SC-Sat1: Introduction to SC-Sat1a

3U CubeSat “SC-Sat1a”


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

Satellite Overview


Item Details
Satellite Name SC-Sat1a
Sister Satellite SC-Sat1
Mission In-orbit operation verification of the spaceborne computer SC-OBC Module A1
Form Factor 3U CubeSat (10 x 10 x 34 cm)
Weight Approx. 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 manufactured by NanoAvionics
Battery Type Lithium-ion
Battery Rated Voltage 7.2V
Battery Capacity 72Wh
Solar Cell Type GaAs
Solar Cell Area (per side) 180cm2
Max Solar Cell Output (per side) 7W

Communication System


Main Transceiver

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

Sub Transceiver

Item Details
Transceiver DSTRX-3 manufactured by DST Technology
Communication Frequency Band S-band
Max Uplink Data Rate 4 kbps
Uplink Modulation Scheme PCM-PSK-PM
Max Downlink Data Rate 64 kbps
Downlink Modulation Scheme BPSK
Power Consumption (Receive Standby) 2.0 W
Power Consumption (Transmit/Receive) 5.0 W
Max Transmit Power 66 mW
Antenna Type Circularly Polarized Patch Antenna
Max Antenna Gain (Main Lobe) Approx. 4.5 dBi

Control (CDH) System


Item Details
OBC for CDH SC-OBC Module A1 + I/O Board
External Interfaces CAN (Main inter-component bus)
RS485 (Sub transceiver)
PWM (Magnetorquer)
I2C (Temperature sensor, Magnetometer, SUN sensor)
GPIO (DSW, etc.)

Attitude Determination and Control (ADCS) System


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

Structure System


Item Details
Manufacturer Task Inc.
Material A5052
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, 2.3 MP

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 No. 3
Launch Site Kii Spaceport
Orbit Sun-synchronous Orbit
Orbit Altitude 500 km
Planned Launch Date February 25, 2026

Related Pages

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