An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By: Ramadas K. Prabhu.
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-2001-211266.; NASA contractor report -- NASA CR-211266.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information
Published: 2001
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Aeroshells.; Computational fluid dynamics.; Inviscid flow.; Mach number.; Mars missions.; Wind tunnel tests.
Notes: Shipping list no.: 2002-0546-M.

Also available via Internet from the NASA Web site. Address as of 2/26/04: http://techreports.larc.nasa.gov/ltrs/PDF/2001/cr/NASA-2001-cr211266.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002] 1 microfiche.