A constellation of small satellites uses MIMO radar to form a large virtual antenna aperture.
An inflatable capture veil resolves deployment complexity by using pneumatic expansion to stabilize a large flexible membrane for orbital debris removal.
Synchronized satellite formations eliminate interferometric phase errors from drifts, enabling high-precision terrain altitude measurement.
Reverse time heat equation isomorphism optimizes satellite effect delivery schedules through variable separation and candidate solution filtering.
Elastic retaining ring secures waveguides via annular grooves, eliminating screw-nut systems to reduce mass and assembly time.