Research Catalog

Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas

Title
  1. Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.
Published by
  1. Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
Author
  1. Bahrami, Parviz A. (Parviz Ahmadi)

Available online

Details

Additional authors
  1. NASA Glenn Research Center, issuing body.
Description
  1. 1 online resource (iv, 13 pages) : color illustrations.
Series statement
  1. NASA/TM ; 2012-216006
Uniform title
  1. NASA technical memorandum ; 2012-216006.
Subject
  1. Aerobraking
  2. Aerocapture
  3. Aerodynamic heat transfer
  4. Ballutes
  5. Drag devices
  6. Spacecraft reentry
  7. Aerothermodynamics
  8. Atmospheric entry
  9. Descent trajectories
  10. Mathematical models
  11. Trajectories
Call number
  1. GPO Internet NAS 1.15:2012-216006
Note
  1. Title from title screen (viewed on June 6, 2013).
  2. "March 2012."
Bibliography (note)
  1. Includes bibliographical references (page 10).
Author
  1. Bahrami, Parviz A. (Parviz Ahmadi), author.
Title
  1. Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.
Publisher
  1. Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
Type of content
  1. text
Type of medium
  1. computer
Type of carrier
  1. online resource
Series
  1. NASA/TM ; 2012-216006
  2. NASA technical memorandum ; 2012-216006.
Bibliography
  1. Includes bibliographical references (page 10).
Connect to:
  1. https://purl.fdlp.gov/GPO/gpo37271
Added author
  1. NASA Glenn Research Center, issuing body.
Gpo item no.
  1. 0830-D (online)
Sudoc no.
  1. NAS 1.15:2012-216006
View in legacy catalog