Paraffin-based fuel has a great potential for several innovative missions, including space
tourism, due to its safety, low environmental impact, high performance and low cost. Despite …

Combustion instability is investigated in a model chamber by changing the recess length of
a gas-centered swirl coaxial injector ranging from 0 mm to 20 mm with a 4 mm interval …

The physical, thermal and ballistic performance of paraffin-based fuel loaded with aluminum
(Al) additive was investigated. The paraffin-based fuels were prepared using varying weight …

Hybrid rockets are entitled with unique features such as simplicity, thrust modulation, safety,
and low cost compared to that of conventional liquid and solid rockets. Despite their distinct …

Based on the experimental and numerical methods, parametric studies on annulus width
and post thickness of a liquid-centered swirl coaxial (LCSC) Injector were performed under …

Rocket fuels are subjected to intense in-flight inertial, pressure and thermal loads that has
drastic effect on its performance. In order to achieve optimal results, we require functionally …

Hybrid rocket fuels are considered safer compared to solid and liquid based rocket fuels due
to operational and handling reasons. The thermal stability and combustion capability are …

Analytic methods are applied to investigate the dynamic behaviors of the model chambers
with different lengths. They are dynamic mode decomposition (DMD), short-time Fourier …

Self-pulsation characteristics of a liquid-centered swirl coaxial (LCSC) injector are
investigated numerically based on the coupled volume of fluid VOF and Level Set (CLSVOF) …

This study investigates the effects of injector spacing and momentum flux ratio on
combustion instability in a model chamber with single and two injectors, both experimentally …