SC-Sat1a Introduction

3U CubeSat “SC-Sat1a”


SC-Sat1a is a 3U-sized CubeSat developed by Space Cubics Inc. for the purpose of long-term orbital demonstration of its space computer, the SC-OBC Module A1. It is equipped with two SC-OBC Module A1 units.

Satellite Overview


Item Content
Satellite Name SC-Sat1a
Sibling Satellite SC-Sat1
Mission In-orbit verification of the space computer SC-OBC Module A1
Dimensions 3U CubeSat (10 x 10 x 34 cm)
Weight Approx. 3kg
Inter-component Communication Bus Controller Area Network (CAN)
Inter-component Communication Protocol The Cubesat Space Protocol (CSP)
Developing Company Space Cubics Inc.

Subsystems

Power System


Item Content
Power Control Board EPS manufactured by NanoAvionics
Battery Type Lithium-ion battery
Battery Rated Voltage 7.2V
Battery Capacity 72Wh
Solar Cell Type GaAs
Solar Cell Area (per side) 180cm²
Maximum Solar Cell Output (per side) 7W

Communication System


Main Transceiver

Item Content
Transceiver SRS-3 manufactured by Satlab
Communication Frequency Band S-band
Maximum Uplink Data Rate 128kbps
Uplink Modulation Scheme GMSK
Maximum Downlink Data Rate 512kbps
Downlink Modulation Scheme GMSK
Power Consumption (Receive Standby) 550mW
Power Consumption (Transmit/Receive) 5.0W
Maximum Transmit Output 1W
Antenna Type Circularly Polarized Patch Antenna
Maximum Antenna Gain (Main Radiation Direction) Approx. 6.0dBi

Sub Transceiver

Item Content
Communication Frequency Band S-band
Maximum Uplink Data Rate 4kbps
Uplink Modulation Scheme PCM-PSK-PM
Maximum Downlink Data Rate 64kbps
Downlink Modulation Scheme BPSK
Power Consumption (Receive Standby) 2.0W
Power Consumption (Transmit/Receive) 5.0W
Maximum Transmit Output 66mW
Antenna Type Circularly Polarized Patch Antenna
Maximum Antenna Gain (Main Radiation Direction) Approx. 4.5dBi

Control and Data Handling (CDH) System


Item Content
CDH OBC SC-OBC Module A1 + I/O Board
External I/O CAN (Main Component Bus)
RS485 (Sub Transceiver)
PWM (Magnetorquer)
I2C (Temperature Sensor, Magnetometer, SUN Sensor)
GPIO (DSW, etc.)

Attitude Determination and Control System (ADCS)


Item Content
ADCS OBC SC-OBC Module A1 + ADCS Board
GNSS Receiver Supported Satellites: GPS, GLONASS, Galileo, BeiDou, QZSS, NavIC, SBAS
GNSS Antenna Dual Patch Antenna, Gain: 4.5dBic
IMU 3-axis Accelerometer, 3-axis Gyroscope
SUN Sensor Standard Accuracy (No Correction): ±1° ~ ±4°
3-axis Magnetometer Measurement Range: ±8 Gauss, Resolution: 0.25mG
3-axis Magnetorquer Dipole Moment: X/Y Axis 0.30Am², Z Axis 0.34Am²
3-axis Reaction Wheel -

Structure System


Item Content
Material AL5052
Surface Treatment (Rail Surface) Hard Anodizing
Surface Treatment (Other) Alodine Treatment

Propulsion System


None

Camera


Item Content
Camera Control OBC Raspberry Pi Zero 2 W
Camera Module Global Shutter, RGB, 2.3MP

Flight Software


Ground Stations


Contracted with two ground stations:

Mission Control System (MCS)


Launch Plan


Item Content
Rocket Company Space One Inc.
Planned Rocket Kairos Rocket Vehicle 3
Launch Site Spaceport Kii
Orbit Sun-Synchronous Orbit
Orbital Altitude 500km
Scheduled Launch Date February 25, 2026

Gallery

Mission Patch


Development Work


Vacuum Test

FM


EM

Vibration Test

RF Test


3D Shape Measurement