A compact bracket, clamp, and fine-tuning screw enable wide and precise antenna angle adjustment while reducing assembly and transport burden.
Deployable beams and tension members form a lightweight 3D antenna structure that preserves shape accuracy while enabling omnidirectional detection.
A semi-rigid deployable reflector uses retained strain energy to form a precise cylindrical parabolic surface for large-aperture, high-frequency links.
A source follower circuit offsets varactor leakage current to hold bias and threshold voltage without larger capacitors or higher refresh rates.
A gimbaled dual-sided deployable panel combines solar power collection and RF reflection to save spacecraft volume while supporting simultaneous use.
Foldable AESA panels form a hemispherical array that cuts mobile satcom setup time and supports GEO, MEO, and LEO links.
String-coupled element holders keep deployable satellite antenna elements at fixed intervals for stable radio transmission and compact storage.