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GEOOSC

Geostationary Orbit Debris Slots Clearance

GEOOSC Logo
GEOOSC Logo

Geostationary Orbit Debris Slots Clearance

Explore the Mission

Our Team

Meet the talented engineers and scientists behind the GEOOSC mission, working together to clear debris from geostationary orbit.

Team Leader
Ziyad AlShamrani

Ziyad AlShamrani

Computer Engineering, Team Leader

  • Defined overall system architecture and data flows
  • Integrated subsystems (power, comms, control, payload)
  • Established I²C/SPI bus protocols and error-handling
  • Coordinated cross-discipline milestones and deliverables
  • Designed, implemented, and integrated the CubeSat embedded systems
Nawaf AlDowayan

Nawaf AlDowayan

Computer Science

  • Developed LiDAR preprocessing, 2D clustering for obstacle avoidance
  • Integrated YOLOv8-based object detector for debris identification
  • Implemented real-time path-planning on Raspberry Pi
  • Built web dashboard for ground-station telemetry and commands
Asim AlZahrani

Asim AlZahrani

Electrical Engineering

  • Designed power budget: solar array sizing, MPPT charger, battery pack
  • Engineered voltage regulation and power-distribution PCB
  • Defined S-band ground-station link budget and comms protocol
  • Validated in-orbit telemetry uplink/downlink reliability
Elyas AlHabub

Elyas AlHabub

Computer Engineering

  • Wrote embedded firmware for ESP32-S3 and Pi Zero sensor hubs
  • Implemented PID-based attitude control via reaction wheels
  • Developed robotic-arm drive code and valve actuation routines
  • Managed command/data packet formatting and CRC checks
Mohammed Muqahhis

Mohammed Muqahhis

Aerospace Engineering

  • Sized and optimized monopropellant thruster via rocket-equation analysis
  • Performed FEM thermal/structural simulations on engine mounts
  • Generated propulsion tank and feed-line CAD and drawings
  • Verified ∆V requirements for GEO-graveyard transfer
Mohammed AlBssiri

Mohammed AlBssiri

Aerospace Engineering

  • Created 12U structural frame CAD with titanium Al-7075 geometry
  • Selected materials, defined fillets and tolerances for launch loads
  • Produced manufacturing drawings (A3 walls, thruster mounts)
  • Conducted vibration and modal analysis per CubeSat standards

Project Overview

Our mission is to develop a sustainable solution for removing debris from geostationary orbit, ensuring the safety and longevity of vital space infrastructure.

Background & Motivation

Geostationary orbit is now clogged with defunct satellites and fragments, threatening vital communications and broadcast platforms. GEOOSC deploys a CubeSat constellation to safely capture and escort 990 kg of end-of-life debris into a dedicated graveyard orbit.

Objectives & Deliverables

  • • Thrust-optimized propulsion for 250 kg per CubeSat
  • • S-band comms with 15 min real-time telemetry uplinks
  • • AI-powered object detection (≥ 90% accuracy)
  • • Robotic arm for secure attachment
  • • Autonomous navigation & obstacle avoidance
  • • Flight-ready prototype demonstration

Design & Development

We used Quality Function Deployment (QFD) to align customer needs—size, cost, reliability—with technical specifications. The final design integrates propulsion, robotics, LiDAR, and on-board AI into a single compact CubeSat.

Final Design & Results

Our design achieves a 3 km/s rendezvous, matches the target velocity, and delivers > 100 N thrust per CubeSat. All performance metrics meet or exceed specification.

Prototype Verification

Lab tests show 95.4% detection accuracy (mAP@0.5) and 355 ms inference time; telemetry latency under 0.1 s—comfortably in the real-time regime.

Conclusions & Next Steps

GEOOSC paves a cost-effective path to GEO debris mitigation. Next: hardware miniaturization, extended mission duration, and constellation scaling.

Contact Us

Have questions about our mission or interested in collaboration? Reach out to the GEOOSC team.

Email Us

For inquiries, feedback, or collaboration opportunities

geoosc0@gmail.com

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