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Atmospheric Models for Aerocapture
Author(s) -
C. G. Justus,
Aleta Duvall,
Ver W. Keller
Publication year - 2004
Publication title -
36th aiaa/asme/sae/asee joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2004-3844
Subject(s) - atmospheric model , computer science , environmental science , aerospace engineering , engineering , meteorology , physics
There are eight destinations in the Solar System with sufficient atmosphere for aerocapture to be a viable aeroassist option - Venus, Earth, Mars, Jupiter, Saturn and its moon Titan, Uranus, and Neptune. Engineering-level atmospheric models for four of these targets (Earth, Mars, Titan, and Neptune) have been developed for NASA to support systems analysis studies of potential future aerocapture missions. Development of a similar atmospheric model for Venus has recently commenced. An important capability of all of these models is their ability to simulate quasi-random density perturbations for Monte Carlo analyses in developing guidance, navigation and control algorithms, and for thermal systems design. Similarities and differences among these atmospheric models are presented, with emphasis on the recently developed Neptune model and on planned characteristics of the Venus model. Example applications for aerocapture are also presented and illustrated. Recent updates to the Titan atmospheric model, in anticipation of applications for trajectory and atmospheric reconstruct of Huygens Robe entry at Titan, are discussed. Recent updates to the Mars atmospheric model, in support of ongoing Mars aerocapture systems analysis studies, are also presented.

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