We reject the "Paper Rocket" approach. Hydra is built on an "Earned Ascent" roadmap—validating physics at every step.
Each phase is independently valuable, flight-test driven, and designed to retire specific technical risks before progressing to higher-energy regimes.
Subscale, uncrewed flight demonstrator designed to validate core guidance, navigation, and control (GNC) architectures, autonomy supervision, and marine-to-air transition dynamics.
Focused on hardware-in-the-loop testing, envelope expansion, and data collection to retire control-law and integration risk prior to larger-scale vehicles.
Medium-scale uncrewed demonstrator intended to mature propulsion integration, staging concepts, and high-energy ascent profiles relevant to two-stage-to-orbit (TSTO) architectures.
Utilizes assisted takeoff and staged ascent techniques to validate operational concepts, structural margins, and thermal environments applicable to future orbital systems.
Conceptual system architecture representing a scalable, sea-based launch platform optimized for high-mass logistics and responsive access applications.
Incorporates hydrodynamic lift, modular staging, and reusable structural elements to explore pathways for increased payload mass fraction, operational cadence, and cost efficiency.
Hydra uses Two-Stage-to-Orbit (TSTO) logic.