Pallada Microsatellite Platform
SPUTNIX
Microsatellite bus for spacecraft of 80–200 kg, providing service systems and accommodation for a wide range of payloads independent of the target-instrument configuration. Designed for high-resolution Earth observation and other LEO missions.
Typed specifications23 values
Discloses 4 of 7 fields engineers filter by in this category (category median 3).
- Data interface
- SpaceWire high speed data exchange onboard bus with service systems and… · datasheet p.3 CAN low speed control onboard bus with service systems and payloa… | LVDS
- Design lifetime
- 3 years min · active lifetime, not less than · datasheet p.3
- Orbit
- LEO LEO, circular, altitude 500-800 km · datasheet p.3
- Max payload mass
- 100 kg max · mass of payload, up to · datasheet p.3
- Regulated voltages for the payload
- 27 V nom. · onboard supply voltage 27 V ±2% (power supply system) · datasheet p.3
- Power generation (orbit average)
- 500 W max · average PSS capacity, up to · datasheet p.3 1 000 W max · peak; maximum PSS capacity, up to 1 000 W
- Attitude control
- 3-axis stabilised ADCS in 3-axis mode · datasheet p.3
- Pointing accuracy
- 0.05 ° max · orientation maintenance ±0,05°, 3-axis mode, absolute relativ… · datasheet p.3
- Propulsion
- optional platform allows placing additional systems: propulsion system… · datasheet p.2
- Payload data downlink rate
- 800 000–1 500 000 kbps X-band 8000-8100 MHz, DVB-S2; determined by the capabilities … · datasheet p.3
- Radio band
- S onboard TM/TC system 2000-2200 MHz · datasheet p.3 X payload data to ground receiving complex 8000-8100 MHz, DVB-S2
- Subsystems included
- ADCS ADCS, 3-axis mode · datasheet p.3 X-band downlink interface with ground payload data receiving complex, 8000-81… | OBC onboard computing complex | S-band radio onboard TM/TC system, 2000-2200 MHz | EPS power supply system (PSS) +1
- Max satellite wet mass
- 80–200 kg mass of spacecraft, in total: 80..200 kg · datasheet p.3
- Satellite class
- microsat 10-100 kg 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
- Platform class
- Microsatellite bus, 80–200 kg spacecraft
- Orbit
- LEO, 500–800 km
- Design lifetime
- ≥ 3 years
- Platform mass (instruments)
- ≤ 120 kg
- Payload mass
- ≤ 80 kg
- Supply voltage
- 27 V
- Solar array power (max)
- up to 500 W
- Average orbital power
- up to 250 W
- TT&C (S-band)
- 1 / 0.5 Mbit/s, CCSDS
- Payload downlink (X-band)
- up to 1500 Mbit/s, DVB-S2
- ADCS
- 3-axis; pointing ±0.05°, attitude determination ≤ 30″, stabilization ±0.001°/s
- Interfaces
- SpaceWire, CAN 2.0B, LVDS
About
Microsatellite bus for spacecraft of 80–200 kg, providing service systems and accommodation for a wide range of payloads independent of the target-instrument configuration. Designed for high-resolution Earth observation and other LEO missions.
Documentation
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