Performance verification of a laboratory scale hydrogen/oxygen combustion chamber [PDF]
Hydrogen, Fuel Cell & Energy Storage, 2022 Liquid propellant missiles are commonly applied to launch satellites that must be located in upper orbits. These systems normally use hydrogen and oxygen propellants that are non-hypergolic mixtures.
Ali Saberimoghaddam*, Elahe Basafa
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Green Hypergolic Ionic Liquids: Future Rocket Propellants
Journal of Ionic Liquids, 2022 Hydrazine and its derivatives have been used as standard propellants for spacecraft propulsion systems since the 1960s, despite being highly toxic and carcinogenic. The propellant synthesis community has constantly been looking for green alternatives for
Umakant Swami +2 more
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Theoretical and Experimental Heat of Combustion Analysis of Paraffin-Based Fuels as Preburn Characterization for Hybrid Rocket [PDF]
Journal of Aerospace Technology and Management, 2020 The energy characteristics and theoretical performance of the hybrid rocket fuels are discussed in this paper. Aluminum (Al) and boron (B) metal additives were used to increase the energy density of the paraffin-based solid fuels.
Yash Pal +2 more
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Study on the Influence of Nozzle Ablation on the Performance of the Solid Rocket Motor
Aerospace, 2023 As a key component of the solid rocket motor, nozzle ablation is very important to the performance of the motor. In order to study the influence of the law of nozzle ablation on motor performance, a two-dimensional axisymmetric model of a ground state ...
Weiqiang Huang +4 more
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Mathematical modeling of plasma thruster device thermal processes [PDF]
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", 2022 A mathematical model of thermodynamic processes occurring in the arcjet thruster device with using argon for arcjet working process carring out. A comparative analysis of the results of experimental data with theoretical data has been carried out. The
V. V. Shalay +2 more
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Technological advancements in Pulse Detonation Engine Technology in the recent past: A Characterized Report [PDF]
INCAS Bulletin, 2019 Pulse Detonation Engine (PDE), is an emerging and promising propulsive technology all over the world in the past few decades. A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust the fuel and oxidizer ...
Bharat Ankur DOGRA +3 more
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Performance Assessment of Fuels TMEDA-DMAZ and Tonka250 with Liquid Oxidizer AK27 [PDF]
Iranian Journal of Chemistry & Chemical Engineering, 2023 Tonka250 is a liquid fuel containing equal percentages of triethylamine and xylidine which has attracted the attention of space industries due to its favorable performance characteristics.
Hossein Rouhandeh +3 more
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Rocket Solid Propellant Alternative Based on Ammonium Dinitramide [PDF]
INCAS Bulletin, 2017 Due to the continuous run for a green environment the current article proposes a new type of solid propellant based on the fairly new synthesized oxidizer, ammonium dinitramide (ADN).
Grigore CICAN, Alexandru-Daniel MITRACHE
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Using the Impulse Method to Determine High-Pressure Dynamic Burning Rate of Solid Propellants
Aerospace, 2023 A new method for determining the burning rate of a solid propellant, called the Impulse Method, is proposed in this paper. It is based on the proportional relationship between the impulse generated and the mass of the burned propellant. The pressure–time
Jiahao Liu +3 more
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Pulsed Detonation Hydroramjet: Design Optimization
Journal of Marine Science and Engineering, 2022 A new type of marine transportation engine, the pulsed detonation hydroramjet (PDH), which was first designed, manufactured, and tested by the present authors, has been further investigated in terms of the potential improvement of its propulsive ...
Sergey M. Frolov +5 more
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