fumito
August 28, 2025, 6:37am
1
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
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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
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