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.