Separation nuts are widely used as release devices to fasten and separate substructures of
launching systems in aerospace applications. High shock transient response is generated …

Spacecraft are subjected to severe mechanical loads, especially during the ascent phase of
the launch. Among several vibrational environments, shock loads, which are caused mainly …

In this study, we investigate nonlinear dynamics of the autonomous separation deployment
maneuver for a space multi-rigid-body system with uncertain-but-bounded parameters by …

This review presents an in-depth examination of the advancements, current state, and future
trends of separation and release devices in aeronautical and astronautical systems …

The shear pin structure is widely used in aeronautics and astronautics structures to deal with
emergency structure separation problems. The shear pin design has a strict restriction on …

This paper presents a multidisciplinary structural optimization approach to design separation
nuts with low-level pyroshock responses for aerospace. A parametric modeling method is …

In this paper, a mathematical model is developed to estimate specifications of a clamp band
joint by taking into account full effects of the uncertainty of the joint parameters with a …

In this paper, based on the development of the non-pyrotechnic low impact connection and
separation device for heavy load connection of large space vehicles, the design method of …

Shock severity measure is the main concern of this study, which is a key component in the
entire shock design and verification process. To simplify the research problem, this study …

Uncertainties of the parameters cause the behavior of the systems to statistical distribution
and change from what is expected. Therefore, in complex and sensitive systems, such as …