QV-Feed

- Q/V-Band Feed System

STATUS | Completed
STATUS DATE | 05/12/2022
ACTIVITY CODE | 5C.326
QV-Feed

Objectives

The objective of this project is to design, build and test a Q/V-band Feed System EQM (Engineering Qualification Model) so that this technology is qualified for flight use on future GEO VHTS systems.
This project draws on the successful development of a Feed System EM (Engineering Model) through a previous ARTES 5.2 programme.
The Feed System EM is shown in Figure 1.

<em>Figure 1. Feed System EM</em>

This product’s primary use is for gateway feed chains in multi-spot beam antennas on board geostationary VHTS systems. The usage of the Q/V-band on the gateway link frees up spectrum on the Ka-band user links. With the exception of the mission specific filters and feed horns, these feeds are generic and can be adapted for different missions. An example Q/V-band gateway coverage is shown in Figure 2.

<em>Figure 2. Q/V-band gateway coverage</em>

 

Challenges

The Q/V-band Feed System has to be a slim-line design:

  • compatible with up to 7 feeds and 30mm spacing between feeds with suitable mechanical interfaces in a feed cluster.

  • covering the complete Q Tx, Q Rx and V Rx bands

  • operating in dual circular polarisation over all frequency bands

  • capable of handling maximum RF power levels without risk of multipaction

  • exhibiting low PIM performance over temperature

  • compatible with the envisaged thermal and vibration environment at component level as well as Feed System level

  • achieving required RF performance across multiple builds

System Architecture

A generic wideband feed architecture has been selected for this EQM feed development. This comprises of a wideband feed horn, wide band polariser, wide band OMT, and a pair of triplexers to accommodate the most challenging filter frequency plan, as shown in Figure 3.

<em>Figure 3. Generic wideband feed architecture</em>

 

Plan

Phase 1: KO to PDR 
Preliminary design phase includes activities to validate key technologies used in EQM. PIM test requirements are defined.

Phase 2: PDR to CDR
Detailed design and analyses performed. Plans defined for PIM tests.

Phase 3: CDR to TRR
EQM components are manufactured. Components and sub-assemblies undergo RF health checks before full Feed System is assembled and RF tested.

Phase 4: Final Review
Feed System EQM is subjected to qualification testing (thermal cycling, vibration, power handling and PIM tests). Test reports are included in FR documentation.

Current Status

Phase 4 completed.

Flight qualification of the Q/V-band Feed System is complete.