Its self-pressurizing design simplifies satellite architecture, while an advanced propellant management system ensures reliable, on demand thrust.With precise, throttleable thrust, Sharanga provides superior control for attitude correction, orbit changes, and formation flying, all within a lightweight, low-power package perfect for CubeSats and small satellites.

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Use cases: orbit‑phasing, collision avoidance, formation control, de‑orbit.

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It addresses the challenges of traditional propulsion systems by offering a compact design capable of milli-newton class thrust for quick attitude corrections and precise maneuvers required in ISR and swarm missions. Its unique reactive vapor phase eliminates the need for complex pressurization systems, reducing overall costs while delivering efficient, adjustable thrust for extended mission durations and advanced satellite operations.Recently, we did the flight-testing of its engineering turned into a qualified/flight model at IN-SPACe facility in Ahmedabad with a pure success rate.