Inflatable Antennas TRIZ Cases

Shape memory composite elements let small-satellite antennas stow compactly for launch and deploy in orbit while preserving omnidirectional communication.

An inflatable Cassegrain antenna with phased beam steering enables high-resolution SAR on sub-100 kg microsatellites at lower cost.

Shape memory composites, an inflatable envelope, and a degradable layer enable compact launch stowage and reliable antenna deployment on small satellites.

Flexible conductive inflatable antennas cut weight and setup time while maintaining RF performance for portable field communications.

Inflation-assisted deployment and shape memory composites let small satellites stow a larger antenna and retain omnidirectional communication.

A degradable support layer protects a stowed shape-memory antenna during launch, then breaks down in orbit to cut mass after deployment.

An inflatable bladder locks AMC layer spacing during deployment, enabling a foldable antenna that preserves directivity with easier transport.

A motor-tracked phased-array antenna keeps moving vehicles aligned to LEO and MEO satellites, improving signal quality and channel-bonded capacity.

A motor-actuated phased-array antenna tracks satellites during vehicle motion to improve signal quality and bond channels for higher data capacity.

A foldable thin-film satellite structure combines antennas and solar cells to cut mass and volume while simplifying deployment.

An inflatable bladder latches a deployable AMC antenna at a fixed FSS spacing, cutting stowed thickness while preserving directivity.

An inflatable bladder sets and latches AMC ground plane spacing, making low-frequency antennas thinner, portable, and easier to deploy.

Tensioned flexible bracing limits transverse mast motion, improving deployed positioning precision, rigidity, and stress resistance.

A degradable support layer and shape memory composites help space antennas survive launch deployment, then shed mass in orbit.

An inflatable bladder latches a flexible AMC antenna at a fixed FSS spacing, enabling thin stowage with maintained directivity after deployment.

External stays unwound from reels stiffen an inflatable satellite mast and guide uniform deployment under thermal and motion-induced strain.

A conductive hollow tube guides liquid flow through a grounding conductor to enable efficient high-frequency power supply.

Fluidized membranes deploy rigid support structures post-launch, resolving the contradiction between compact satellite volume and high-gain antenna performance.

Inflatable membrane expands flexible antenna from flat stored configuration to conical deployed shape, resolving volume constraints in small satellites.