BAE Systems Satellite Platform P10
In Space Missions
A compact spacecraft solution designed for payload accommodation flexibility at an affordable price with full redundancy.
Typed specifications48 values
Discloses 5 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 140 kg max · datasheet p.2
- Envelope (L×W×H)
- 0.9 x 0.9 x 0.9 m Stowed Spacecraft · datasheet p.2 0.9 x 0.9 x 0.9 stowed spacecraft (LxWxH) | 0.9 m x 0.9 m x 0.9 m Stowed Spacecraft Dimension (LxWxH)
- Data interface
- CAN Payload Interfaces · datasheet p.2 RS-422 Payload Interfaces: RS422 | RS-422 Payload | CAN payload interface | LVDS Payload Interfaces +3
- Design lifetime
- 5 years Low Earth Orbit · datasheet p.2 5 years mission lifetime, LEO 400-600 km
- Orbit
- LEO Low Earth Orbit; altitude 400-600 km; inclination 0° to 97.8° · datasheet p.2
- Max payload mass
- 35 kg Payload Mass Capability · datasheet p.2 35 kg max · Payload Mass Capability
- Payload envelope (L × W × H)
- 0.7 x 0.7 x 0.40 m Payload Volume Capability (LxWxH); hemispherical open concept… · datasheet p.2 0.7 x 0.7 x 0.40 Payload Volume Capability (LxWxH)
- Power available to payload
- 13 W min · BOL OAP, Nadir pointing (>13W) · datasheet p.2 20 W min · BOL OAP, Sun Pointing (>20W)
- Regulated voltages for the payload
- 3.3 V Regulated payload switch voltage · datasheet p.2 5 V Regulated payload switch voltage | 12 V Regulated payload switch voltage
- Unregulated bus for the payload
- 28 V nom. · unregulated, ±4V · datasheet p.2 28 V ±4V | 28 V nom. · Unregulated: 28V (±4V) payload switch voltage
- Onboard storage for payload data
- 2 048 GB On Board Storage · datasheet p.2
- Power generation (orbit average)
- 33 W min · OAP, Nadir (>33W); 500km SSO with 10:30 LTAN · datasheet p.2 48 W min · OAP, Sun Pointing (>48W); 500km SSO with 10:30 LTAN
- Battery capacity
- 432 Wh 28V (±4V) · datasheet p.2
- Attitude control
- 3-axis stabilised Stabilisation Method 3-axis; Nadir, Sun, and Inertial Pointin… · datasheet p.2
- Pointing accuracy
- 0.16 ° datasheet p.2
- Attitude knowledge
- 0.05 ° datasheet p.2
- Propulsion
- included Electric Propulsion; total impulse 15 kNs; thrust 10μN to 1mN · datasheet p.2
- Delta-v
- 107 m/s Propulsion dV · datasheet p.2
- Payload data downlink rate
- 512 kbps S-Band Command and Telemetry downlink (uplink 128 kbps) · datasheet p.2 150 000 kbps X-Band High Speed Downlink
- Radio band
- S Command and Telemetry · datasheet p.2 X High Speed Downlink
- Subsystems included
- X-band downlink 150 Mbps · datasheet p.2 ADCS 3-axis stabilisation | battery 432 Wh 28V | S-band radio Command and Telemetry S-Band | propulsion Electric Propulsion +1
- Max satellite wet mass
- 140 kg max · Max Wet Spacecraft Mass (Platform, Payload, Propellent) · datasheet p.2
- Satellite class
- smallsat 100-500 kg very capable small satellite · 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 supplier1 lines, in the manufacturer's own wording
- Payload Mass
- 35 kg
About
The BAE Systems satellite platform P10 is a compact spacecraft solution designed for payload accommodation flexibility at an affordable price with full redundancy. The P10 is a very capable small satellite, offering a rapid schedule to meet demanding mission requirements. Key features include its compact design and payload flexibility at an affordable price. This platform is ideal for missions requiring a small satellite with efficient payload integration and a quick turnaround.
Documentation
- Satellite-Platform-P10-FS-Oct2024.pdf PDF source: in-space.co.uk ↗
- Satellite-Platform-P20-FS-Oct2024.pdf PDF source: in-space.co.uk ↗
- Satellite-Platform-P30-FS-Oct2024.pdf PDF source: in-space.co.uk ↗
Need the full ICD, test reports or a specific revision? Ask the supplier directly.