SS-G3 Sun Sensor
TY-Space TechnologyThe SS-G3 Sun Sensor is a product offered by TY-Space Technology, likely used for attitude determination in space…
59 satellite platforms, components and ground equipment from manufacturers worldwide.
The SS-G3 Sun Sensor is a product offered by TY-Space Technology, likely used for attitude determination in space…
The Pyxis Space Sun Sensor is an ultra-compact, lightweight attitude sensor that provides coarse Sun direction measurement for…
The Nano Sun Sensor on a Chip (NanoSSOC) is a two-axis, low-cost sun sensor known for high accuracy…
The Advanced Coarse Sun Sensor (ACSS) is a highly reliable and radiation-hardened device for sun-tracking and attitude determination…
Miniature, fully autonomous digital sun sensor with <0.02° precision and CubeSat Space Protocol over I2C.
High-dynamic-range sun sensor specifically optimized for GEO operations — wide operating range handling full GEO illumination conditions without…
Ultra-high-accuracy CubeSat sun sensor — 0.0015° precision, 12g, I2C/SPI digital output, ideal for precision pointing missions.
Fine sun sensor for CubeSats and small satellites — 0.09° accuracy, ±60° FOV, 12g, 3.3V supply, digital I2C/SPI…
The AQUILA series sun sensors provide reliable and accurate sun-angle measurements for spacecraft attitude determination and control, suitable…
Small, lightweight single-detector sun sensor with cosine-symmetric field of view for solar-array pointing and sun acquisition.
2-axis, 4-detector pyramid-configuration coarse sun sensor for solar array pointing and sun acquisition.
Self-redundant cosine-response sun sensor delivering reliable wide-angle solar position data for safe-mode operations.
Compact, lightweight version of the Fine Sun Sensor for small satellites and CubeSats requiring precise sun-vector data.
Analogue quadrant-detector sun sensor providing precise two-axis solar aspect angle for yaw steering and earth-pointing missions.
Rugged self-redundant sun sensor delivering coarse solar position data for safe-mode and coarse maneuvering.
Sun sensor for microsatellites and small spacecraft. Half-angle 45° FOV, 0.15° accuracy, 43×43×16 mm, 45 g, CAN2B. Uses…
Two-axis digital sun sensor for nanosatellites. ±60° FOV, <0.3° accuracy, 31.3×27.5×10.3 mm, 7 g, CAN interface. Factory calibrated,…
Self-redundant cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 15 g ultralight, 0 W passive, >100 kRad TID.
These are saved in this browser only. Sign in and they move to your account, where they stay across devices.
We use cookies. Strictly necessary cookies keep the platform working. With your consent we also use Google Analytics to understand how the platform is used and improve it. We do not use advertising cookies. Cookie Policy · Privacy
How is your experience with the platform? Your message goes straight to our team.
Thank you! Your feedback has been sent to our team.