P-DoT CubeSat Satellite Platform
Dhruva Space
TRL-9 CubeSat bus (0.5U to 12U) for LEO missions, pre-qualified for payload integration with 3-axis stabilization and up to 5-year mission lifetime.
Typed specifications7 values
Discloses 3 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 1–24 kg product page
- Design lifetime
- 5 years max · product page
- Form factor
- 0.5U product page 12U
- Orbit
- LEO product page
- Attitude control
- 3-axis stabilised product page
- Pointing accuracy
- 0.1 ° max · 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 supplier8 lines, in the manufacturer's own wording
- Form factor
- 0.5U to 12U CubeSat
- Platform mass
- 1–24 kg
- Mission lifetime
- Up to 5 years
- Pointing accuracy
- Up to 0.1°
- Stabilization
- 3-axis stabilized
- Solar arrays
- Body-mounted and deployable
- TRL
- 9 (space-qualified, Thybolt mission)
- Orbit
- LEO-optimized
About
The P-DoT (Polaris Demonstrator of Technologies) is Dhruva Space’s CubeSat-class satellite platform, covering form factors from 0.5U to 12U with platform mass from 1 to 24 kg. Developed indigenously and verified to TRL 9 through the Thybolt mission aboard ISRO PSLV-C54, the P-DoT is LEO-optimized and scalable for Earth observation constellations. It supports multi-payload configurations with body-mounted and deployable solar arrays, 3-axis stabilization for advanced missions (pointing accuracy up to 0.1°), and up to 5-year nominal mission lifetime. Pre-qualified, pre-assembled (mechanical and electrical), and ready for payload integration. Suitable for M2M, IoT, and technology demonstration applications.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.