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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Rocket Flight Path by Jamie Waters

“…This project uses Newton’s Second Law of Motion, Euler’s method, basic physics, and basic calculus to model the flight path of a rocket. From this, one can find the height and velocity at any point from launch to the maximum altitude, or apogee. …”
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Rocketing to Energy Sustainability by David LePoire

“…This metaphor is constructed based similarity of a rocket’s and civilization’s transition from one stable state to another at a higher level accomplished using a limited supply of fuel. …”
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Electric Rocket Launcher Aircraft—Drone-Launched Short Range Rocket System by Mikhail Shubov

Subjects: “…electric-pump-fed rocket engine…”
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CEEMD-MultiRocket: Integrating CEEMD with Improved MultiRocket for Time Series Classification by Panjie Wang, Jiang Wu, Yuan Wei, Taiyong Li

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Design and fabricate rocket engine by Tg Kamarul Azhan, Tg Kamaruddin

“…The objective of this project is to design and fabricate the Rocket Engine.This project describe the shape of Rocket that will fabricate follow the dimension that give by my supervisor.Actually there a several type of Rocket Engine.There are Rocket Engine based of thermal,water,hybrid,solid,and resistojet(electronic).So,the Rocket that will fabricate is from the solid type.One of the important thing a rocket is type of noozle,from the research in the internet De’Laval Noozle is the better type of noozle to use.Then material also another important thing in making Rocket.Material that will use must have good enough strenght to hold the explosion that will happen to move up the rocket.The better material is Stainless Steel it is light and have a good strenght,but cause of limited soucrce the material that use for make this Rocket is from mild steel.It is also have good strenght but it heavy than stainless steel.This project start from making the design and make it using Solid Work Software.Finish the design then the rocket can be made use a Lathe Machnine.Majority this rocket will be made by Lathe Machine.But from the start of fabricte the machine that involve also like bendsaw and drilling machine.Rocket engine that will be made have three part.First part is cap to close the hole on the upper body,a body and noozle.All this part will be assembly and were tied by bolt.It was susessfully done and able to function as needed.…”
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Development of solid rocket propellant by Mohammad Norshim, Mohamed Hashim

“…Rocket propellant has been identified as a component that played an important role in the development of rockets. …”
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Rocket Motor with Composite Casing by Zbigniew Drabik, Tomasz Rasztabiga

Subjects: “…two-stage rocket…”
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Dynamic Analysis of Rockets Launcher by Dragoljub Vujic*, Vlado Djurkovic, Nikola Milenkovic, Slavisa Trajkovic

Subjects: “…rocket launcher…”
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Rocket Lab Mission to Venus by Richard French, Christophe Mandy, Richard Hunter, Ehson Mosleh, Doug Sinclair, Peter Beck, Sara Seager, Janusz J. Petkowski, Christopher E. Carr, David H. Grinspoon, Darrel Baumgardner, on behalf of the Rocket Lab Venus Team

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Artillery and rocket support in operations by Jotić Slaviša M., Slavković Rade V.

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CONDUCTING RESEARCH: IS IT ROCKET SCIENCE? by Ilke Coskun Benlidayi

“…CONDUCTING RESEARCH: IS IT ROCKET SCIENCE?…”
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Lung rockets and pulmonary functions by Sherif R. A. El-Fatah, Radwa A. El-Hefny, Randa I. Ahmed, Doaa M. A. El-Tawab

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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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Hydrogen peroxide – A promising oxidizer for rocket propulsion and its application in solid rocket propellants by Wioleta Kopacz, Adam Okninski, Anna Kasztankiewicz, Paweł Nowakowski, Grzegorz Rarata, Pawel Maksimowski

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THE PROBLEM OF THE OPTIMIZATION THE DESIGN PARAMETERS AND CONTROL PROGRAMS OF THE CONTROLLED ROCKET WITH SOLID PROPELLANT ROCKET ENGINE by Светлана Васильевна Сюткина-Доронина

“…The complex problem of the simultaneous optimization of the control programs and design parameters of the controlled single-stage rocket with cruise solid propellant rocket engine is formulated. …”
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Development of a rocket recovery system by Nur Fitrina, Mat Nawi

“…The design, fabricate and testing of a rocket recovery system is presented in this report. …”
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Drone Launched Short Range Rockets by Mikhail V. Shubov

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STABILIZATION OF ROCKET MOTION UNDER UNCERTAINTY by Вольт Васильович Авдєєв

“…The article deals with the support of the guaranteed stability factor of a stabilizing system (SS) for the rocket motion under uncertainty of coefficients in the mathematical model and absence of their stable statistical characteristics. …”
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Genetic Algorithm Application in Guided Rockets by AliReza Rezaei

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