Radiatively Driven Hypersonic Wind Tunnel/Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (RDHWT/MARIAH II) Ultrahigh-Pressure Technoloy and Nozzle Survivability Experiments Review
Author:
Affiliation:
1. MSE Technology Applications, Inc
2. Oak Ridge National Laboratory
3. Aerospace Testing Alliance
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2483
Reference10 articles.
1. Costantino, M.andDarnell, I. "Ultra-HighPressure ModelingandExperiments Review,"AIAA-2004-2482,24thAIAAAerodynamicMeasurementTechnologyandGroundTestingConference,Portland,OR, June28-July1,2004.
2. Tarrant,G.S."End ClosureFailure IncidentReport,"MSEReport, February11,2004.
3. Felderman, E.J., Shope, F. L.,Liu,C.T., andSchneibel,J."PotentialNewMaterialsforHypersonic Nozzles,"2003NationalSpaceandMissileMaterialsSymposium(NSMMS), SanDiego, CA,June2003.
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