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Acoustic protection on payload fairings of expendable launch vehicles

机译:消耗性运载火箭有效载荷整流罩的声学保护

摘要

By means of this acoustic protection it is possible to protect the payloads of expendable launch vehicles effectively against noise emissions from the rocket propulsion system which may result in damage of the payloads. For this purpose acoustic absorbers (8) tuned to a defined frequency range are provided and are arranged in foamed plastic mats (7) disposed on the insides (6) of the payload fairing (1). The acoustic absorbers (8) are composed of a cup-shaped lower part (12) and an upper part (13) having a horn (18). The horn (8) tapers in a curved-conical manner from a larger diameter (Dm) to a smaller diameter (Dt) and projects into the lower part (12) by a defined distance (a) from a bottom (14) thereof. Slits (21) for the dissipation of the directed flow energy occurring in the horn (18) are disposed in the wall of the horn in the area of the smaller diameter (Dt).
机译:借助于这种声学保护,可以有效地保护消耗性运载火箭的有效载荷免受火箭推进系统的噪声发射,该噪声可能导致有效载荷的损坏。为此目的,提供了调谐到限定频率范围的吸声器(8),并将其布置在布置在有效载荷整流罩(1)的内部(6)上的泡沫塑料垫(7)中。吸声器(8)由杯状的下部(12)和具有喇叭(18)的上部(13)构成。喇叭(8)以圆锥形的方式从较大的直径(Dm)到较小的直径(Dt)成锥形,并且从其底部(14)以限定的距离(a)伸入下部(12)。用于消散发生在喇叭(18)中的定向流动能量的狭缝(21)设置在喇叭壁中的较小直径(Dt)的区域中。

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