethernet MDI interface using four differential pairs. The pin allocation is shown below and is repeated for both Ethernet ports.

MDI pair

Positive pin

Negative pin

Pair A

Pin 1: A_P

Pin 9: A_N

Pair B

Pin 3: B_P

Pin 11: B_N

Pair C

Pin 5: C_P

Pin 13: C_N

Pair D

Pin 7: D_P

Pin 15: D_N

Unused / no connection

Pins 2, 4, 6, 8, 10, 12, 14

Connector on OBC

Nano-D 15-way

J3 = Ethernet 1, J4 = Ethernet 2

OBC connector part

A29100-015

Mating connector

A28000-015

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J3/J4 Ethernet Nano-D pinout reference.

External magnetic-isolation adapter concept

Item

Description

Input side

Two connectors mate to OBC J3 and J4. These carry the four MDI pairs for Ethernet 1 and Ethernet 2.

Isolation stage

Two single-port Gigabit Ethernet magnetics/transformer modules are fitted on the mini-board: one for Ethernet 1 and one for Ethernet 2.

Output side

Two isolated Ethernet output connectors are provided for connection to the satellite bus or harness.

Connector options

The satellite-side connector type is selectable. The board can use Nano-D, Micro-D, RJ45 for lab/GSE use, or a mission-specific connector, subject to mechanical and harness constraints.

Mounting

The adapter can be shaped to mount close to the OBC, on the OBC stack, or elsewhere nearby in the satellite, subject to harness length and mechanical constraints.

 

Candidate magnetics / transformer options

The adapter board can be built using either of the following candidate single-port Gigabit Ethernet magnetics modules, or an equivalent device selected against the final isolation, temperature, mechanical, and procurement requirements:

Candidate device

Type

Use on adapter

Notes

WE-749023015

Single-port 1000BASE-T LAN magnetics / transformer module

One per Ethernet port

Candidate part.

Pulse HX5120NLT

Single-port 1000BASE-T LAN magnetics / transformer module

One per Ethernet port

Candidate low-profile SMT part.

 

Note: These are passive magnetics, not active PHY chips. Therefore, the board does not add another Ethernet controller; it only adds the isolation transformer function, common-mode/noise control, termination/protection, and the required output connectorization.

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Functional arrangement of the external magnetic-isolation adapter.

Electrical topology

 

The adapter implements the following functional path for each Ethernet port:

 

OBC PHY → J3/J4 MDI pairs → adapter input connector → Gigabit Ethernet magnetics → isolated output connector → satellite bus/harness

 

  • The OBC Ethernet PHY is a 10/100/1000 voltage-mode copper PHY operating in SGMII-to-copper mode from the PolarFire SoC GEM MAC.
  • The four MDI pairs from J3/J4 are carried to the adapter board as controlled 100-ohm differential pairs.
  • The magnetics provide the galvanic isolation boundary between the OBC-side Ethernet domain and the satellite-side Ethernet harness/interface.
  • The termination, shield, ESD, and connector-shell treatment on the output side can be adapted to the satellite grounding and EMC approach.
  • The mini-board can be made as a compact passive board and mechanically fixed close to the OBC to minimize the non-isolated MDI extension length.
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Example single-port magnetics schematic block for one J3/J4 Ethernet interface.