Launch Systems TRIZ Cases
- Fiber-Reinforced HTS Structures to Prevent Cracking During Calcination
Continuous SiC-like fibers reinforce brittle HTS during calcination and crystallization, reducing oxidation, contamination, and cracking.
- Inflatable Space Enclosures for Adjustable Gravity Activities
An inflatable spacecraft enclosure creates a pressurized activity volume with UAV support, enabling sports and events under adjustable gravity and aerodynamics.
- Fiber-Reinforced HTS Coils to Prevent Calcination Cracking
Continuous coated fibers reinforce brittle HTS coils while limiting oxidation contamination and cracking during high-temperature calcination.
- Fiber-Reinforced HTS Tethers for Brittle Superconductor Forming
Continuous fibers reinforce brittle HTS tethers, preventing cracking and contamination while enabling practical shapes and lower-cost production.
- Fiber-Reinforced HTS Structures to Prevent Sintering Contamination
Continuous long fibers reinforce HTS shapes while preventing sintering contamination and agglomeration, reducing cracking and easing manufacture.
- Fiber-Reinforced HTS Compositions for Crack-Resistant Shaping
Continuous fibers reinforce brittle HTS materials, preventing contamination and cracking while enabling shaped superconducting components.
- Fuel Tank Baffle Petal Layout for Residual Fuel Dumping
Segmented baffle petals keep residual fuel near the sump and dump tube during deceleration, enabling controlled dumping in reusable launch vehicles.
- Electromagnetic Linear Driver
An electromagnetic captured-armature driver repositions payloads without propellant, reducing vibration damage in orbital maneuvers.