Image Details
Caption: Figure F1.
Schematic layout of the GECAM-C (HEBS) payload on the SATech-01 satellite. The HEBS instrument is designed with a two-compartment structure to maximize its FoV. The red arrows indicate the two main components: the top and bottom domes, which collectively form the primary structure of the HEBS payload and house its detector units. The payload coordinate system (xp, yp, zp) is also shown for reference.
© 2026. The Author(s). Published by the American Astronomical Society.