Diamond Member SpaceMan 0 Posted June 21 Diamond Member Share Posted June 21 2 min readPreparations for Next Moonwalk Simulations Underway (and Underwater) This is the hidden content, please Sign In or Sign Up Launch of the Hypersonic International Flight Research Experimentation Program (HIFiRE) Flight 2 sounding rocket, a ****** NASA-Air Force Research Laboratory flight experiment, May 1, 2012.Credit: AFRL Technical Challenges (TCs) are finite-duration research and development endeavors supporting the strategic goals of NASA. The Hypersonic Technology project’s Technical Challenges include estimation of uncertainty for hypersonic research problems and vehicle systems, testing controls for switching engines mid-flight, and researching more efficient fuel combustors for large ramjets, which will be needed by future commercial high-speed planes. Uncertainty Quantification This Technical Challenge is complete!TC-1: System-Level Uncertainty Quantification Methodology Development and Validation: NASA developed and validated a system-level uncertainty propagation methodology to guide uncertainty-informed decision making by identifying fundamental research areas that will reduce the system performance uncertainty. Learn more about Uncertainty Quantification on TechPort Turbine-Based Combined Cycle TC-2: Turbine-Based Combined Cycle Mode Transition Technology Development: The Combined Cycle Mode Transition challenge demonstrates autonomous control and establishes performance/operability assessment methodologies for future reusable hypersonic propulsion systems that use turbine engines at slow speeds while transitioning to scramjets for high-speed operations. This challenge addresses the technology barrier of propulsion system mode transition via ground tests. Learn more about Combined Cycle on TechPort Improved Combustor Scaling Laws for Hypersonics TC-3: Development of Improved Combustor Scaling Laws for Dual-Mode Ramjets: To improve current engine performance and enable engine scale up to fully reusable vehicle scales 100 times larger, NASA will develop and deliver mathematical models and associated validation test data with quantified uncertainty that support the design of high-speed combustors inclusive of green fuels. NASA will demonstrate such capability by reducing the length of the state-of-the-art cavity flameholder by 25 percent (10 percent threshold, 25 percent goal cavity length reduction relative to a state-of-the-art baseline.) Learn more about Combustor Scaling on TechPort Read More About the Hypersonic Technology Project About the Author This is the hidden content, please Sign In or Sign Up Shannon EichornShannon Eichorn is the Strategic Engagement Lead for NASA’s Advanced Air Vehicles Program. She is a former test engineer in supersonic wind tunnels and former engineer managing facilities, such as the Aeroacoustic Propulsion Lab, Glenn Extreme Environments Rig, and Creek Road Cryogenics Complex. This is the hidden content, please Sign In or Sign Up logo This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up logo This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up Linkedin logo This is the hidden content, please Sign In or Sign Up Explore More This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> 2 min read Hypersonic Technology Project Overview Article 21 mins ago This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> 2 min read Hypersonic Research Topics Article 22 mins ago This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> 2 min read High-Speed Market Studies Article 3 days ago Keep Exploring Discover Related Topics Technology Transfer & Spinoffs This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> Small Business Innovation Research (SBIR) / Small Business Technology Transfer (STTR) This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> Manufacturing and Materials This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> Why Go to Space This is the hidden content, please Sign In or Sign Up /applications/core/interface/js/spacer.png"> Share Details Last Updated Jun 21, 2024 EditorJim BankeContactShannon Eichorn*****@*****.tld Related Terms This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up This is the hidden content, please Sign In or Sign Up Link to comment https://hopzone.eu/forums/topic/49486-nasa-hypersonics-technical-challenges/ Share on other sites More sharing options...
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