Hifire-5 flight test results
Web26 de abr. de 2024 · The USAF, he said, will have radar track and telemetry capture on the ground from the 45th Space Wing located at Cape Canaveral. The USAF, Dolvin said, planned its first X-60A test flight for ... Web26 de fev. de 2015 · The Hypersonic International Flight Research Experimentation (HIFiRE-5) is a hypersonic flight test vehicle designed to investigate the …
Hifire-5 flight test results
Did you know?
WebHIFiRE-5 Flight Test Results. Thomas J. Juliano, David W. Adamczak, R. Kimmel; Physics. 2015; The Hypersonic International Flight Research Experimentation (HIFiRE-5) is a hypersonic flight test vehicle designed to investigate the aerothermodynamics of a three-dimensional geometry. It is a … Expand. 34. Save. WebT. J. Juliano, L. Paquin, and M. P. Borg, “Measurement of HIFiRE-5 Boundary-Layer Transition in a Mach-6 Quiet Tunnel with Infrared Thermography”, AIAA Journal,57(5) ... “HIFiRE-5 Flight Test Results”. Journal of Spacecraft and Rockets, 52(3):650–663, May–June 2015. Selected Conference Publications.
WebHIFiRE flight 5 is devoted to measuring transition on a three-dimensional body. This paper summarizes payload configuration, trajectory, vehicle stability limits and roughness … Web31 de jan. de 2024 · The geometric configuration of MF-1 is almost identical to that of HIFiRE-1, except that the head radius of MF-1 is twice as large as that of HIFiRE-1. The BLT results of both flight tests are similar. However, linear stability analysis shows that the boundary layer of MF-1 is more stable than that of HIFiRE-1, which is shown in Fig. 19.
Web7 de jan. de 2013 · HIFiRE-5 was the first HIFiRE flight to use both the Inertial Sciences Digital Miniature Attitude Reference System (DMARS-R) IMU and Ashtech DG14 Global … Web19 de out. de 2009 · HIFiRE flights one and five (HIFiRE-1 and HIFiRE-5, respectively) were devoted to boundary-layer transition. The body of knowledge from the research campaigns showed a complex transition behavior.
Web11 de abr. de 2011 · A series of hydrocarbon-fueled direct-connect scramjet ground tests has been completed in the NASA Langley Arc-Heated Scramjet Test Facility (AHSTF) at simulated Mach 8 flight conditions. These experiments were part of an initial test phase to support Flight 2 of the Hypersonic International Flight Research Experimentation …
Web26 de fev. de 2015 · The Hypersonic International Flight Research Experimentation (HIFiRE-5) is a hypersonic flight test vehicle designed to investigate the … sharon cummings fishWebHIFiRE-5 is a hypersonic flight-test experiment designed to investigate the aerothermodynamics of a three-dimensional geometry. The vehicle is an elliptic cone … sharon cummings-robertssharon cummings facebookWeb2. HIFiRE-5 Experiment The HIFiRE-5 concept configuration consists of an S-30 first stage [19] and Improved Orion [20] second stage, shown in Fig. 2.1. The S-30 / Orion stack will boost the test article to approximately 270 km, with a peak reentry Mach number of 7.5. The test article consists of a blunt-nosed elliptic cone of 2:1 ellipticity, 0 ... population of uzbekistan in 2022WebThe HIFiRE-5 test article was an elliptic cone with a 2.5-mm nose radius and 2:1 aspect ratio and a 7-degree minor-axis half-angle. The vehicle was flown in April 2012. sharon cummings artist biographyWeb7 de ago. de 2024 · The Hypersonic International Flight Research Experimentation Program (HIFiRE) launches an experimental hypersonic scramjet vehicle from the Pacific Missile Range Facility in Hawaii during … sharon cummings realtorWebHIFiRE-5 flight test heating analysis. TJ Juliano, D Adamczak, RL Kimmel. 52nd Aerospace Sciences Meeting, 0076 ... TJ Juliano, KJ Disotell, JW Gregory, J Crafton, S Fonov. Measurement Science and Technology 23 (4), 045303, 2012. 46: 2012: HIFiRE-5 flight test results. TJ Juliano, D Adamczak, RL Kimmel. Journal of Spacecraft and … sharon cummings art