Ethereal Exploration Guild
@EtherealXTech
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Official home of the Guild on Twitter.
Bengaluru, India
Joined February 2022
To clarify, the LOX turbopump, along with the RP1 turbopump, is designed to power our upper-stage engine, Pegasus 2.0.
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Status note from the Guild: India’s first privately developed indigenous LOX turbo pump assembly. The additively manufactured turbopump will be tested in Base 001 - our 700,000 sq. ft. semi-cryogenic engine test facility.
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The future of deep exploration is being built here in India. Grateful for the vision and the ecosystem that makes it possible. @PiyushGoyal @narendramodi @isro @INSPACeIND
भारत के स्टार्टअप्स अब अंतरिक्ष की दुनिया में भी आत्मनिर्भरता की नई उड़ान भर रहे हैं। 🚀 माननीय प्रधानमंत्री श्री @NarendraModi जी के नेतृत्व ���ें शुरू की गई #StartupIndia पहल और विभिन्न नीतिगत सुधारों ने युवा उद्यमियों को प्रोत्साहित किया है। इसी का परिणाम है कि Ethereal X जैसे
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How fast they evolve. Meet Pegasus 2.0 – the largest 3D printed Thrust Chamber Assembly in India. Optimized for weight, better performance, and increased engine lifecycle.
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India’s space startup, Ethereal Exploration Guild met Amb. Vani Rao. The Bengaluru based group is building India's first reusable space launch vehicle. Wonderful to see India’s talented engineers contributing to our robust aerospace & innovation ecosystem. Many opportunities for
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We’re not catching up. We’re setting the pace. Next time you see test hardware that doesn’t look like this — ask why.
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This RP-1 skid is capable of replicating a wide range of mission requirements, enabling us to qualify our engines with global rigor. It’s not just about performance — it’s about raising the bar for how propulsion systems are engineered, tested, and proven.
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For our brilliant team of engineers, this means a level of fidelity and system responsiveness that’s essential for tuning and validating complex propulsion systems.
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Rated up to 200 bar and designed to manage high flow rates with real-time responsiveness, this facility enables deep control of tank pressure, line pressure, and line flow rate — all with a closed-loop response time of just 360 milliseconds.
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You're looking at India’s highest-pressure-rated semi-cryogenic RP-1 test setup, engineered for our Pegasus engine development program.
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Meet EtherealX, a Bengaluru-based startup founded by Mechanical Engineer and lIAS Scientist-Astronaut Graduate Manu J Nair, Former ISRO engineer Shubhayu Sardar, and Aerospace Engineer Prashant Sharma. #EtherealX #RazorCrestMk1 #ReusableRockets #PrivateRocketEngine #SpaceTech
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They're here to transform the global space industry with India's most powerful private rocket engine! Their mission? To make space launches fully reusable, reducing costs and cutting down the time needed for satellite launches!
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Razor Crest Mk-1 - EtherealX's game-changing rocket - will carry up to 24.8 tons into Lower Earth Orbit (LEO) and is fully reusable! That means both the booster and upper stage return to Earth after each launch, making it more efficient than ever.
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What powers this rocket's upper stage? The Pegasus Thrust Chamber Assemblies (TCA) - India's first-ever reusable rocket engine! This engine can generate 40 kN of thrust and achieve a specific impulse (Isp) of 293 seconds at sea level.
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It's one of the most efficient semi-cryogenic engines worldwide! The Full Flow Segregated Cooling Cycle (FSCC) that runs the engine is a game-changer, making this rocket engine one of the most efficient India has ever developed!
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Presenting Bharat's first reusable rocket engine's TCA:
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The new watermark of potential we set with this TCA; 1. The world’s first RP-1/LOX engine TCA that can also run on an expander cycle. 2. India’s first bi-propellant-cooled engine's TCA. 3. India’s most powerful indigenously developed semi-cryogenic TCA.
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The TCA is designed to produce 40kN of thrust and provide an Isp of 293s (sea-level). If the Isp persists during our test campaign, this will be India's most efficient semi-cryogenic TCA.
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This TCA will be part of the engines that power our vehicle's upper stage. For the first time in five decades of rocketry, an upper stage will be run by a proprietary, all-new rocket engine feed cycle: the Full Flow Segregated Cooling Cycle (FSCC), an indigenously developed cycle
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