Aeroheating Characteristics for a Two-Stage-To-Orbit Concept During Separation at Mach 6-Reference-Cited by-同舟云学术

Aeroheating Characteristics for a Two-Stage-To-Orbit Concept During Separation at Mach 6

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
language:
Short-container-title:

Author:

Liechty Derek¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5139

Reference13 articles.

1. 1Murphy,K.J.,Buning,P.G.,Pamadi,B.N.,Scallion,W.I.,andJones,K.M."OverviewofTransonictoHypersonicStage SeparationToolDevelopmentforMulti-Stage-To-OrbitConcepts,"AIAAPaper2004-2595,July2004.

2. 2NGLTFactSheet,http://www1.msfc.nasa.gov/NEWSROOM/background/facts/ngltfacts.pdf,Nov.2003.

3. 3Micol,J.R."HypersonicAerodynamic/AerothermodynamicTestingCapabilitiesatLangleyResearchCenter:AerothermodynamicFacilitiesComplex,"AIAAPaper95-2107,June1995.

4. 5Buck,G.M."AutomatedThermalMappingTechniquesUsingChromaticImageAnalysis,"NASATM101554,April1989.

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