PDHT Payload Data Handling and Transmission

  • Status
    Completed
  • Status date
    2025-05-20
  • Activity Code
    5D.035
Objectives

The objective of this activity is to develop and verify an Engineering Model (EM) and an Engineering Qualification Model (EQM) of a new payload for LEO satellites for high-speed downlink to ground based on the DVB-S2X standard. Key features of the payload are:

  • High-speed input data interfaces (multiple 10 Gbps interfaces)
  • High-capacity data storage (~3.8 TB)
  • High-capacity downlink (>5 Gbps downlink rate)
  • Support transmission bandwidth up to 1.4 Gsps / 1.5 GHz
  • Integrated 10W Ka-band transmitter.
Challenges

Key challenges in the project are:

  • Selection and implementation of Field-Programmable Gate Array (FPGA) based processing platform
  • Find and qualify suitable devices for high-capacity data storage
  • Find and qualify suitable Ka-band high power amplifier (HPA)
  • Mechanical design - including heat transfer, and tolerance to required vibration and shock levels
  • Hardware and firmware tolerance to radiation levels in LEO
  • Power efficient design
  • Characterisation of power amplifier and proper control of Output Back-Off for relevant modulation schemes.
Benefits

The PDHT combines high storage capacity with ultra-fast downlink speed, higher than existing payloads available on the market.

Features
Image of the product. Image credit: ESA

Product features:

  • DVB-S2X downlink
    • Baud rates up to 1400 Megasymbols per second (Msps)
    • Data rates up to 5 Gbps
    • Adaptive Coding and Modulation (ACM)
  • Fully in-orbit reprogrammable payload where algorithms and air interface can be updated
  • High-capacity data storage (~3.8 TB)
  • Multiple 10 Gbps fibre interfaces for data input
  • CoaxPress interface for data input from camera
  • Option for Controller Area Network (CAN) or RS-485 interface to On-Board Charger (OBC)
  • Redundant interfaces.
System Architecture

The figure below shows how the PDHT payload is connected to other units on the satellite platform.

Diagram of the system architecture. Image credit: ESA

 

Plan
  • Kick off: March 2021
  • Preliminary Design Review (PDR): September 2021
  • Critical Design Review (CDR): May 2023
  • Test Readiness Review (TRR): November 2023
  • Test Review Board (TRB): March 2025
  • Final Review (FR): May 2025.
Current status

The final review of the project was held in May 2025.

Prime Contractor