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A louder rumble in Rocket City! We just completed our first BE-4 engine hotfire test at the historic Test Stand 4670 in Huntsville. We also continue to test BE-4 engines at our Texas facility. The BE-4 engine produces 550,000 pounds of thrust and is our most powerful engine yet.

Blue Origin

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230,984 görüntüleme • 2 yıl önce •via X (Twitter)

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💪💪💪

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Prodigious! Go Big Blue!

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Starship power raptor engine 🔥

Space By Storm profil fotoğrafı

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Sweet BE4 Heat!!! 😎🚀🔥🔥🔥

💫Shamara💫 profil fotoğrafı

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Look at y’all getting me all worked up in Huntsville! 🚀🔥😉

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Triethylborane?

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2/10 high five execution

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Isn’t the BE-4 a flight proven engine. What’s so special about this test? (Not saying it isn’t awesome)

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Joel Eby2 yıl önce

Crank it up. The big engine has arrived at 4670. Can't tell you how much I love days like this.

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Congrats nice accomplishment.

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Hotfire at our test facility in preparation for testing the new combustion chamber for the next-generation Astra first stage engine that will power Rocket 4.

Hotfire at our test facility in preparation for testing the new combustion chamber for the next-generation Astra first stage engine that will power Rocket 4.

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In a recent hotfire our BE-3U engine reached more than 211,500 lbf thrust. That makes BE-3U the highest thrust-to-weight hydrogen engine in history, at more than 90! Here is the video of that test for your enjoyment.

In a recent hotfire our BE-3U engine reached more than 211,500 lbf thrust. That makes BE-3U the highest thrust-to-weight hydrogen engine in history, at more than 90! Here is the video of that test for your enjoyment.

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What’s hotter than a Texas summer? Our Miranda engine.🔥 We fired our Miranda engine at full power for 226 seconds— that’s almost 4 minutes! This endurance test verifies that the engine can perform beyond the nominal flight duration, meaning this engine is one step closer to being ready for flight. Seven of these Miranda engines will generate the thrust needed to lift our Eclipse rocket off the launch pad and propel it into orbit.

What’s hotter than a Texas summer? Our Miranda engine.🔥 We fired our Miranda engine at full power for 226 seconds— that’s almost 4 minutes! This endurance test verifies that the engine can perform beyond the nominal flight duration, meaning this engine is one step closer to being ready for flight. Seven of these Miranda engines will generate the thrust needed to lift our Eclipse rocket off the launch pad and propel it into orbit.

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Last week, our BE-7 team conducted another successful Thrust Chamber Assembly (TCA) test at NASA Marshall Space Flight Center Test Stand 116. Our tests on an upgraded TCA bring our cumulative test time to more than 4000 seconds, and we are on track in our engine development path.

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Out at the Rocket Ranch, Test Stand 1 is our workhorse - firing at least one engine a day. Hear from the team building and testing our engines so they are ready for launch!

Out at the Rocket Ranch, Test Stand 1 is our workhorse - firing at least one engine a day. Hear from the team building and testing our engines so they are ready for launch!

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Volume on! Yesterday we completed a 60 second hot fire test of our full length Miranda engine! All of which was designed, built, and tested at our Rocket Ranch in Briggs, TX.

Volume on! Yesterday we completed a 60 second hot fire test of our full length Miranda engine! All of which was designed, built, and tested at our Rocket Ranch in Briggs, TX.

Firefly Aerospace

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With rocket engines, boring is good. To that end, please enjoy this 1,030-second (17+ min!) BE-7 engine burn. This test represents the Apogee Raise Maneuver or ARM burn for our Blue Moon Mark 1 Lunar lander, plus margin, the longest burn required by the mission to reach the Moon. You may have noticed that the engine for this test does not have a nozzle. BE‑7 is tested in both vacuum and atmospheric conditions. This test was at GEEx—our atmospheric test position in West Texas.

With rocket engines, boring is good. To that end, please enjoy this 1,030-second (17+ min!) BE-7 engine burn. This test represents the Apogee Raise Maneuver or ARM burn for our Blue Moon Mark 1 Lunar lander, plus margin, the longest burn required by the mission to reach the Moon. You may have noticed that the engine for this test does not have a nozzle. BE‑7 is tested in both vacuum and atmospheric conditions. This test was at GEEx—our atmospheric test position in West Texas.

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January’s GS2 performed remarkably during our inaugural New Glenn launch, delivering our payload to orbit with less than 1% deviation from the target. Today, we completed a full duration 15-second hotfire test of the upper stage for our NG-2 mission. This time, we achieved enhanced performance from the BE-3U engine, increasing the maximum thrust from 173,000 lbf to 175,000 lbf per engine, further expanding New Glenn’s capabilities for our customers.

January’s GS2 performed remarkably during our inaugural New Glenn launch, delivering our payload to orbit with less than 1% deviation from the target. Today, we completed a full duration 15-second hotfire test of the upper stage for our NG-2 mission. This time, we achieved enhanced performance from the BE-3U engine, increasing the maximum thrust from 173,000 lbf to 175,000 lbf per engine, further expanding New Glenn’s capabilities for our customers.

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Canada's first orbital-class rocket engine is now being manufactured! Our patent pending Hadfield-150 engine is the largest and most powerful rocket engine ever built in Canada, and the first known Canadian orbital-class engine to make it to this stage. The Hadfield-150 builds on everything we learned after years of painstakingly designing, manufacturing, and testing the Hadfield-10 series, our first regeneratively cooled and additively manufactured liquid rocket engine. Every engine test, both successful and unsuccessful on our Darkhorse test stand at Area 66, retired risk that's now carried straight into Hadfield-150 and sovereign orbital launch for Canada. A few details about the Hadfield-150 engine series: ✅ Designed to power Tundra and Tundra+, our light and medium-lift launch vehicles, and built to scale to Tempest, our larger reusable medium lift vehicle ✅ Manufactured entirely in-house, from design to print to test, for true sovereign launch capability ✅ Produced at Rocket Factory 1, on our expanding fleet of metal additive manufacturing systems at the AMA Lab, including the largest known metal 3D printer in Canada ✅ Designed for reusability and medium-lift scale from the outset, and built to significantly cut the time, infrastructure, manufacturing and cost iterative engine testing usually requires, with room to scale to even larger engines by leveraging the same design ✅ Capable of engine-out functionality, so losing one on an early flight doesn't have to mean losing the mission ✅ Optimized for Canada's Launch the North initiative, to deliver sovereign operational capability in a time and cost efficient manner Initial testing starts later this year at our new Blackhawk orbital engine test cell at Area 66, our private test range in Ontario. Stacked, integrated vehicle testing comes later at the Atlantic Spaceport Complex, our spaceport in Newfoundland and Labrador. Stay tuned for some exciting and fiery milestones ahead! 🚀🇨🇦 National Defence Defence Research and Development Canada Canadian Space Agency Transport Canada NGen Canada

Canada's first orbital-class rocket engine is now being manufactured! Our patent pending Hadfield-150 engine is the largest and most powerful rocket engine ever built in Canada, and the first known Canadian orbital-class engine to make it to this stage. The Hadfield-150 builds on everything we learned after years of painstakingly designing, manufacturing, and testing the Hadfield-10 series, our first regeneratively cooled and additively manufactured liquid rocket engine. Every engine test, both successful and unsuccessful on our Darkhorse test stand at Area 66, retired risk that's now carried straight into Hadfield-150 and sovereign orbital launch for Canada. A few details about the Hadfield-150 engine series: ✅ Designed to power Tundra and Tundra+, our light and medium-lift launch vehicles, and built to scale to Tempest, our larger reusable medium lift vehicle ✅ Manufactured entirely in-house, from design to print to test, for true sovereign launch capability ✅ Produced at Rocket Factory 1, on our expanding fleet of metal additive manufacturing systems at the AMA Lab, including the largest known metal 3D printer in Canada ✅ Designed for reusability and medium-lift scale from the outset, and built to significantly cut the time, infrastructure, manufacturing and cost iterative engine testing usually requires, with room to scale to even larger engines by leveraging the same design ✅ Capable of engine-out functionality, so losing one on an early flight doesn't have to mean losing the mission ✅ Optimized for Canada's Launch the North initiative, to deliver sovereign operational capability in a time and cost efficient manner Initial testing starts later this year at our new Blackhawk orbital engine test cell at Area 66, our private test range in Ontario. Stacked, integrated vehicle testing comes later at the Atlantic Spaceport Complex, our spaceport in Newfoundland and Labrador. Stay tuned for some exciting and fiery milestones ahead! 🚀🇨🇦 National Defence Defence Research and Development Canada Canadian Space Agency Transport Canada NGen Canada

NordSpace 🇨🇦

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🔥 Exactly a decade ago, we ignited our first rocket engine. Today, we’re igniting Europe’s path to space. Since 2015, we’ve grown into the largest private European developer of rocket engine technology, with the ability to design, manufacture, test, and fly liquid-fuelled rocket engines entirely in-house. With the TEPREL engine family, we’ve successfully demonstrated spaceflight-proven technology. Now, with TEPREL-C, we’ve taken a bold step forward, with our first fully internally developed turbopump, one of the most complex subsystems in propulsion engineering. At PLD Space, we're not just following the path, we're defining the future of space access.

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I've come to appreciate boring hotfires. Our BE-7 team recently completed a 2,500 second hotfire test at 10klbf on a development engine, setting the record for the longest-duration turbo pump-fed liquid rocket engine hotfire. This built on some of the most rigorous testing in the history of propulsion, with the previous record set by the RS-25 engine that powered the Space Shuttle. They recorded two 2,017 second tests in 1988. It's not lost on us that we're following a path those engineers blazed, and we're grateful for it. Grab the popcorn and enjoy watching 41 minutes of hotfire goodness.

I've come to appreciate boring hotfires. Our BE-7 team recently completed a 2,500 second hotfire test at 10klbf on a development engine, setting the record for the longest-duration turbo pump-fed liquid rocket engine hotfire. This built on some of the most rigorous testing in the history of propulsion, with the previous record set by the RS-25 engine that powered the Space Shuttle. They recorded two 2,017 second tests in 1988. It's not lost on us that we're following a path those engineers blazed, and we're grateful for it. Grab the popcorn and enjoy watching 41 minutes of hotfire goodness.

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🇺🇦🇷🇺 Chief designer at Ukraine's Fire Point says first domestically produced ballistic missiles to be launched against Russia this fall "The only thing separating us there is the engine test. Once we test the engine, we start flight tests" Further escalation of the war is inevitable

🇺🇦🇷🇺 Chief designer at Ukraine's Fire Point says first domestically produced ballistic missiles to be launched against Russia this fall "The only thing separating us there is the engine test. Once we test the engine, we start flight tests" Further escalation of the war is inevitable

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This bootstrapped startup just completed the first successful hot-fire test of their cryogenic methalox engine. And they did it from their own test facility called SPARC. Which they built in under 3 months. This engine is called Cryonix. Each of these engines will be capable of producing a thrust of 100kN. And nine of these engines will power their own small lift launch vehicle called Mach Blue. They are planning to do commercial launches within the next 3 years.

This bootstrapped startup just completed the first successful hot-fire test of their cryogenic methalox engine. And they did it from their own test facility called SPARC. Which they built in under 3 months. This engine is called Cryonix. Each of these engines will be capable of producing a thrust of 100kN. And nine of these engines will power their own small lift launch vehicle called Mach Blue. They are planning to do commercial launches within the next 3 years.

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21,263 görüntüleme • 1 ay önce

This week on the test stand: the Astra team continues pushing the run box limits of our Rocket 4.0 first stage engine combustion chamber.

This week on the test stand: the Astra team continues pushing the run box limits of our Rocket 4.0 first stage engine combustion chamber.

Astra

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🔥 Ship 39 has just completed the first ever 6 engine static fire test of a V3 ship! I suspect tomorrow we will see a single engine test using the header tanks! 🎥: Avid Space

🔥 Ship 39 has just completed the first ever 6 engine static fire test of a V3 ship! I suspect tomorrow we will see a single engine test using the header tanks! 🎥: Avid Space

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E-2 Thrust Vector Control testing is underway! This test includes frequency sweeps starting at a maximum gimbal angle of ±7 degrees, using hardware from a previous engine revision. After completing additional testing on the component stand, the actuator will be deployed to the test site for its first gimballed test fire.

E-2 Thrust Vector Control testing is underway! This test includes frequency sweeps starting at a maximum gimbal angle of ±7 degrees, using hardware from a previous engine revision. After completing additional testing on the component stand, the actuator will be deployed to the test site for its first gimballed test fire.

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We are in the final preparations to test fire our first cryogenic methane engine, a 20 kN (2 tons force) rocket thruster generated without human intervention by the Noyron Large Computational Engineering Model.

We are in the final preparations to test fire our first cryogenic methane engine, a 20 kN (2 tons force) rocket thruster generated without human intervention by the Noyron Large Computational Engineering Model.

LEAP 71

32,462 görüntüleme • 8 ay önce

After years of development, testing and refinement, we are printing one of our last Hadfield-10 rocket engines, a bittersweet moment 🫡 More of our team is transitioning toward getting our much larger orbital-class Hadfield-100 engine ready for the test stand, and getting Canada to orbit for the first time with our Tundra rocket. The pressure-fed Hadfield-10 series has been the backbone of NordSpace's propulsion program since our earliest days. It's the engine that proved we could design, manufacture, test and fly liquid rocket engines from scratch, entirely in-house, at the pace necessary to reach orbit. It powered our first successful hot-fire tests, survived our most demanding qualification campaigns, and gave our team the hard-won knowledge that no textbook or simulation could provide. It also powers our Taiga sub-orbital vehicle, which is taking flight in a few weeks. Every experimental lesson learned in its development from combustion stability, regenerative cooling, additive manufacturing, and test operations lives on in what comes next. That knowledge now flows directly into our turbopump fed Hadfield-100 engine, the most powerful rocket engine in Canadian history. Designed to power our orbital Tundra rocket to deliver 500+ kg to LEO and scaling further to 1,100 kg LEO in the Tundra+ configuration. Architected from day one to grow to the thrust levels required for our reusable Titan medium-lift vehicle targeting 5,000+ kg to LEO while striking the right balance between performance, scalability, heritage, and speed of development to meet the Government of Canada's targets. The Hadfield-10's design will also form the foundation of our SHARP Sabre hypersonic rocket's M2S-HyRock engine. The full shift to the Hadfield-100 is a major milestone for us, and it's not just about more powerful engines. The infrastructure we're developing from moving to a much larger facility, acquiring much larger metal 3D printers, developing new test cells, and pursuing rigorous standards all feed in to this next phase of growth for our program. To everyone on the NordSpace team who designed, printed, tested, and refined these engines across so many late nights, early mornings and weekends, thank you. This chapter made everything that follows possible, and the next one starts now. Ad astra per aspera 🚀🇨🇦 National Defence Canadian Space Agency Defence Research and Development Canada Canadian Armed Forces Transport Canada

After years of development, testing and refinement, we are printing one of our last Hadfield-10 rocket engines, a bittersweet moment 🫡 More of our team is transitioning toward getting our much larger orbital-class Hadfield-100 engine ready for the test stand, and getting Canada to orbit for the first time with our Tundra rocket. The pressure-fed Hadfield-10 series has been the backbone of NordSpace's propulsion program since our earliest days. It's the engine that proved we could design, manufacture, test and fly liquid rocket engines from scratch, entirely in-house, at the pace necessary to reach orbit. It powered our first successful hot-fire tests, survived our most demanding qualification campaigns, and gave our team the hard-won knowledge that no textbook or simulation could provide. It also powers our Taiga sub-orbital vehicle, which is taking flight in a few weeks. Every experimental lesson learned in its development from combustion stability, regenerative cooling, additive manufacturing, and test operations lives on in what comes next. That knowledge now flows directly into our turbopump fed Hadfield-100 engine, the most powerful rocket engine in Canadian history. Designed to power our orbital Tundra rocket to deliver 500+ kg to LEO and scaling further to 1,100 kg LEO in the Tundra+ configuration. Architected from day one to grow to the thrust levels required for our reusable Titan medium-lift vehicle targeting 5,000+ kg to LEO while striking the right balance between performance, scalability, heritage, and speed of development to meet the Government of Canada's targets. The Hadfield-10's design will also form the foundation of our SHARP Sabre hypersonic rocket's M2S-HyRock engine. The full shift to the Hadfield-100 is a major milestone for us, and it's not just about more powerful engines. The infrastructure we're developing from moving to a much larger facility, acquiring much larger metal 3D printers, developing new test cells, and pursuing rigorous standards all feed in to this next phase of growth for our program. To everyone on the NordSpace team who designed, printed, tested, and refined these engines across so many late nights, early mornings and weekends, thank you. This chapter made everything that follows possible, and the next one starts now. Ad astra per aspera 🚀🇨🇦 National Defence Canadian Space Agency Defence Research and Development Canada Canadian Armed Forces Transport Canada

NordSpace 🇨🇦

42,533 görüntüleme • 5 ay önce

Our contribution to #UAENationalDay fireworks - the Emirates’ first MethaLOX rocket engine. 20 kN (2 tons), 50 bar chamber pressure. First test campaign just completed. Designed by the Noyron Large Computational Engineering Model without human intervention.

Our contribution to #UAENationalDay fireworks - the Emirates’ first MethaLOX rocket engine. 20 kN (2 tons), 50 bar chamber pressure. First test campaign just completed. Designed by the Noyron Large Computational Engineering Model without human intervention.

LEAP 71

23,332 görüntüleme • 8 ay önce