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HyperPASS, a New Aeroassist ToolA new software tool designed to perform aeroassist studies has been developed by Global Aerospace Corporation (GAC). The Hypersonic Planetary Aeroassist Simulation System (HyperPASS) [1] enables users to perform guided aerocapture, guided ballute aerocapture, aerobraking, orbit decay, or unguided entry simulations at any of six target bodies (Venus, Earth, Mars, Jupiter, Titan, or Neptune). HyperPASS is currently being used for trade studies to investigate (1) aerocapture performance with alternate aeroshell types, varying flight path angle and entry velocity, different gload and heating limits, and angle of attack and angle of bank variations; (2) variable, attached ballute geometry; (3) railgun launched projectile trajectories, and (4) preliminary orbit decay evolution. After completing a simulation, there are numerous visualization options in which data can be plotted, saved, or exported to various formats. Several analysis examples will be described.
Document ID
20070014632
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Gates, Kristin
(Global Aerospace Corp. Altadena, CA, United States)
McRonald, Angus
(Global Aerospace Corp. Altadena, CA, United States)
Nock, Kerry
(Global Aerospace Corp. Altadena, CA, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 2005
Publication Information
Publication: 2nd International Planetary Probe Workshop
Subject Category
Space Sciences (General)
Distribution Limits
Public
Copyright
Public Use Permitted.
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