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

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Online Access

Connect to online resource - All users (Federal Depository Library Program Persistant URL)