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MIURA 5 tanks in action! Pressurization system stability test under nominal propellant flow conditions, validating control avionics, flight software PID, pressurization and venting systems across Stage 1 and Stage 2 tanks ✅ Next step: full-stage testing.

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PLD Space

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45,118 görüntüleme • 1 ay önce •via X (Twitter)

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Terran R moved closer to flight readiness in April with key integration, test, and launch infrastructure milestones. 🏗️ Build: Stage two integration advanced with avionics, harnesses, valves, and raceways installed. All first stage Aeon R engines for flight one have been manufactured, assembled, and shipped. 🔥 Test: Teams began software run-for-record testing on the completed stage two HITL build, while Aeon V reached key service life milestones during full-duration mission duty cycles. 🌴 Launch: At LC-16, the water tower and lightning protection systems rose as launch site activation work continued across the LOX farm, water systems, and more.
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Terran R build is accelerating across the vehicle and in parallel, production capacity continues to expand with the addition of dozens of new powder bed fusion printers and CNC machines. ✅ Stage 2 downcomer and forward test adapter installed ahead of acceptance testing ✅ Stage 1 fuel tank welding complete, with COPVs installed and barrel painting finished

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From Space Beach and the Space Coast, Terran R hardware and infrastructure are coming to life across design, build, test and launch. 🏭 On the factory floor teams installed the second stage downcomer and forward test adapter on the tank in preparation for acceptance testing, with continued progress on first stage fuel tank build. 🖥️ Teams completed thrust structure hardware-in-the-loop hardware integration, creating a testbed for software, avionics, and partner teams to validate designs and automation before use on the vehicle.

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Our team has started test campaigns on TEPREL-C throttle capabilities to enable future Stage 1 re-entry control. This effort includes testing materials, engine components, and operational sequences to ensure MIURA 5 can perform powered re-entry retro-propulsive manoeuvre prior to landing. These test campaigns have been developed in collaboration with ESA’s FLPP framework contracts and will be progressively implemented in upcoming MIURA 5 flights.

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🔴MIURA 5 Progress Update now live! MIURA 5 is rapidly coming together, with tangible progress across manufacturing, integration, testing and launch infrastructure. All of our team is taking part in the path towards flight readiness: • Manufacturing and integration of the two first MIURA 5 qualification units (QM1 & QM2) in record time to validate the complete subsystem before flight unit production. • Parallel qualification test campaigns, successfully ongoing across all launch vehicle components, from engines to avionics, from software to GNC algorithms. • Ground Support Equipment is being manufactured in Spain and will soon undergo on-site testing, while civil works at our launch complex at CSG (Kourou) moves forward simultaneously. See full content below:
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🔴MIURA 5 Progress Update now live! MIURA 5 is rapidly coming together, with tangible progress across manufacturing, integration, testing and launch infrastructure. All of our team is taking part in the path towards flight readiness: • Manufacturing and integration of the two first MIURA 5 qualification units (QM1 & QM2) in record time to validate the complete subsystem before flight unit production. • Parallel qualification test campaigns, successfully ongoing across all launch vehicle components, from engines to avionics, from software to GNC algorithms. • Ground Support Equipment is being manufactured in Spain and will soon undergo on-site testing, while civil works at our launch complex at CSG (Kourou) moves forward simultaneously. See full content below:

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Great power demands precise control! ⚡️ The Composite Nozzle and Flex Nozzle Control System of Vikram-1's Stage 1 (Kalam-1200) just aced their pre-flight tests. ✅ This "steering system" to thrust vector the rocket is now ready for integration with the motor for the upcoming static fire test. 🔥 #rocketscience #space

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The Terran R program entered a new phase in May as stage 2 rolled out of Long Beach and began its journey to NASA Stennis. 🏗️ Build: Completed stage 2 integration while advancing thrust structure, interstage, and stage 1 qualification hardware. 🔥 Test: Aeon V second stage engine completed its qualification campaign, hitting key service life, duration, and start milestones for flight one. 🌴Launch: Water tower reached its final height at 305 feet; lightning protection system erection continued
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The Terran R program entered a new phase in May as stage 2 rolled out of Long Beach and began its journey to NASA Stennis. 🏗️ Build: Completed stage 2 integration while advancing thrust structure, interstage, and stage 1 qualification hardware. 🔥 Test: Aeon V second stage engine completed its qualification campaign, hitting key service life, duration, and start milestones for flight one. 🌴Launch: Water tower reached its final height at 305 feet; lightning protection system erection continued

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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. 🚀 Building on the 237-second long-duration ground test in May 2024, the combustor has been advanced with a Dual-Propellant Regenerative Cooling scheme. 📈 ⚙️ Unlike conventional single-propellant regenerative cooling, this approach utilizes both fuel and oxidizer as coolants, enabling: 🔹 Reduced feed pressure requirements 🔹 Lighter propellant tanks 🔹 Lower overall kick-stage mass 🔥 By preheating and vaporizing both coolants, the system also achieves: 🔹 Improved mixing efficiency 🔹 Shorter ignition delay 🔹 Enhanced combustion stability and efficiency 💡 Overcoming High Technical Barriers Most notably, the recent test validated stable regenerative cooling under low-pressure, subcritical conditions — a technically demanding regime — and mitigated the risks associated with using liquid oxygen (LOX) as a coolant. The application of a gas–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. 🙌 #SpaceInnovation #HANBITMicro #KickStage #MethaneEngine #RocketEngineering #SpaceTech
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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. 🚀 Building on the 237-second long-duration ground test in May 2024, the combustor has been advanced with a Dual-Propellant Regenerative Cooling scheme. 📈 ⚙️ Unlike conventional single-propellant regenerative cooling, this approach utilizes both fuel and oxidizer as coolants, enabling: 🔹 Reduced feed pressure requirements 🔹 Lighter propellant tanks 🔹 Lower overall kick-stage mass 🔥 By preheating and vaporizing both coolants, the system also achieves: 🔹 Improved mixing efficiency 🔹 Shorter ignition delay 🔹 Enhanced combustion stability and efficiency 💡 Overcoming High Technical Barriers Most notably, the recent test validated stable regenerative cooling under low-pressure, subcritical conditions — a technically demanding regime — and mitigated the risks associated with using liquid oxygen (LOX) as a coolant. The application of a gas–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. 🙌 #SpaceInnovation #HANBITMicro #KickStage #MethaneEngine #RocketEngineering #SpaceTech

innospacecorp

18,949 görüntüleme • 5 ay önce

Archimedes second stage engine full duration burn - complete ✅ (and what a thing of beauty). The AVac (Archimedes Vacuum) engine produces 1.2x lbf of its Stage 1 variant and stands ~2.5m taller thanks to its extended nozzle optimized for the vacuum conditions of space. Recent AVac testing included a stub skirt for the nozzle. Since full length vacuum nozzles at ground level risk flow separation and instability, stub skirts are used to anchor our engineers' analysis for how the engine will perform with the full nozzle in vacuum conditions - all critical preparation for Neutron's first flight.
5:40

Archimedes second stage engine full duration burn - complete ✅ (and what a thing of beauty). The AVac (Archimedes Vacuum) engine produces 1.2x lbf of its Stage 1 variant and stands ~2.5m taller thanks to its extended nozzle optimized for the vacuum conditions of space. Recent AVac testing included a stub skirt for the nozzle. Since full length vacuum nozzles at ground level risk flow separation and instability, stub skirts are used to anchor our engineers' analysis for how the engine will perform with the full nozzle in vacuum conditions - all critical preparation for Neutron's first flight.

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Literally shaking! Behind the scenes of a special test 🚀 Earlier this year, Redshift, our third stage, completed a full vibration test campaign in flight configuration! Unlike isolated component checks, this was the real deal: all systems integrated and tested under simulated launch conditions. Because launch is no gentle ride. Everything must endure intense vibrations and still perform flawlessly. The result? Electronic connections remained strong, the systems (including antennas, telemetry, flight computer, navigation systems) stayed up and running, and we obtained valuable data to further refine and improve. Enjoy this glimpse of Team Redshift and their work behind the scenes, turning challenges into progress, one test at a time!
2:23

Literally shaking! Behind the scenes of a special test 🚀 Earlier this year, Redshift, our third stage, completed a full vibration test campaign in flight configuration! Unlike isolated component checks, this was the real deal: all systems integrated and tested under simulated launch conditions. Because launch is no gentle ride. Everything must endure intense vibrations and still perform flawlessly. The result? Electronic connections remained strong, the systems (including antennas, telemetry, flight computer, navigation systems) stayed up and running, and we obtained valuable data to further refine and improve. Enjoy this glimpse of Team Redshift and their work behind the scenes, turning challenges into progress, one test at a time!

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34,860 görüntüleme • 11 ay önce

Starship Ship 40 is back home in Mega Bay 2 just in time for the weekend after a busy week away at Massey's that included a successful single engine static fire test. We will have watch and see what the next stage for it will be in the pre flight testing ahead of Flight 13 NSF - NASASpaceflight.com |
1:02

Starship Ship 40 is back home in Mega Bay 2 just in time for the weekend after a busy week away at Massey's that included a successful single engine static fire test. We will have watch and see what the next stage for it will be in the pre flight testing ahead of Flight 13 NSF - NASASpaceflight.com |

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13,479 görüntüleme • 1 ay önce