XDSAT NS
XDLINX Space Labs
6U small satellite platform for EO optical, SAR, SIGINT, IoT and laser payloads with hosted-payload ISR mission support.
Typed specifications9 values
Discloses 1 of 7 fields engineers filter by in this category (category median 3).
- Power consumption
- 126 W product page
- Form factor
- 6U product page
- Payload volume, U
- 4 U product page
- Power generation (orbit average)
- 66 W product page
- Battery capacity
- 126 Wh product page
- Propulsion
- included product page
- Payload data downlink rate
- 500 000 kbps max · X-band downlink · product page
- Radio band
- X product page
- Flight heritage
- Launched 2023 product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier12 lines, in the manufacturer's own wording
- Bus type
- 6U
- Bus os
- Antaris SatOS — distributed compute for bus, payload edge and SDR
- Payload volume / mass
- 4U
- Payloads CAN support
- EO Optical, SAR, Siglnt, IoT, Laser
- Pointing accuracy & stability / orbit knowledge
- ±0.002° (1-sigma), 3 axes, 2 Trackers; 1 arc-sec over 1 sec; 4m, 0.05m/s
- Power storage
- 126 Wh
- Solar panels
- 66 W
- Propulsion
- Multiple Electric & Chemical Propulsion Systems Available
- TT&C, sw update
- Secure & Flexible via S-Band SDR & UHF
- Data downlink
- X-band up to 500 Mbps
- Ground control
- Public or Private GS with Antaris MC Software
- Flight heritage
- Launched 2023
About
XDSAT NS is the smallest member of XDLINX Space Labs’ ready-to-launch XDSAT satellite platform family, built on a 6U bus with 4U of payload volume/mass available for hosted payloads. It runs the Antaris SatOS distributed compute stack across bus, payload edge and SDR, and can support EO optical, SAR, SIGINT, IoT and laser payloads. The platform provides 3-axis pointing accuracy and stability of ±0.002° (1-sigma) with 2 star trackers, orbit knowledge of 1 arc-second over 1 second, and 4 m / 0.05 m/s navigation performance. Power is supplied by 66 W solar panels backed by 126 Wh of storage, with multiple electric and chemical propulsion systems available. TT&C and software updates are handled securely and flexibly via S-band SDR and UHF, with X-band data downlink up to 500 Mbps, and ground control available via public or private ground stations running Antaris mission control software. XDSAT NS has flight heritage from a 2023 launch.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.