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i-Space recently completed a hot fire test of Hyperbola-3's Second Stage Auxiliary Power System. It features a bi-propellant design with 16 thrusters to handle everything from attitude control to orbit trimming and propellant management for engine restarts to deorbit passivation

59,999 views โ€ข 6 months ago โ€ขvia X (Twitter)

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Advancing LOX/LCH4 Dual-Propellant Cooling for HANBIT-Micro INNOSPACE has successfully completed a series of combustion tests for its upgraded 4 kN-class liquid-methane kick-stage combustor for HANBIT-Micro. ๐Ÿš€ Building on the 237-second long-duration ground test in May 2024, the combustor has been advanced with a Dual-Propellant Regenerative Cooling scheme. ๐Ÿ“ˆ โš™๏ธ Unlike conventional single-propellant regenerative cooling, this approach utilizes both fuel and oxidizer as coolants, enabling: ๐Ÿ”น Reduced feed pressure requirements ๐Ÿ”น Lighter propellant tanks ๐Ÿ”น Lower overall kick-stage mass ๐Ÿ”ฅ By preheating and vaporizing both coolants, the system also achieves: ๐Ÿ”น Improved mixing efficiency ๐Ÿ”น Shorter ignition delay ๐Ÿ”น Enhanced combustion stability and efficiency ๐Ÿ’ก Overcoming High Technical Barriers Most notably, the recent test validated stable regenerative cooling under low-pressure, subcritical conditions โ€” a technically demanding regime โ€” and mitigated the risks associated with using liquid oxygen (LOX) as a coolant. The application of a gasโ€“gas swirl injector further demonstrated improved mixing performance. With this milestone, INNOSPACE continues to advance methane propulsion technology and enhance the maturity of the HANBIT-Micro kick-stage system. Please stay tuned for the next phase of development. ๐Ÿ™Œ #SpaceInnovation #HANBITMicro #KickStage #MethaneEngine #RocketEngineering #SpaceTech

innospacecorp

18,949 views โ€ข 3 months ago