@article {Igolkin:2019:0736-2935:4612,
title = "Reducing acoustic loads on a spacecraft inside a rocket fairing",
journal = "INTER-NOISE and NOISE-CON Congress and Conference Proceedings",
parent_itemid = "infobike://ince/incecp",
publishercode ="ince",
year = "2019",
volume = "259",
number = "5",
publication date ="2019-09-30T00:00:00",
pages = "4612-4621",
itemtype = "ARTICLE",
issn = "0736-2935",
url = "https://ince.publisher.ingentaconnect.com/content/ince/incecp/2019/00000259/00000005/art00064",
author = "Igolkin, Aleksandr and Popov, Pavel and Shakhmatov, Evgeniy",
abstract = "Reducing acoustic loads on complex shape objects placed inside a cylindrical shell result in design challenges. An example of such a task is accommodation of the spacecraft (SC) inside the fairing of a launch vehicle. The paper presents a mathematical model for determining acoustic
loads acting on the spacecraft depending on the acoustic absorption factor of the fairing surface, SC and the SC configuration. As a result, we have received spectra of root-mean-square acoustic pressure levels which make it possible to adapt this SC to the requirements of the fairing.",
}