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Space Launch System Mobile Launcher Modal Pretest Analysis
Akers, James C. ; Sills, Joel W., Jr
Glenn Research Center 2020
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Título:
Space Launch System Mobile Launcher Modal Pretest Analysis
Autor:
Akers, James C.
;
Sills, Joel W., Jr
Assuntos:
Spacecraft Design, Testing And Performance
Notas:
Glenn Research Center
Houston, TX
GRC-E-DAA-TN77647
GRC
Descrição:
NASA is developing an expendable heavy lift launch
vehicle
capability, the Space Launch System, to support lunar and deep space exploration. To support this capability, an updated
ground
infrastructure is required including modifying an existing Mobile Launcher system. The Mobile Launcher is a very large heavy beam/truss steel structure designed to support the Space Launch System during its buildup and integration in the
Vehicle
Assembly Building, transportation from the
Vehicle
Assembly Building out to the launch pad, and provides the launch platform at the launch pad. The previous Saturn/Apollo and Space Shuttle programs had integrated
vehicle
ground
vibration tests of their integrated launch vehicles performed with simulated free-free boundary conditions to experimentally anchor and validate structural and flight controls analysis models. For the Space Launch System program, the Mobile Launcher will be used as the modal test fixture for the
ground
vibration test of the first Space Launch System flight vehicle, Artemis 1, programmatically referred to as the integrated vehicle modal test. The integrated vehicle modal test of the Artemis 1 integrated launch vehicle will have its core and second stages unfueled while mounted to the Mobile Launcher while inside the Vehicle Assembly Building, which is currently scheduled for the summer of 2020. The Space Launch System program has implemented a building block approach for dynamic model validation. The modal test of the Mobile Launcher is an important part of this building block approach in supporting the integrated vehicle modal test since the Mobile Launcher will serve as a structurally dynamic test fixture whose modes will couple with the modes of the Artemis 1 integrated vehicle. The Mobile Launcher modal test will further support understanding the structural dynamics of the Mobile Launcher and Space Launch System during rollout to the launch pad, which will play a key role in better understanding and prediction of the rollout forces acting on the launch vehicle. The Mobile Launcher modal test is currently scheduled for the summer of 2019. Due to a very tight modal testing schedule, this independent Mobile Launcher modal pretest analysis has been performed to ensure there is a high likelihood of successfully completing the modal test (i.e. identify the primary target modes) using the planned instrumentation, shakers, and excitation types. This paper will discuss this Mobile Launcher modal pretest analysis for its three test configurations and the unique challenges faced due to the Mobile Launcher’s size and weight, which are typically not faced when modal testing aerospace structures.
Editor:
Glenn Research Center
Data de criação/publicação:
2020
Idioma:
Inglês
Links
View record in NASA$$FView record in $$GNASA
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