Department of Space and Upper Atmosphere Research Commission, Pakistan
Research Article
Determination of Acoustic Characteristics of Melamine foam with
Experimental Validation
Author(s): Behzad Ahmed Zai*, Saad Sami and Rashid Ali
Space launch vehicles experience severe dynamic loadings throughout the flight. Acoustic loads are one such load
that is very critical to the launch vehicle at the time of ignition and take off. The amplitudes of acoustic loadings are
generally very high and required to be diminished to save electronic components. Typically, one of the most common
and efficient insulating materials is Melamine Foam (MF). This paper analyses the acoustic and environmental
noise reduction using MF panels of variable thicknesses (25, 50, and 75 mm). Commercial FEA software is used
to estimate the acoustic parameters, which are experimentally, validated using an impedance tube based on the
transfer matrix method. The impedance tube can measure the normal incident sound absorption coefficient and
transmission loss for the frequency range of 64 Hz to 6.2 kHz. A conventional, two-.. View more»