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JAE: A Jupiter Atmospheric Entry Probe Heating CodeThe strong gravitational attraction of Jupiter on probes approaching the planet results in very high atmospheric entry velocities. The values relative to the rotating atmosphere can vary from about 47 to 60 km/sec, depending on the latitude of the entry. Therefore, the peak heating rates and heat shield mass fractions exceed those for any other atmospheric entries. For example, the Galileo probe's heat shield mass fraction was 50%, of which 45% was devoted to the forebody. Although the Galileo probe's mission was very successful, many more scientific questions about the Jovian atmosphere remain to be answered and additional probe missions are being planned. Recent developments in microelectronics have raised the possibility of building smaller and less expensive probes than Galileo. Therefore, it was desirable to develop a code that could quickly compute the forebody entry heating environments when performing parametric probe sizing studies. The Jupiter Atmospheric Entry (JAE) code was developed to meet this requirement. The body geometry consists of a blunt-nosed conical shape of arbitrary nose and base radius and cone angles up to about 65 deg at zero angle of attack.
Document ID
20020051879
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wercinski, Paul F.
(NASA Ames Research Center Moffett Field, CA United States)
Tauber, Michael E.
(NASA Ames Research Center Moffett Field, CA United States)
Yang, Lily
(Sterling Software, Inc. Palo Alto, CA United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Lunar And Planetary Science And Exploration
Funding Number(s)
PROJECT: RTOP 242-33-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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