Oxford Space Systems / January 2026

Wrapped‑Rib:
designed on Earth,
proven in orbit.

Mechanical Design Lead for the deployable X-band antenna now operating aboard SSTL’s CarbSAR spacecraft.

Mission profile

Industry
Space since 2016
Discipline
Mechanical + systems
Registration
CEng / IMechE
Location
Greater Oxford
Selected work

01 / Selected work

Spacecraft mechanisms, robotics, embedded control and representative test hardware.

Astroscale2022—Present
01

COSMIC Mission

Active Debris Removal

Lead mechanical designer for the COSMIC mission, Astroscale’s spacecraft solution for the UK’s national Active Debris Removal mission, developing rendezvous and proximity operations hardware and robotic-arm technology.

  • Spacecraft design
  • RPO
  • Robotics
  • Analysis
CG image of the COSMIC debris-removal spacecraft above Earth with its robotic arm extended
CG image of COSMIC with robotic arm extended · Image: Astroscale

Mission development / Pre-launch

COSMIC timeline

Phase 0–A Feasibility Study Kick-Off
Phase B Kick-Off
Phase B System Requirements Review
Phase B Preliminary Design Review
Phase 2 Kick-Off
Phase 2 Mid-Term Review
Phase 2 Complete
AstroscaleELSA-M
02

ELSA‑M

Commercial end-of-life servicing

Senior Mechanical Designer for ELSA‑M, developing the spacecraft structural design through Critical Design Review and supporting qualification testing. The 520 kg servicer is now preparing for launch to demonstrate removal of a prepared Eutelsat OneWeb satellite.

  • Structural design
  • CDR
  • Qualification
  • Flight hardware
CG image of the ELSA-M servicer magnetically docked with a client satellite in orbit
CG image of ELSA‑M docking with debris · Image: Astroscale

Mission development / Pre-launch

ELSA‑M timeline

Pre-launch
Phase 1 Kick-Off
Pre-launch
Phase 3 Kick-Off
Phase 4 Kick-Off — flight model AIT
CDR complete
ISAR Aerospace selected for launch
TISICS + AstroscaleRobotic manipulation
03
A multi-jointed robotic arm demonstrating spacecraft capture between two representative satellite structures
Robotic capture testing in a representative spacecraft environment

Airbus · LARAD · RISMA · VISPA

Lightweight robotic arms and capture mechanics

At TISICS, I supported Airbus’s LARAD and RISMA robotic-arm programmes, designing and procuring lightweight metal-matrix-composite components for the manipulators.

Later, at Astroscale, I contributed to VISPA by developing the LAR capture mechanics at the Satellite Applications Catapult’s In-Orbit Servicing and Manufacturing facility.

  • Robotic arms
  • MMC structures
  • Capture mechanisms
  • IOSM
ODIN SpaceIndependent work
04

The Odin Black Box

Supporting flight-software development alongside electronics engineering, mechanical design and purpose-built testbeds. Taking hardware through environmental qualification including vibration, TVAC and EMI testing.

  • Flight software
  • Electronics
  • Testbeds
  • Qualification
Explore ODIN technology
ODIN Black Box connected by cables to a flexible Nano Sensor strip

Hover, focus or tap a node to inspect the hardware · Image and specifications: ODIN Space

AstroscalePrototyping
05

Trade-show and GNC testbed models

Designed and built 3D-printed and scaled servicer and client-spacecraft models for trade-show demonstrations and GNC and computer-vision simulations. In the testbeds, the client models are manipulated using three-axis motorised gimbals that I designed, built and integrated; I also developed the embedded firmware and operator UI used to control them.

King Charles III viewing an Astroscale servicer and client spacecraft model during a mission demonstration
Models that communicate the mission King Charles III speaks with Astroscale about its missions at the official opening of the UK Space and Defence Gateway at Harwell. Image: Astroscale.
  • GNC simulation
  • Computer vision
  • Mechanisms
  • Firmware
  • UI
  • 3D printing

02 / Experience

Astroscale · Didcot

Senior Mechanical Design Engineer

Mechanical design for active debris removal and in-orbit servicing, plus representative test assets and mechatronic sensor-test systems.

Oxford Space Systems · Didcot

Senior Mechanical & Thermal Engineer

Mechanical Design Lead for the Wrapped‑Rib antenna; technical leadership across deployable structures, analysis, qualification planning and customer reviews.

03 / Capabilities

01

Mechanical systems

CAD, mechanisms, drawing to BS 8888, design for manufacture, structural and thermal analysis.

02

Embedded & electronics

Firmware, sensor integration, motor control, PCB-level development and operator interfaces.

03

Test & qualification

Representative testbeds, procedures, vibration, thermal vacuum, EMI and subsystem validation.

04

Technical leadership

Work-package ownership, multidisciplinary reviews, stakeholder trade-offs, mentoring and delivery.

Published research

Co-author, Self-healing of structural carbon fibres in polymer composites, Cogent Engineering 7.1 (2020).

04 / Contact

For spacecraft, robotics, test-system and multidisciplinary engineering conversations, connect with me on LinkedIn.

Connect on LinkedIn