HARDWARE / PRODUCTAdded 22 Jul 2026

ARIETIS-NS 3-Axis Rad-Tolerant Space Gyroscope System

Innalabs
ARIETIS-NS 3-Axis Rad-Tolerant Space Gyroscope System

Space-qualified 3-axis CVG for LEO/GEO/MEO, 30krad TID, ITAR-free, serial production, 16-year lifetime.

Typed specifications9 values

Discloses 4 of 11 fields engineers filter by in this category (category median 3).

Mass
1 200 g
max · product page 2 300 g max
Bias instability
0.1 °/h
max · product page
Angle random walk
0.005 °/√h
max · product page
Power consumption
7 W
max · product page
Operating temperature
-25 °C
product page
Design lifetime
16 years
product page 6 years
Random vibration
18 g RMS
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 supplier21 lines, in the manufacturer's own wording
Measurement range
[-12°/s; +12°/s]
Switch-on response time
≤6 seconds
Angular random walk (ARW)
≤0.005°/√hr
In-run bias stability
≤0.1°/hr
Bias errors (3σ)
≤10°/hr
Scale factor repeatability (3σ)
≤3000 ppm
Radiation TID
30krad (COTS screened)
SEL
SEL-free at 60 MeV
Data interface
RS422 or RS485
Reliability
1000 FIT (FIDES)
Mass (LEO config)
<1.2 kg
Mass (GEO config)
<2.3 kg
Power consumption
≤7 W
Power interface
28 VDC nominal
Operating temperature
-25°C to +65°C
Launch vibration
18 grms
Operational lifetime (flight)
16 years
Operational lifetime (ground)
6 years
ITAR
ITAR-free
TRL
9 (serial production, flight models delivered)
Number of axes
3

About

The InnaLabs ARIETIS-NS is a high-performance, commercial, space-qualified rad-tolerant 3-axis gyroscope system designed for satellite applications across LEO, GEO, and MEO missions. Utilizing screened COTS components to withstand space radiation, it achieves 30krad TID tolerance and SEL-free operation. ITAR-free and currently in serial production with flight models already delivered to customers. Features RS422 or RS485 data interface and 28 VDC power. Available in LEO (<1.2 kg) and GEO (<2.3 kg) configurations. Operational lifetime up to 16 years in flight and 6 years on ground. Supports launch vibration loads up to 18 grms. In-run bias stability ≤0.1°/hr with ARW ≤0.005°/√hr. Switch-on response time ≤6 seconds.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.innalabs.com ↗

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