Orbital Debris Capture and Deorbit System for Nanosatellites | Available Intellectual Property | Rensselaer Polytechnic Institute

Orbital Debris Capture and Deorbit System for Nanosatellites

RPI ID: 2018-018-201

Innovation Summary:
This invention provides a system for capturing and deorbiting space debris using a robotic satellite equipped with a debris collection mechanism. The system autonomously identifies, targets, and secures debris objects in orbit, then guides them into a controlled deorbit trajectory. It integrates object recognition, autonomous navigation, and propulsion subsystems. The design is modular and scalable, making it adaptable to a variety of mission profiles and debris types.

Challenges / Opportunities:
Space debris poses a growing threat to satellites and space missions, with limited and costly solutions currently available. Traditional debris removal methods are complex and often require manual intervention. This invention offers a practical, autonomous approach to debris mitigation. It opens opportunities for commercial and governmental space agencies to enhance orbital safety and ensure long-term sustainability of space operations.

Key Benefits / Advantages:
✔ Autonomous operation reduces need for ground control
✔ Modular design adaptable to various debris sizes and orbits
✔ Enhances space traffic safety through collision prevention
✔ Supports sustainable orbit management and long-term space operations

Applications:
• Satellite servicing and debris removal
• Orbital traffic management
• Space sustainability initiatives
• Aerospace defense and security

Keywords:
#spacedebris #deorbitingsystem #autonomoussatellite #orbitalcleanup #spacesustainability

Intellectual Property:
US Issued Patent 12,017,803 B2
Patent Information:
Inventors:
Jackson Lyons
Kurt Anderson
Keywords:
CubeSat
Nanosatellite
Orbital Debris
Space Junk
For Information, Contact:
Natasha Sanford
Licensing Associate
Rensselaer Polytechnic Institute
sanfon@rpi.edu