Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmospheric Entry-Reference-Cited by-同舟云学术

Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmospheric Entry

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
language:
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Author:

Garcia Joseph¹,Brown James¹,Kinney David¹,Bowles Jeffrey¹,Jiang Xun²,Dupzyk Ian²,Huynh Loc²,Lau Eric³

Affiliation:

1. NASA Ames Research Center

2. ELORET Corporation

3. ELORET Coporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-5052

Reference25 articles.

1. Brown, J.L. "The EffectofForebodyGeometryon TurbulentHeating andThermalProtection SystemSizing for Future Mars MissionsConcepts," InternationalPlanetaryProbeWorkshop4,June,2006.

2. WrightH.,S.,Oh D.Y.,Weshelle, C.H., Fisher, J. L.,Dyke, R. E., Edquist, K.T.,Brown, J.L., Justh, H. L., Munk,M. M."MarsAerocaptureSytems Study," NASATM-2006-214522,Nov.2006.

3. Garcia,J.A.,Brown, J.L., BowlesJ.V.,Kinney,D.J.,andHuynhL.C."AParametricCo-Optimizationof Lifting BluntBodyVehicle ConceptsforAtmospheric Entry",21stInternationalConferenceonParallel ComputationalFluidDynamics,May18-22,2009,MoffettField, CA.

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