Approaches to low fuel regression rate in hybrid rocket engines
D Pastrone - International Journal of Aerospace Engineering, 2012 - Wiley Online Library
Hybrid rocket engines are promising propulsion systems which present appealing features
such as safety, low cost, and environmental friendliness. On the other hand, certain issues …
such as safety, low cost, and environmental friendliness. On the other hand, certain issues …
On use of hybrid rocket propulsion for suborbital vehicles
A Okninski - Acta Astronautica, 2018 - Elsevier
While the majority of operating suborbital rockets use solid rocket propulsion, recent
advancements in the field of hybrid rocket motors lead to renewed interest in their use in …
advancements in the field of hybrid rocket motors lead to renewed interest in their use in …
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers—A Short Review
Hybrid rocket engines (HREs) offer a low-cost, reliable, and environmentally friendly solution
for both launch and in-space applications. Hybrid propellants have been identified as green …
for both launch and in-space applications. Hybrid propellants have been identified as green …
Testing of a long-burning-time paraffin-based hybrid rocket motor
E Paccagnella, M Santi, A Ruffin, F Barato… - Journal of Propulsion …, 2019 - arc.aiaa.org
One of the main issues that prevents the widespread use of hybrid propulsion is the low
regression rate of classical hybrid fuels. Recently, paraffin-based fuels have been proposed …
regression rate of classical hybrid fuels. Recently, paraffin-based fuels have been proposed …
Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain
H Tian, X Li, P Zeng, N Yu, G Cai - Acta Astronautica, 2014 - Elsevier
This paper presents three-dimensional numerical simulations and experimental studies of
the hybrid rocket motor with multi-port fuel grain. The numerical model is established based …
the hybrid rocket motor with multi-port fuel grain. The numerical model is established based …
[PDF][PDF] Development of a University-Based Simplified H₂O₂/PE Hybrid Sounding Rocket at KAIST
This paper reports development process of a university-based sounding rocket using
simplified hybrid rocket propulsion system for low-altitude flight application. A hybrid …
simplified hybrid rocket propulsion system for low-altitude flight application. A hybrid …
A computational tool for predicting hybrid rocket motor performance
B Genevieve, JF Pitot de la Beaujardiere, MJ Brooks - R&D Journal, 2017 - scielo.org.za
ABSTRACT A model is described to aid in the design of hybrid rockets and in the prediction
of motor performance, specifically with respect to the University of KwaZulu-Natal's Phoenix …
of motor performance, specifically with respect to the University of KwaZulu-Natal's Phoenix …
Performance sensitivity study on a blowdown nitrous oxide paraffin wax hybrid sounding rocket
A hybrid rocket design methodology is dependent on a number of factors, such as mission
requirements and resource availability and thus no single solution exists. An in-house …
requirements and resource availability and thus no single solution exists. An in-house …
Regression rate performance of paraffin wax and bees wax–Gox with varied grain configuration in a hybrid rocket motor
V AR - Aircraft Engineering and Aerospace Technology, 2021 - emerald.com
Purpose This paper aims to determine the regression rate using wax fuels for three different
grain configurations and find a suitable grain port design for hybrid rocket application …
grain configurations and find a suitable grain port design for hybrid rocket application …
[PDF][PDF] Performance characterisation of metal additives in paraffin wax hybrid rocket fuel grains.
CS Maharaj - 2018 - core.ac.uk
Abstract The Aerospace Systems Research Group (ASReG) at the University of KwaZulu
Natal is actively develo** sounding rockets in the Phoenix Hybrid Sounding Rocket …
Natal is actively develo** sounding rockets in the Phoenix Hybrid Sounding Rocket …