In recent decades, solid fuel combustion propulsion of spacecraft has become one of the
most popular choices for rocket propulsion systems. The reasons for this success are a wide …

During launch vehicle ascent, the base flow regimes of multi-nozzle rockets become
increasingly complex owing to plume interactions. We developed a numerical method using …

The thermal radiation of micron-sized condensed phase particles plays a dominant role
during the heat transfer process in aluminized Solid Rocket Motors (SRMs). Open research …

Although there are several studies existing in the literature modeling the infrared radiation
signatures of solid motor rocket plumes, none of them investigate the effect of some …

In this paper, the design and implementation of a proposed visual system, based on laser
spectroscopy (LS) of the products of solid missile fuel combustion (MFC), is one of the most …

Currently, none of the steady-state and transient bubbling fluidized bed combustor models
couples the solution of the radiative transfer equation with the solution of conservation …

In recent decades, solid fuel combustion propulsion of spacecraft has become one of the
most popular choices for rocket propulsion systems. The reasons for this success are a wide …

In this paper, present a unique model of a comprehensive spectrograph Systems. the
proposed optical system evaluates the performance of solid fuel columns SFC on the basis …

Line-of-sight spectral observations in the near ultraviolet regime are made of the high-speed
afterburning exhaust plume from a lab-scale rocket simulator which reacts gaseous H 2 with …

The thermal radiation signature produced by rocket engine exhaust plumes is a challenging
phenomenon to analyze. The thermal emissions are affected by several characteristics, such …