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NASA Engineering and Safety Center Technical Bulletin No. 21-02: Genesis Flight Mechanics SimulationGenesis Flight Mechanics Simulation
The NASA Engineering and Safety Center (NESC) consolidated and modernized a suite of legacy flight mechanics simulations, including the Flight Analysis and Simulation Tool (FAST), resulting in Genesis, a generic, multi-vehicle, variable-degree-of-freedom flight mechanics simulation for ascent, aerocapture, entry, descent, and landing (A2EDL) trajectory design.

Genesis is more flexible, capable, and performant than FAST. It enables trajectory optimization and interactive trajectory generation. Its interoperability with Copernicus, an exo-atmospheric and interplanetary trajectory design tool, facilitates end-to-end trajectory optimization across all mission phases. Genesis is implemented in Julia, a new language for technical computing that combines the ease of use of scripting languages with the run-time performance of compiled languages.
Document ID
20210014768
Acquisition Source
Langley Research Center
Document Type
Other - NESC Technical Bulletin
Authors
Daniel G Murri
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 28, 2021
Publication Date
May 13, 2021
Subject Category
Mechanical Engineering
Report/Patent Number
Technical Bulletin 21-02
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
EDL
Genesis
Flight Mechanics
Simulation
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