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

Bibliographic Details
Uniform Title:	NASA technical memorandum ; 217746.
Main Author:	Palaszewski, Bryan Alan Richard (Author)
Corporate Authors:	NASA Glenn Research Center (Issuing body) United States. National Aeronautics and Space Administration (sponsoring body.) AIAA Aerospace Sciences Meeting
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:	Connect to online resource - All users (Federal Depository Library Program Persistant URL)
Physical Description:	1 online resource (25 pages) : illustrations.
Variant Title:	Supersonic retropropulsion wind tunnel testing.
Format:	Government Document Electronic Conference Proceeding eBook

Description
Note:	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."
Call Number:	NAS 1.15:2012-217746 Online
Bibliography Note:	Includes bibliographical references (pages 4-6).