Results 31 to 40 of about 14,246 (239)

A LABSCALE HYBRID ROCKET MOTOR IGNITION SYSTEM [PDF]

The International Conference on Applied Mechanics and Mechanical Engineering, 2012
ABSTRACTThe hybrid propulsion has the superiority of safety (Non-explosive), simplicity (highreliability), low environmental pollution and available technology over traditional solidand liquid propulsion, all these benefits have a tendency to low cost and laboratorywork.
A. Makled, H. Mostafa, M. Al-Sanabawy, M. Al-Timimi   +3 more
openaire   +1 more source

Beeswax–EVA/Activated-Charcoal-Based Fuels for Hybrid Rockets: Thermal and Ballistic Evaluation

Energies, 2022
Beeswax (C46H92O) is a naturally derived substance that has the potential to be used as a solid fuel for hybrid rocket applications and as a substitute for paraffin wax fuel in hybrid rockets.
Sri Nithya Mahottamananda, Yash Pal, Mengu Dinesh, Antonella Ingenito   +3 more
doaj   +1 more source

Optimization design in single wagon-wheel fuel grain of hybrid rocket motor

FirePhysChem, 2021
The grain design of hybrid rocket motor is a design of proper fuel grain geometry and flow adjustment scheme based on the total impulse, thrust, chamber pressure, length and outer diameter of combustion chamber.
Wei Tianfang, Cai Guobiao, Tian Hui, Zhu Hao, Zhang Yuanjun, Li Xintong   +5 more
doaj   +1 more source

Hydrogen peroxide – A promising oxidizer for rocket propulsion and its application in solid rocket propellants

FirePhysChem, 2022
This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid rocket motor grains.
Wioleta Kopacz, Adam Okninski, Anna Kasztankiewicz, Paweł Nowakowski, Grzegorz Rarata, Pawel Maksimowski   +5 more
doaj   +1 more source

Numerical Simulation of Chemical Propulsion Systems: Survey and Fundamental Mathematical Modeling Approach

Aerospace, 2023
This study deals with the mathematical modeling and numerical simulation of chemical propulsion systems (CPSs). For this, we investigate and summarize a comprehensive collection of the simulation modeling developments of CPSs in academic works ...
Jihyoung Cha
doaj   +1 more source

Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors

Fire, 2023
As the research on hybrid rocket motors advances, more accurate tools are needed to estimate the performance of the system by determining its fundamental parameters. One of them is certainly the regression rate of the solid fuel.
Alessandro Rampazzo, Francesco Barato
doaj   +1 more source

Long-Duration Dynamic Numerical Simulation of Combustion and Flow in Hybrid Rocket Motors Considering Nozzle Erosion

Aerospace
Hybrid rocket motors have great development potential due to their outstanding thrust adjustment flexibility and long-term operation ability. However, nozzle erosion during the motor operation can cause an increase in the throat area of the nozzle, which
Xiangyu Meng, Hui Tian, Xiaoting Niu, Hao Zhu, Jingfei Gao, Guobiao Cai   +5 more
doaj   +1 more source

Numerical Simulations of Flow and Fuel Regression Rate Coupling in Hybrid Rocket Motors [PDF]

INCAS Bulletin, 2017
The hybrid propulsion offers some remarkable advantages like high safety and high specific impulse and thus it is considered a promising technology for the next generation launchers and space systems. The purpose of this work is to validate a design tool
Marius STOIA-DJESKA, Florin FRUNZULICA, Florin MINGIREANU   +2 more
doaj   +1 more source

Effect of tangential swirl air inlet angle on the combustion efficiency of a hybrid powder-solid ramjet [PDF]

, 2019
A new ramjet configuration using powder and solid fuel as propellant is investigated, namely, hybrid powder-solid ramjet (HPSR). Boron particles were used as the powder in this study.
ANSYS Inc, Ao, Betelin, Cai, Chang, Chelaru, Chen, dawara, Gany, Gany, Glassman, Goroshin, Haijun Sun, Hu, Humberto Medina, Hussmann, Hussmann, Jung, Kalpakli, Kazaoka, King, Li, Li, Liang, Loftus, Magnussen, Meinköhn, Morsi, Musa, Musa, NASA, Natan, Nie, Pern, Pern, Povitsky, Rashkovskiy, Rodić, Rui Jia, Sandall, Sender, Shih, Shorr, Varghese, Wang, Xia, Xia, Xu, Yeh, Yihua Xu   +49 more
core   +1 more source

METALIZED FUEL HYBRID ROCKET MOTOR PARAMETRIC STUDY [PDF]

International Conference on Aerospace Sciences and Aviation Technology, 2015
The objective of this paper is to study theoretically and experimentally the effects of different design parameters on hybrid rocket motor (HRM). HRM propellant constituents are Polyethylene (PE) with Al powder additive as solid fuel and gaseous oxygen (GO2) as oxidizer.
openaire   +1 more source