Determining Potassium Nitrate performance as solid rocket propellant for rocket engine by Dahalan, Md. Nizam, Mohd Jaafar, Mohd Nazri, Wan Ali, Wan Khairuddin, Mamat, Rizalman, Abd. Ghani, Mohd Shaiful Azman

“…Research and development on solid rocket propellant were carried out extensively on the whole process of production and performance testing. …”
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Propellant development for small rockets by Rahmat, Mohd. Zaki Yamani, Mohd. Jaafar, Mohammad Nazri, Abdul-Latif, Ainullotfi, Wan Ali, Wan Khairuddin, Mat Yajid, Zuriana Mariati, Kimsin, Intan Noryanah

“…The solid propellant rocket is the basis for most recent rocket inventions where it is utilized mostly in military rockets. …”
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Development of solid rocket propulsion system at UTM by Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin, Dahalan, Md. Nizam, Mamat, Rizalman

“…Rockets have been used from as early as the thirteenth century as fireworks and weapons. …”
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Development of solid rocket propulsion system at UTM by Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin, Dahalan, Md. Nizam

“…Rockets have been used from as early as the thirteenth century as fireworks and weapons. …”
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Ballistic properties of a polybutadiene propellant for rocket application by Ang, Kiang Long

“…Hydroxy-terminated polybutadiene (HTPB) based propellant is a complex chemical reagent used for rocket propulsion, and changes in the chemical formulation can significantly affect the propellant ballistic performance. …”

Combustion characterization of ammonium perchlorate based solid rocket propellant by Aziz, Amir

“…There were many studies on ammonium perchlorate (AP) based solid rocket propellant (SRP) and some data already exist. …”
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Development of a computer program for rocket aerodynmic coefficients estimation by Dahalan, Md. Nizam, Su, Vin Cent, Ammoo, Mohd. Shar

“…A computational method has been developed to realize an efficient and accurate user friendly computational program called RocketCalculator, which integrates carefully assessed methodologies and offer flexibilities of the rocket configurations and velocities up to Mach number 3.0 and angle of attack of 25 degrees. …”
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Design and development of a hydrogen-peroxide rocket-engine facility by Krishnan, Subramaniam, Ahn, Sang-Hee, Lee, Choong-Won

“…Addressing the first two points resulted in successful firing of the rocket engine…”
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Development of a 100-n hydrogen peroxide rocket engine by Krishnan, S., Lee, Choong Won

“…Addressing the first two points resulted in successful firing of the rocket engine.…”
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Design and development of 50-N hydrogen peroxide monopropellant rocket thruster by Othman, Norazila

Advances in aluminum powder usage as an energetic material and applications for rocket propellant by Sadeghipour, S., Ghaderian, J., Abdul Wahid, Mazlan

“…Different sizes of aluminum powders are employed to produce composite rocket propellants with the bases of Ammonium Perchlorate (AP) and Hydroxyl-Terminated-Polybutadiene (HTPB) as oxidizer and binder respectively. …”

Development of a 10 newton hydrogen peroxide monopropellant rocket thruster by Nambaraja, Kuberaraaj

“…Therefore, a 10 Newton rocket thruster has been designed and fabricated. …”
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Advances in aluminum powder usage as an energetic material and applications for rocket propellant by Sadeghipour, Sakineh, Ghaderian, Javad, A. Wahid, Mazlan

“…Different sizes of aluminum powders are employed to produce composite rocket propellants with the bases of Ammonium Perchlorate (AP) and Hydroxyl-Terminated-Polybutadiene (HTPB) as oxidizer and binder respectively. …”

Aerodynamic study of air flow over a curved fin rocket by Dahalan, M. N., Suni, A. F., Ishak, I. S., Mohd., N. A. R. N., Mat, S.

“…This paper summarizes a study of the aerodynamic characteristics of a curved fin rocket. The study was conducted with the use of semi-empirical method and numerical simulation. …”

Experimental solid and liquid propellant rocket development in Universiti Teknologi Malaysia: 1992-2011 by Wan Ali, Wan Khairuddin, Kiang, Long Ang, Mohd. Jaafar, Mohammad Nazri

“…This paper reports on the research and development activities related to the experimental solid and liquid propellant rocket in Universiti Teknologi Malaysia (UTM) from year 1992 to 2011. …”
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Development of solid rocket propellant based on Isophorone Diisocyanate - Hydroxyl terminated natural rubber binder by Onn, Munirah, Md. Nor, Hussin, Wan Ali, Wan Khairuddin

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Synthesis and characterization of hydroxyl terminated epoxidized natural rubber as a binder for solid rocket propellant by Abdul Razak, Nor Erma Shuhadah

“…Therefore, it is expected that HTENR is suitable to be used as a binder in solid rocket propellant.…”
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Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant by Ab Wahid, Mastura, Wan Ali, Wan Khairuddin

“…The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. …”

Control of vibrational power input to semi-infinite anisotropic beam by Dahalan, Md. Nizam, Su, Vin Cent, Ammoo, Mohd. Shariff

“…A computational method has been developed to realize an efficient and accurate user friendly computational program called RocketCalculator, which integrates carefully assessed methodologies and offer flexibilities of the rocket configurations and velocities up to Mach number 3.0 and angle of attack of 25 degrees. …”
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Fabrication of ceramic nozzle made from clay-alumina mixture by Rosli, Muhamad Nurizad

“…Heat transfer from hot gases to the chamber and nozzle walls, can result in weakening the rocket casing. Thus proper and complete insulation is needed to protect the casing material from reaching melting temperature or become damaged at elevated temperature. …”
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