The Aerosciences Branch (EV33) at the George C. Marshall Space Flight Center (MSFC) has been responsible for a series of wind tunnel tests on the National Aeronautics and Space Administration's (NASA) Space Launch System (SLS) vehicles. The primary purpose of these tests was to obtain aerodynamic data during the ascent phase and establish databases that can be used by the Guidance, Navigation, and Mission Analysis Branch (EV42) for trajectory simulations. The paper describes the test particulars regarding models and measurements and the facilities used, as well as database preparations.
Aerodynamic Tests of the Space Launch System for Database Development
AIAA SciTech 2014 Conference ; 2014 ; Baltimore, MD, United States
2014-01-13
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aerodynamic Tests of the Space Launch System for Database Development (AIAA 2014-1256)
British Library Conference Proceedings | 2014
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