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Small Satellite Reaction Wheels
Physical
Mass - 90g
Dimensions - 33.4x33.4x31.5mm
Operating temperature - -10°C to 60°C
Vibration - 8.9g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 190mW
Peak power - 2.3W
Communications - I2C/UART/CANPerformance
Speed range - ±6000
Momentum @ max speed - 3.6mNms
Max torque - 2.3mNm
Static imbalance - <0.004 g·cm
Dynamic imbalance - <0.014 g·cm

Small Satellite Reaction Wheels
Physical
Mass - 60g
Dimensions - 28x28x26.2mm
Operating temperature - -10°C to 60°C
Vibration - 14g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 150mW
Peak power - 0.65W
Communications - I2C/UART/CANPerformance
Speed range - ±8000
Momentum @ max speed - 1.77mNms
Max torque - 0.23mNm
Static imbalance - <0.003 g·cm
Dynamic imbalance - <0.005 g·cm

HIGH-PERFORMANCE CHAMELEON CAMERA SYSTEMS FOR CUBESATS

CHAMELEON - MS
Spatial resolution (GSD) at 500 km - PAN 10 m; MS 20 m
Swath at 500 km - 40 km
Mass (Including electronics) - 1.6 kg
Spectral bands - 7 × MS
Satellite Bus Size - Compatible with 3U or 6U
Physical Size - 2 U (10 cm × 10 cm × 20 cm excl. electronics)
(10 cm × 10 cm × 21.5 cm with rear-mounted CU)
Flight Heritage - Flight Model Hyperspectral delivered for 2020 launch
Data format - 8-bit or 16-bit
Integrated mass data storage - 128 Gigabytes
Compression - RAW or J2K lossless or lossy
Data interface - LVDS, SPI, I2C, CAN, RS422
Power Usage - imaging mode: < 10 W; readout mode: < 5 W
Power Supply - 5V DC
Operating temperature - +10˚C to +30˚C
Survival Temperature - -20˚C to +70˚C
Radiation Tolerance (TID) - Tested to 30k Rad

CHAMELEON - HS
Spatial resolution (GSD) at 500 km - Binned to 20 m or 40 m
Swath at 500 km - 20 km
Mass (Including electronics) - 1.6 kg
Spectral bands - 148 × HS
Satellite Bus Size - Compatible with 3U or 6U
Physical Size - 2 U (10 cm × 10 cm × 20 cm excl. electronics)
(10 cm × 10 cm × 21.5 cm with rear-mounted CU)
Flight Heritage - Flight Model Hyperspectral delivered for 2020 launch
Data format - 8-bit or 16-bit
Integrated mass data storage - 128 Gigabytes
Compression - RAW or J2K lossless or lossy
Data interface - LVDS, SPI, I2C, CAN, RS422
Power Usage - imaging mode: < 10 W; readout mode: < 5 W
Power Supply - 5V DC
Operating temperature - +10˚C to +30˚C
Survival Temperature - -20˚C to +70˚C
Radiation Tolerance (TID) - Tested to 30k Rad

Electrical Power Supply system for small nanosatellites

Main Features
Optimal for 1U and 2U platforms
Battery voltage 8V
20 Wh battery onboard
Photovoltaic power conversion up to 30 W
ISS launch compliant version available
Key functionality
3 input channels with independent power point setting
Three different photovoltaic power point options
Battery under-voltage and over-voltage protection
Two regulated power buses
6 user-controlled output switches w. latching current limiter
Discrete control of output switches
Onboard housekeeping measurements
Interface to battery board NanoPower BP4 and BPX
Separation-switch interface with latching mechanism
Remove-Before-Flight-pin interface
Onboard lithium ion battery pack
Onboard microcontroller with I2C interface
CSP network protocol for seamless integration with other GomSpace products

Complete power system for 3U-nanosatellite

The 3U Power Pack includes a power supply, battery pack and full solar panel set for a 3U nanosatellite:

1 NanoPower P31uS
1 NanoPower BP4
1 NanoPower P110UA
1 NanoPower P110UB
1 NanoPower P110UC
1 NanoPower P110A
1 NanoPower P110B
1 NanoPower P110C
4 NanoPower P110AS
4 NanoPower P110BS
Power Harness
Main features:
Photovoltaic power up to 60 W
Two regulated power buses: 3.3V@5A and 5V@4A
Up to six 3.3V@3A outputs
Up to six 5V@3A outputs
Battery capacity: 2600-5200 mAh

Small and powerful battery module for CubeSats

Feautures :
18650 Li-Ion cells with a nominal capacity of 2600 mAh
Two configurations are available:
2P-2S: 6 - 8.4 V & 5.2 Ah
1P-4S: 12 - 16.8 V & 2.6 Ah
Integrated temperature sensors with digital interface
Battery heater
Auxiliary MOSFET switch (e.g. to drive thermal knives for deployables)
Stackable for increased capacity
Fits standard PC104
ISS launch compliant version availabl

Versatile On-board Computer for Cube, Nano and Microsat missions

Feautures :
High-performance AVR32 MCU with advanced power saving features
512 KB build-in flash
128 MB NOR flash (On two dies of 64 MB each)
32 kB FRAM for persistent configuration storage
32 MB SDRAM
RTC clock
On-board temperature sensors
Interfaces:
I2C, UART, CAN-Bus
8 external ADC channels that can also be used as GPIO
External SPI with 3 chip selects
Cubesat Space Protocol (CSP)
GOSH interface for check-out
Attitude control system features:
3-Axis magneto resistive sensor
3-Axis gyroscope
3 bidirectional PWM outputs with current measurements
I2C interface for GomSpace Sensor Bus (GSSB)
Electrical features:
2 x 20-position hard-gold plated FSI one-piece connector

High performing Camera-system for Earth Observation Projects

Feautures :
Integrated System:

Industrial Lens
3-megapixel color sensor
Advanced data processing and storage on-board
Image Acquisition:

1/2" (4:3) format color CMOS sensor
2048 x 1536 pixels
10-bit RGB Bayer pattern
Lens Performance (for each lens version):

8 mm lens: <260 m/pixel from 650 km
35 mm lens: <60 m/pixel from 650 km
70 mm lens: <30 m/pixel from 650 km
400-750 nm spectral transmission
Data Processing:

High performance ARM processor
512 MB on-board DDR2 RAM
2 GB solid state image storage
RAW, BMP and JPEG output format
Interface:

CSP-enable CAN, I2C and TTL level serial interfaces
Serial port with text-based console for debugging
Mechanical Features:

Standard PC/104 size, 96 mm x 90 mm
Mass: from 169 g with the 8 or 35 mm lens
Mass: from 277 g with the 70 mm lens

Reaction wheel for nanosatellites

Main features
Long life brushless motor design
Integrated control electronics
Enclosed design
Hybrid bearings
Lubricant free
Vacuum rated
Long life
Redundant data interfaces
SPI
I2C
UART
Speed and torque control capability
Low jitter with precisely balanced flywheel

Flight-proven Electric Power System (EPS)

Feautures :
Input Channels - 3 (one for each CubeSat axis)
Input Voltage (Per Solar Panel Channel) - up to 5.5 V
Input Current (Per Solar Panel Channel) - up to 1.8 A
Six Connectors For - the solar panels
Integrated Blocking Diode For Each - solar panel connector
Battery Pack Power - 10.2 Wh (20.4 Wh with EPS I Plus)
Battery Pack Voltage - 3.7 V nominal
Mass - 208 g
Stackable Battery Packs - up to 8 A
Output Power Buses - 3.3 V, 5 V, BCR (5 V max) and Battery raw
Interfaces - UART, I2C, USB-C
Switches - Two deployment and one Remove Before Flight (RBF)
Control - Six general purpose outputs for shutdown/reset of external modules
Interfaces - UART, I2C, USB

A flight-proven protoboard

Feautures :
Compatibility - PC104 form-factor
Prototype Area - standard spacing of 2.54 mm (100 mils)
Power - 3.3 V, 5 V and GND pins
Mass - 28 g
PC104 Type - 104 Pins CubeSat Kit Connector
Other Options - Available with machine-soldered 104 Pins Samtec connectors

A hands-on educational kit consisting of two low-power
transceivers and a space simulation board

Feautures :
Operating Frequency Bandwidth - 430-450 MHz (physical)
Links - UHF (physical), S-band and X-band
Losses Physical Simulation - free space and additional (atmospheric, polarization etc.) losses
External Noise - interference and jamming
Frequency Compensation - Doppler effects and transceiver compensation
Configurable - Different modulation schemes, transmission speeds and packet parameters