Cosmonautic Ground Equipments TRIZ Cases

Composite compartments, straps, and cushioning protect heavy satellite terminal parts from air-drop shocks and speed deployment in remote locations.

High-momentum synchrotron photons replace linear motor acceleration to push launch objects beyond the 7 km/s orbital-speed limit.

Magnetic levitation and acceleration launch an aerospace vehicle horizontally, cutting vertical launch risk while supporting reusable boosters and orbiters.

Telescoping planks and rotating supports let one service platform fit different launch vehicle shapes, cutting reconfiguration time and crane risk.

Energetic welding anchors landing supports to floating platforms on touchdown, stabilizing rocket stages without manual securing.

An electromagnet, weight body, and drive line stabilize normal and abnormal rocket umbilical retrieval while preventing launch damage.

Foldable wings and a rotating propulsion boom let this eVTOL shift between vertical and horizontal flight without fixed skyport infrastructure.

Microbead-filled vacuum rigidizing walls conform around satellite equipment to limit low-gravity movement and absorb launch vibration.

An articulated eVTOL skyboom carries personal vehicles through vertical-to-horizontal flight without full skyport infrastructure, easing congestion and access limits.

A mobile container unit combines drum storage, metered peroxide delivery, and ultrapure water rinsing to enable safe rocket refueling without fixed HTP infrastructure.

Vacuum-deployable microbead structures conform around satellite equipment to prevent floating and absorb transport vibrations.

Floating-platform movement and wind can destabilize landed rocket stages; an energetic stud anchors the support element rapidly.

A sealing faceplate applies touch-up coating to targeted surface areas without masking, reducing surface damage and hazardous waste.

A sealed faceplate applies touch-up coating precisely without masking, while collecting excess material to limit surface damage and hazardous waste.

See how a sealed faceplate applies coating precisely without masking, limiting surface damage and collecting excess from rocket-body touch-up work.

A sealed faceplate applies touch-up coating without masking, protecting surfaces and collecting excess material to reduce hazardous waste.

Four rope groups and movable wheel sets form a Z-shaped capture net that intercepts rocket case bodies while reducing traction force and work.

Pneumatic, magnetic, and electrostatic stages separate lunar ice from regolith without energy-intensive thermal extraction.

Electromagnetic release and gravity retrieval simplify launch vehicle umbilical recovery.

A launcher, capsule, and receiver recover kinetic energy during low-gravity cargo transfer for habitat and mining power.

Distance sensors guide movable support pads to track the rocket trajectory, preventing structural damage from misalignment.

Automated coordination system determines safe launch windows using real-time orbital and airspace data feeds.

A reusable launch vehicle propulsion unit cradle positions all fluid and electric links on a single removal plane for simplified maintenance.

A standalone ground-based apparatus cushions landing impact and channels hot exhaust gases away, reducing booster weight and fuel requirements.

Movable gantries receive space rockets via spreadable arms, eliminating uncertain touchdown and falling risks from direct leg landings.

Replacing high-strength tethers, an inflatable tube leverages pneumatic wind forces to support its own weight and eliminate extreme material requirements.

Connected flying vehicles leverage the Coanda effect to reduce fuel consumption and gravitational drag during atmospheric payload delivery.

A control system monitors real-time LNG composition and density during launch vehicle fueling to calculate precise mass targets.

A centrifugal launch system uses a vacuum chamber and rotating tether to accelerate payloads to high speeds.

Water buoyancy accelerates the launch vehicle, reducing propellant mass and logistical costs for orbital insertion.

Removable thrust chamber units resolve reusability trade-offs in rocket-powered launch systems.

Federated architecture processes airspace and orbital data to resolve infrastructure complexity while ensuring safe passage.

A reusable space plane launch vehicle uses magnetic levitation to reach hypersonic speeds while scavenging thermal energy from atmospheric shockwaves.

A vertical tower filled with water lifts vehicles using buoyancy forces.

Telescoping poles and cables stabilize upright rockets on ships, reducing lateral loading risks.

A flexible recovery fixture engages a rocket capture device above the center of gravity to enable vertical landing.

Pneumatic and magnetic separation isolates ice from regolith, reducing mining power by 98.3% and avoiding heavy vehicle transport risks.

A propulsion stage shifts its center of mass by displacing a current storage device to control flight attitude during descent.

Radial and peripheral cables constrain a rocket engine diverging section during ignition to prevent structural deformation.

A micro-fusion engine harnesses cosmic rays and muons to generate braking thrust for spacecraft deceleration.

A magnetic anchor landing system secures aerospace vehicles using electromagnetic clamping forces on the substrate.

Interchangeable modular rooms attach to a common portal, enabling quick adaptation to different launch vehicles without disrupting launch cadence.

A fueling connector employs a breakable link and lever to unlock mating parts during liftoff, eliminating manual disconnection delays.

Segmented cutting and socket modules access single-use valves, extending satellite operational life by 3 to 5 years.

Rotating tether mechanism accelerates payloads via centrifugal force in a vacuum, reducing propellant needs and launch costs.