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

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 …

This paper focuses on the research on regression rate of hybrid rocket motor with single-port
wagon wheel fuel grain. Both experiment and numerical investigations are carried out to …

This paper extensively reviews hybrid rocket propulsion-related activities from combustion
engine designs to launch tests. Starting with a brief review of rocket propulsion development …

This study demonstrated the performance of flight control systems of a hybrid rocket in a
hovering flight test by developing a rocket designated HTTP-3AT powered by High Test …

The mechanical and combustion properties of metal-nested composite hybrid rocket fuel
grains composed of spiral aluminium (Al) frameworks fabricated using three-dimensional …

The objective of this paper is to design a two stage sounding rocket and its nozzles using
fusion 360 and analysis of different properties using simulation on ANSYS software. The …

A non-intrusive method for determining the time-resolved fuel mass flow rate in a hybrid
rocket engine is proposed based on tunable diode laser absorption spectroscopy (TDLAS) …

Hybrid rocket motors (HRMs) easily achieve variable thrust by changing oxidizer mass flow
rate. This paper represents numerical and experimental studies on the throttleable HRM with …