Results 91 to 100 of about 412,817 (220)

Rocket Rocket Ship

open access: yes, 2014
ColourRocket Rocket ...

core  

Numerical simulation study of aluminum particle evaporation combustion process based on SPH method

open access: yesAIP Advances
A large variety of metal fuels is usually added to the modern solid rocket propellants to improve the propellant energy and motor specific impulse and to suppress high frequency unstable combustion. Among them, aluminum is the most common additive.
Du-dou Wang   +3 more
doaj   +1 more source

A lumped kinetic model for heavy fuel oil combustion

open access: yes, 2015
The study proposes a new procedure based on the Coats-Redfern method to develop kinetic model for predicting the combustion characteristics of heavy fuel oils.
Han, Yunqing   +3 more
core  

Designing and Testing of HDPE–N2O Hybrid Rocket Engine

open access: yesEngineering Proceedings
Hybrid Rocket Engines (HREs) combine the advantages of solid and liquid propellants, offering thrust control, simplicity, safety, and cost efficiency.
Triyan Pal Arora   +6 more
doaj   +1 more source

Combustion characterization of ammonium perchlorate based solid rocket propellant [PDF]

open access: yes, 2011
There were many studies on ammonium perchlorate (AP) based solid rocket propellant (SRP) and some data already exist. However, there is no complete data available in Malaysia especially the information on the combustion characteristics of baseline data ...
Aziz, Amir
core  

Evaluation of N,N,N′,N′-Tetramethylethylenediamine (TMEDA) as an Alternative Fuel for a Hypergolic Bipropellant Rocket Engine

open access: yesFuels
Experimental research was conducted to characterize the ignition delay time and combustion performance of non-toxic reactants as a possible replacement for highly toxic fuels, such as hydrazine.
Joshua M. Hollingshead   +3 more
doaj   +1 more source

Combustion of methanol in diesel engine using diethyl ether as ignition enhancer

open access: yes, 2017
In this study, combustion of methanol in diesel engine is investigated using diethyl ether (DEE) as an ignition enhancer. Both experimental and numerical studies were performed and the results are compared with baseline diesel fuel.
Vallinayagam, R.   +5 more
core  

Experimental and numerical investigation on micro-motion characteristics of lightweight spacecraft. [PDF]

open access: yesPLoS One
Su D   +7 more
europepmc   +1 more source

Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]

open access: yesMolecules
Janowska K   +6 more
europepmc   +1 more source

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