Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Bahrami, Parviz A. (Parviz Ahmadi) (Author)
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
Series:	NASA technical memorandum ; 2012-216006.
Subjects:	Aerobraking. Aerocapture. Aerodynamic heat transfer. Ballutes. Drag devices. Spacecraft reentry. Aerothermodynamics. Atmospheric entry. Descent trajectories. Mathematical models. Trajectories.

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Call Number:	NAS 1.15:2012-216006
NAS 1.15:2012-216006	Available