HARDWARE / PRODUCTUpdated 24 Jul 2026

METEORITE Satellite Bus

Moog Space Defense Group
METEORITE Satellite Bus

METEORITE is Moog’s purpose-built small satellite bus targeting ESPA rideshare and dedicated launches into LEO, MEO, and GEO orbits. The platform carries up to 220 kg payload with 150 W average and 2 kW peak power, supplied from body-mounted and deployable solar panels feeding an unregulated 28 VDC bus. Attitude control achieves better than 60 […]

Typed specifications22 values

Discloses 5 of 7 fields engineers filter by in this category (category median 3).

Mass
120 kg
bus dry mass · datasheet p.2
Envelope (L×W×H)
22 x 28 x 23.65 in
bus volume, height or radial direction if on ESPA · datasheet p.2
Power consumption
2 000 W
product page
Data interface
SpaceWire
2 x SpaceWire · datasheet p.2 LVDS GPS 1PPS via LVDS
Radiation tolerance (TID)
25.5 krad
total dose with 0.200 in Al shielding · datasheet p.2
Design lifetime
2 years
min · mission life 2-5 years, depends on orbit · datasheet p.2 5 years max · mission life 2-5 years, depends on orbit
Export status
EAR
falls under the jurisdiction of the EAR · datasheet p.2
Orbit
LEO
500 to 1200 km · datasheet p.2
Max payload mass
220 kg
datasheet p.2
Power available to payload
150 W
example OAP payload power, orbit and mission dependent · datasheet p.2 2 000 W peak payload power, orbit and mission dependent
Unregulated bus for the payload
28 V
nom. · 28 [25/33] VDC unregulated, multiple 1.2 A switches · datasheet p.2
Attitude control
3-axis stabilised
reaction wheels and torque rods · datasheet p.1
Pointing accuracy
0.017 °
max · pointing accuracy, 1 sigma · datasheet p.2
Attitude knowledge
0.011 °
max · attitude knowledge telemetry accuracy, 1 sigma · datasheet p.2
Propulsion
included
green propulsion system · datasheet p.1
Delta-v
175 m/s
min · with 200 kg dry mass · datasheet p.2
Payload mounting
22 in x 28 in flat deck, up to 30 in height for ESPA launch or more for dedicated small launch
datasheet p.2
Material (as printed)
all aluminum structure
datasheet p.1
Satellite class
ESPA-class
datasheet p.1

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 supplier16 lines, in the manufacturer's own wording
Orbital range
500–1200 km LEO, MEO, GEO (ESPA class)
Mission life
2–5 years
Bus dry mass
120 kg
Payload mass capacity
220 kg
Dimensions
22 × 28 × 23.65 inches
Delta-v
>175 m/s at 200 kg dry
Payload power (average)
~150 W
Payload power (peak)
2 kW
Supply voltage
28 VDC unregulated (25–33 V range)
Pointing accuracy
<60 arcsec (1σ)
Jitter / stability
<10 arcsec
Max slew rate
2.5 deg/sec
Radiation tolerance
25.5 kRad TID at 0.200 in Al shielding
Position knowledge
<4 m
Propulsion
Moog ASCENT green monopropellant (AF-M315E)
Cpu
Moog BRE440 radiation-hardened processor

About

METEORITE is Moog’s purpose-built small satellite bus targeting ESPA rideshare and dedicated launches into LEO, MEO, and GEO orbits. The platform carries up to 220 kg payload with 150 W average and 2 kW peak power, supplied from body-mounted and deployable solar panels feeding an unregulated 28 VDC bus. Attitude control achieves better than 60 arcsec (1σ) pointing accuracy with less than 10 arcsec stability and jitter, with a maximum slew rate of 2.5 deg/sec. The baseline propulsion uses Moog’s ASCENT green monopropellant system delivering more than 175 m/s delta-V at 200 kg dry mass. Avionics are built around Moog’s BRE440 radiation-hardened CPU. Total bus dry mass is 120 kg within a 22 × 28 × 23.65 inch envelope. Position knowledge is better than 4 m. The METEORITE bus supports 2–5 year mission life in the 500–1200 km altitude range with 25.5 kRad total dose tolerance at 0.200 inch aluminum shielding.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: www.moog.com ↗

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