SC-Sat1: SC-Sat1a Introduction

3U CubeSat “SC-Sat1a”


SC-Sat1a is a 3U-sized CubeSat developed by Space Cubics Inc. for the 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 Details
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 Approximately 3 kg
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 Details
Power Control Board EPS by NanoAvionics
Battery Type Lithium-ion
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 Details
Transceiver SRS-3 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 Power 1W
Antenna Type Circularly Polarized Patch Antenna
Maximum Antenna Gain (Main Radiation Direction) Approximately 6.0dBi

Sub Transceiver

Item Details
Transceiver DSTRX-3 by DST Technology
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 Power 66mW
Antenna Type Circularly Polarized Patch Antenna
Maximum Antenna Gain (Main Radiation Direction) Approximately 4.5dBi

Control and Data Handling (CDH) System


Item Details
OBC for CDH SC-OBC Module A1 + I/O Board
External Interfaces 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 Details
OBC for Attitude Control 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 -

Structural System


Item Details
Manufacturer Task Inc.
Material A5052 Aluminum Alloy
Surface Treatment (Rail Surface) Hard Anodizing
Surface Treatment (Other) Alodine Treatment

Propulsion System


None

Camera


Item Details
OBC for Camera Control 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 Details
Rocket Company Space One Inc.
Planned Rocket KAIROS Rocket Flight 3
Launch Site Space Port 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

Fit Check with POD

Launch Site Work

Final Stowage into POD

Installation Inside Fairing