P-Nu MicroSat Satellite Platform
Robust and scalable microsatellite bus (up to 500 kg) with 3-axis stabilization, station-keeping propulsion, and LEO optimization for constellation deployment.
Technical specifications
- Platform mass
- Up to 500 kg
- Mission lifetime
- Up to 5 years
- Pointing accuracy
- Up to 0.1°
- Stabilization
- 3-axis stabilized
- Propulsion
- Orbit station keeping
- Solar arrays
- Spacecraft solar arrays (body-mounted and deployable)
- Orbit
- LEO-optimized
About
The P-Nu is Dhruva Space’s MicroSat-class satellite platform, the largest in the Dhruva family, supporting platform masses up to 500 kg. It is designed for demanding LEO Earth observation and communications constellation applications, multi-payload configurations, and payloads requiring station-keeping propulsion. The P-Nu features 3-axis stabilization with up to 0.1° pointing accuracy, body-mounted and deployable spacecraft solar arrays, and a 5-year nominal mission lifetime. Pre-qualified and pre-assembled for streamlined payload integration.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
