Advances in Launch Vehicle Ascent and Booster Separation CFD
Speakers: Derek Dalle & Jamie Meeroff, Computational Aerosciences Branch, NASA Ames Research Center
Presentation
Abstract
With the imminent launch of Artemis I, this seminar will present highlights of the work done by the Ames SLS CFD Team, part of the Computational Aerosciences branch at NASA Ames, to support the Artemis program and specifically Space Launch System (SLS) over the last 8 years. The team at Ames primarily provides aerodynamic analysis using CFD between the point where the vehicle reaches Mach 0,5 and booster separation. The team also provides aerodynamics using CFD for booster separation itself, which only takes about one second in flight but needs about 10 thousand individual CFD solutions to analyze.
The talk will feature some of the details of performing CFD for a modern launch vehicle program where computational analysis plays a growing role compared to previous programs that relied purely on wind tunnel and flight testing. It will also offer advice for any program that needs to run hundreds or more CFD cases and hint at the upcoming release of the CAPE software developed and used by the Ames SLS CFD Team to manage such large data sets.
Funded by the NASA’s SLS Program.
Biography