ODALISS
Emxys
ODALISS is a high-performance nanosatellite platform with optical communications, providing all necessary subsystems for space missions, available in 3U and 6U CubeSat sizes.
Key figurescomparable across the catalogue
- Power
- 8 W
- Data rate
- 1,550 Mbps
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Structure material
- 7075 Aluminum Hard Anodized
- Structure architecture
- High-performance architecture for high-speed logic interconnection
- Structure sizes
- 3U and 6U CubeSat
- Intended orbit
- LEO
- Power system
- Modular Li-Ion battery packs
- Solar panels
- 3U and 6U available
- Power
- 8 W
- Peak power (per pack)
- 36 W
- Power profile
- Fully configurable
- Non-regulated bus
- +7.4 V
- Regulated buses
- +5 V, +3.3 V
- ADCS actuators
- 3 Reaction wheels + 3 Magnetorquers
- Attitude determination
- via Sun Sensor and Magnetometer
- Attitude accuracy
- <0.1º
- 3-σ pointing control/ knowledge
- <0.1º/<0.1º
- OBC processor
- dual core CORTEX M4+ CORTEX M7 at 480 MHz
- OBC flash storage capacity
- up to 8 GB
- OBC sdram
- 64 MB
- High-performance payload computer (dipp) processor
- Dual Core ARM A9 + FPGA 28K LGs Fabric
- High-performance payload computer (dipp) flash storage
- up to 256 GB
- High-performance payload computer (dipp) os
- Linux OS
- High-performance payload computer (dipp) programming framework
- High level (Python, Javascript, etc.)
- Logic interfaces
- 10/100 Ethernet, SPI, I2C, UART, RS-485, RS-422, USB, etc.
- TTC transceiver
- on-flight reconfigurable Low-Power VHF-UHF (up to 900 MHz band)
- TTC uplink/downlink
- up to 9.6KB
- Optical communications downlink
- Mechanisms-Free C BAND (1550 nm) Laser transmitter
- Optical communications downlink speed
- up to 500 MBps
- RF data downlink
- S Band SDR Based transceiver
- RF data downlink speed
- up to 6MBps
- S-band antenna
- Patch antenna integrated in solar panel
- TTC antenna
- deployable turnstile monopole, dual dipole configuration, etc.
About
ODALISS is a comprehensive high-performance nanosatellite platform equipped with optical communications, integrating all essential subsystems required to realize a space mission. The platform is built around a high-performance bus that supports data-intensive payloads through a scalable architecture. Its internal bus offers a rich array of logic interfaces and power lines to accommodate demanding applications. ODALISS is designed for data-intensive applications, featuring a high-performance architecture with optical communications downlink. It ensures signal integrity with a double 80-pin rugged backplane optimized for high-speed operations. The platform offers flexibility through a high-density backplane providing a rich logic interface for complex payloads. It allows users to focus on their mission and payloads due to its integrated avionics and supports complex endeavors with the backing of an experienced team. The structure is made of 7075 Aluminum Hard Anodized, with a high-performance architecture for high-speed logic interconnection, and is available in 3U and 6U CubeSat sizes for LEO orbits. The power system includes modular Li-Ion battery packs, 3U and 6U solar panels, 8W nominal power, 36W peak power per pack, a fully configurable power profile, and both non-regulated (+7.4V) and regulated (+5V, +3.3V) buses. The ADCS features 3 reaction wheels and 3 magnetorquers, with attitude determination via a sun sensor and magnetometer, achieving <0.1º attitude accuracy and <0.1º/<0.1º 3-σ pointing control/knowledge. Computers include an OBC based on dual-core CORTEX M4+ CORTEX M7 at 480 MHz with up to 8GB Flash storage and 64 MB SDRAM, and a High-Performance Payload Computer (DIPP) based on Dual Core ARM A9 + FPGA 28K LGs Fabric, up to 256 GB Flash storage, powered by Linux OS with high-level programming frameworks (Python, Javascript, etc.). It offers a rich set of logic interfaces including 10/100 Ethernet, SPI, I2C, UART, RS-485, RS-422, USB, etc. Communications include a TTC based on an on-flight reconfigurable Low-Power VHF-UHF transceiver (up to 900 MHz band) with up to 9.6KB uplink/downlink, a data downlink via optical communications based on a mechanisms-free C BAND (1550nm) Laser transmitter with up to 500 MBps downlink, and an RF data downlink via an S Band SDR Based transceiver (up to 6MBps). It also integrates an S-Band Patch antenna in the solar panel and offers TTC antenna options like deployable turnstile monopole and dual dipole configuration.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.