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.