Cosmonautic Radiation Protection TRIZ Cases
- Inflatable Space Enclosures for Low-Gravity Activities
Deployable pressurized membranes create reconfigurable low-gravity venues in space, with drones and wireless power supporting events.
- Deployable Laser Shield Vehicle for Adaptive Satellite Protection
A repositionable shield vehicle uses reflective and ablative layers to block live laser threats and protect satellites with continuous coverage.
- Multilayer Insulation Reuse for Satellite Deorbiting Drag
By detaching MLI layers to act as drag flaps and expose the structure, this case deorbits satellites without added deorbit hardware.
- Spacecraft Protective Blanket Using Carbon Nanotube Composites
Multi-layer blankets with carbon nanotube composites reduce spacecraft mass while protecting against debris and electromagnetic interference.
- Starshade Assembly Using Tensegrity Truss and Segmented Petals
Segmenting the starshade into separate petal assemblies and a fan-fold covering reduces deployment complexity while enabling larger blocking areas.
- Diatom-Inspired SiC/SiOx Heat Shield for Re-entry Radiation Reflection
Quasi-periodic diatom pores in a silicon carbide and silica composite reflect re-entry radiation, reducing thermal loading on the heat shield.
- Composite Radiation Shield Using Polymer-Bound Hydrides
Polymer-bound hydride composites absorb high-energy particle radiation while maintaining structural integrity and preventing material degradation.
- Flexible Fuel Containers and Androgynous Coupling for Spacecraft Refueling
Flexible containers store propellant in space while androgynous coupling structures enable docking between spacecraft.
- Multi-axis Articulated Solar Light Shade for Space Sensors
An articulated sunshade with a partial conical baffle tube and pivotable visor shields sensors from solar glare without requiring spacecraft maneuvers.
- Hollowed Asteroid Spacecraft Shielding
A hollowed asteroid spacecraft uses pulverized material curtains for radiation protection.
- Co-cured Multi-Functional Protective Assemblies for Aerospace Structures
A co-cured protective assembly merges radiation, ballistic, and thermal layers into a single composite structure bonded to aerospace vehicles.
- Modular CubeSat Avionics with Stackable Connectors
Stackable connectors join parallel circuit boards in a modular chassis, reducing development complexity for diverse CubeSat missions.
- Variable Emissivity Perovskite Coatings for Spacecraft Thermal Control
Perovskite oxide coatings replace heavy mechanical louvers by dynamically shifting emissivity at critical temperatures, reducing weight and power consumption.
- Deployable Shield for Directed-Energy Weapon Protection
Hinged spokes reposition a reflective shield between the vehicle and incoming laser threats, resolving static protection limitations.
- Oriented Wire Electrostatic Radiation Protection for Spacecraft
Oriented wire electrostatic radiation protection deflects solar particles via charged conductors, replacing massive physical barriers to reduce spacecraft mass.
- Dynamic Magnetic Field Shield for Spacecraft Radiation Protection
Dynamic magnetic field shields deflect high-energy particles via perturbed structures, reducing power consumption compared to static fields.
- Open-Sided Spacecraft Central Cylinder Mass Reduction
A spacecraft central cylinder serves as the sole closed cross-section while open sides remove redundant structural mass.