Structural-dynamics problems pertinent to the design of launch vehicles suitable for a lunar mission are discussed. Some measurements of the natural modes of a model of the Saturn launch vehicle are pre- sented. Recent information concerning launch-vehicle loads associated with buffeting, aerodynamic noise, and winds is also presented.
CITATION STYLE
Launch vehicle dynamics. (2008). In Rocket and Spacecraft Propulsion (pp. 135–164). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-69203-4_5
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