Cover Image

Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing /

Bibliographic Details
Main Author: Palaszewski, Bryan Alan Richard (Author)
Corporate Authors: United States. National Aeronautics and Space Administration (sponsoring body.), AIAA Aerospace Sciences Meeting
Format: Government Document Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:NASA technical memorandum ; 217746.
Subjects:
Computational fluid dynamics.
Planetary landing.
Aerodynamic brakes.
Landing aids.
Soft landing.
Landing sites.
Rocket engines.
Shock wave interaction.
Supersonic flight.
Online Access:https://purl.fdlp.gov/GPO/gpo39373
Description
Item Description:Title from title screen (viewed Aug. 29, 2013).
"December 2012."
"Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012."
"AIAA-2012-401."
Physical Description:1 online resource (25 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 4-6).