Artificial Satellites TRIZ Cases
- Debris Capture Pouch with Aerogel Core
A semi-penetrable pouch envelops a particle-absorbing core to fracture and trap orbital debris, preventing secondary collision risks from expelled fragments.
- Satellite Control Spacecraft Debris Removal via Magnetic Capture
A satellite-control spacecraft captures orbital debris using a robotic arm and applies a magnetic control medium for precise manipulation.
- Modular Spacecraft Bus with External Docking for Payload Replacement
Segmented spacecraft buses supply power and thermal management to dockable payloads, reducing orbital debris by enabling component replacement.
- Multipoint Payload Release System With Networked Firing Control
Networked firing control units address hold-down release mechanisms via a shared interface bus for selective payload deployment.
- Distributed Space Traffic Management System for Collision Avoidance
A distributed space traffic management system coordinates multiple devices to share orbital data and perform danger analysis.
- Electrostatic Actuation for Gravity Sensor Test Mass Control
Segmented actuators and feedback loops capture test masses without physical contact, preventing collisions during gravitational wave observations.
- Hybrid Lunar Sensor for Cislunar and Surface Monitoring
A hybrid sensor system monitors cislunar space and the lunar surface using dynamic operational modes, resolving complexity from distinct instruments.
- Satellite Orbit Normal Estimation via Magnetic Field Rotation
A satellite device estimates orbit normal using Earth magnetic field measurements and rotation speed data for accurate attitude control.
- Spacecraft Mating Mechanisms Soft Hard Capture
Soft and hard capture elements align spacecraft while cup-cone interfaces resist external forces during docking operations.
- Decentralized Modular Space Body Architecture
Decentralized control units in interchangeable space modules eliminate central bottlenecks and reduce redundant system complexity.
- Unfolding Rolled Hollow Member via Root Expansion Mechanism
Rotating winding core unfolds elongate hollow member while expansion mechanism moves second shell half away from root to expand cross-section.
- Inflatable Spacecraft Carrier Module Design
An inflatable spacecraft carrier provides a spacious internal environment for servicing multiple vehicles in orbit.
- Satellite Drag Flap Atmospheric Density Measurement
Deployable drag flap subjects satellite to aerodynamic torque, enabling real-time density estimation without expensive ground-based tracking systems.
- Magneto-coupler Stabilizes Rotating Space Debris
Launched magneto-couplers stabilize rotating space debris by reducing angular velocity, enabling safe capture without collision risk.