dhruva-space

Launch provider India Verified
6 Products
14 Years Active
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About dhruva-space

Dhruva Space Private Limited is an Indian national-award-winning space technology company founded in 2012 and headquartered in Hyderabad, Telangana, providing full-stack space engineering solutions encompassing satellite platforms, launch services, and ground station network infrastructure. The company manufactures satellite bus platforms (P-DoT, P-30, P-Nu) across multiple mass classes and produces the DSOD series of satellite deployers.

Dhruva Space operates AstraView, an Earth observation imagery service delivering high-resolution imagery for agriculture, infrastructure monitoring, and environmental applications. The company's ground station infrastructure spans multiple frequency bands, complemented by an international presence through Dhruva Space GmbH in Graz, Austria. With over 200 staff and a 28,000 sq ft facility currently expanding to 280,000 sq ft, the company is scaling rapidly to meet growing demand.

Dhruva Space serves communications, IoT, Earth observation, climate monitoring, and national security applications, positioning itself as a comprehensive partner for satellite missions requiring both spacecraft development and operational infrastructure. The company's integrated capabilities — from satellite design through launch services and ground operations — make it a rare one-stop solution provider in India's emerging commercial space sector.

Capabilities

Launch vehicles 2

Products

6

TRL 9 · Flight-proven

Space-qualified CubeSat orbital deployers (1U, 3U, 6U, 12U, 16U) with non-pyrotechnic HDRM, onboard telemetry sensors, and ISRO PSLV flight heritage.

1 6
TRL 9 · Flight-proven

Compact and modular nanosat bus (20–50 kg) with TRL 9 and flagship hosted-payload capability for IOD/IOV missions up to 12U payloads in LEO.

1 10
TRL 9 · Flight-proven

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.

1 8

Robust and scalable microsatellite bus (up to 500 kg) with 3-axis stabilization, station-keeping propulsion, and LEO optimization for constellation deployment.

1 7

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