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