1. Optimisation and performance evaluation of an environmentally friendly rocket composite propellant
- Author
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Funsho Alaba Akeredolu, Jacob Ademola Sonibare, Jamiu Adetayo Adeniran, Gbadebo Omoniyi Adeniyi, and A. J. Adesanmi
- Subjects
Propellant ,animal structures ,Materials science ,business.product_category ,musculoskeletal, neural, and ocular physiology ,General Chemical Engineering ,technology, industry, and agriculture ,Opacifier ,Thrust ,macromolecular substances ,02 engineering and technology ,010501 environmental sciences ,Characteristic velocity ,Combustion ,01 natural sciences ,020401 chemical engineering ,Rocket ,Specific impulse ,Response surface methodology ,0204 chemical engineering ,Composite material ,business ,0105 earth and related environmental sciences - Abstract
This paper investigated the effects of laboratory synthesised rocket composite propellants’ formulations on propellant performance parameters using response surface methodology (RSM). For the sake of a safe environment, the propellant is made of chemical constituents that have less severe effects on air quality. Experimental measurements of propellant performance parameters were carried out using the ballistic evaluation method. The thrust generated during combustion, the burn time and the propellant combustion temperature were measured using a data acquisition facility equipped with a button load cell and a thermocouple. Specific impulse, density, temperature, characteristic velocity, molecular weight and heat ratio were computed from the measured parameters. The resulting optimum rocket composite propellant formulations were 65.1%, 18.1%, 9.1%, 3.6%, 2.2% and 1.9% for the oxidiser, binder, fuel, opacifier, burning rate enhancer and catalysts, respectively. The corresponding performance indices i...
- Published
- 2018
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