Hello Bisola,

Regrettably I know of no binding standard that launch vehicles abide by.

It's generally a matter of accommodating the acoustic and vibrational loads that your chosen launch vehicle impose *on* the payload, rather than the launcher conforming to some standard.

Most (all?) launch vehicles will have their acoustic spectra listed in their user manuals - take them with a pinch of salt and engineer in robust margins.

Oh, and test.

Always test.

Here's an example of such a spectrum.

https://www.northropgrumman.com/wp-content/uploads/Pegasus-User-Guide-1.pdf

(p32)

Normally this comes with the launcher specification. Also, I think NASA and other space agencies have standard generic noise curve.

Hi Bisola,

Undoubtedly, the intensity of vibrations will be greater at the takeoff time and acceleration of spacecraft. In constant speed mode, everything sounds good. Such as gas centrifuge system for different phases that have different stability conditions, and here we use systems can certifies stability of the centrifugal high-speed rotating machine with high reliability. To create stability in systems with high acceleration and direct or linear movement, it is very necessary to install a mechanical system to reduce the vibrations of the system body and especially the internal compartment containing mankind. There are standards and boundaries to determine the maximum tolerable vibration based on Design Basic Accidents for transient states. As in space fantastic films, similar cases are seen when passing through places with strong gravitational force.

please follow this link below:

http://www.klabs.org/DEI/References/design_guidelines/design_series/1259.pdf