This paper presents the development of indigenous hybrid rocket technology, using 98%
hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with …

Hybrid rocket propulsion, first demonstrated by the Russian GIRD-09 rocket in 1933,
combines liquid oxidizer and solid fuel for thrust generation. Despite numerous advantages …

This paper presents the status of developments worldwide regarding use of hybrid rocket
motors for space transportation. Historical roots are presented and reasons for revisiting …

The combustion performance of a novel fuel grain having a nested helical structure was
experimentally investigated using a laboratory-scale hybrid rocket engine. This grain …

The low regression rate of Hybrid Rocket Engines (HREs) is one prominent characteristic
that is addressed in most abstracts concerning hybrid propulsion. Over the years …

HTPB/paraffin fuels exhibit high regression rates and excellent mechanical properties due to
the droplet entrainment and enhancement of the HTPB matrix, however, the special structure …

In this work the regression rate performance and flow physics of a lab-scale hybrid rocket
engine burning gaseous oxygen and paraffin-based fuels are experimentally and …

In the current work, Chemkin Pro's HCCI numerical model is used in order to explore the
feasibility of using hydrogen in a dual fuel concept where hydrogen peroxide acts as ignition …

A novel model for estimating the regression rate of HTPB/paraffin fuels was developed in
this work. The factors considered included the microscopic physical structure of paraffin …

In the current work, the use of hydrogen peroxide as an additive to hydrogen/air mixtures is
proposed and explored computationally, in conditions relevant to compression ignition …