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.
Key figurescomparable across the catalogue
- Mass
- 1 kg
- Design life
- 5 years
- TRL
- 9
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- 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.