Javascript must be enabled to continue!
Improvement of Composite Propellants Energy Using Explosive Materials
View through CrossRef
Composite propellants are energetic materials have ability to ignite, burn fast and cause several simultaneous exothermic chemical reactions which produce huge amounts of gases under high pressures and temperatures which can spread spontaneously. 1n the present study, the explosive material hexogen (Cyclo tri-methylene tri-nitramine) was used to improve the performance properties of composite propellants, especially the specific impulse. For several formulations of hexogen at different added percentages, the specific impulse was calculated using thermodynamic calculations program of composite propellants. The results given were compared with those formulations not including hexogen. It was seen that; hexogen caused a significant positive effect in the specific impulse. Accordingly, the energy of composite propellant was improved positively in the samples containing hexogen till 40% of the oxidizer ratio. Also, it was noticed that the specific impulse began to decrease gradually for the oxidizers containing more than 40% of hexogen which caused in a decreasing of composite propellant energy. Finally, it was concluded that, the use of some amount of explosive materials like hexogen can improve composite propellants energy successfully.
Title: Improvement of Composite Propellants Energy Using Explosive Materials
Description:
Composite propellants are energetic materials have ability to ignite, burn fast and cause several simultaneous exothermic chemical reactions which produce huge amounts of gases under high pressures and temperatures which can spread spontaneously.
1n the present study, the explosive material hexogen (Cyclo tri-methylene tri-nitramine) was used to improve the performance properties of composite propellants, especially the specific impulse.
For several formulations of hexogen at different added percentages, the specific impulse was calculated using thermodynamic calculations program of composite propellants.
The results given were compared with those formulations not including hexogen.
It was seen that; hexogen caused a significant positive effect in the specific impulse.
Accordingly, the energy of composite propellant was improved positively in the samples containing hexogen till 40% of the oxidizer ratio.
Also, it was noticed that the specific impulse began to decrease gradually for the oxidizers containing more than 40% of hexogen which caused in a decreasing of composite propellant energy.
Finally, it was concluded that, the use of some amount of explosive materials like hexogen can improve composite propellants energy successfully.
Related Results
NONLINEAR STATIC ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS
NONLINEAR STATIC ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS USING ANALYSIS OF COMPOSITE SHELLS
This paper presents the results of the geometric nonlinear analysis of composite shell subjected to static load by using an edge-based smoothed finite elements (ES) and the mixed i...
Solid Propellants
Solid Propellants
AbstractSolid propellants are widely used in rocket propulsion applications. They are often tailored by specific applications such as space launchers, missiles, and guns. Solid pro...
Experimental Study on Underwater Explosive Weld Interface and Mechanical Properties of Carbon Steel–Stainless Steel
Experimental Study on Underwater Explosive Weld Interface and Mechanical Properties of Carbon Steel–Stainless Steel
ABSTRACTTo investigate the influence of the thickness of the intermediate water layer and the thickness of the explosive on the quality of underwater explosive welding of Q235R car...
Characterization of ADN and ADN‐Based Propellants
Characterization of ADN and ADN‐Based Propellants
AbstractAmmonium dinitramide (ADN), NH4N(NO2)2 is being considered as one of the potential new energetic oxidizers for composite propellants. In this study, ADN crystals, prills an...
Research progress in data-driven constitutive modeling of composite solid propellants
Research progress in data-driven constitutive modeling of composite solid propellants
With the continuous advancement of technology, composite solid propellants play an increasingly widespread and crucial role in fields such as aerospace and military applications. A...
THE EFFECT OF PLYOMETRICS TRAINING ON EXPLOSIVE POWER OF MEDICAL STUDENTS IN DIPONEGORO UNIVERSITY
THE EFFECT OF PLYOMETRICS TRAINING ON EXPLOSIVE POWER OF MEDICAL STUDENTS IN DIPONEGORO UNIVERSITY
Introduction : Explosive power are the combination maximum strength and maximum velocity. High value of muscle strength and velocity can lead to good measurement of explosive power...
Characterization of the Plasticized GAP/PEG and GAP/PCL Block Copolyurethane Binder Matrices and its Propellants
Characterization of the Plasticized GAP/PEG and GAP/PCL Block Copolyurethane Binder Matrices and its Propellants
AbstractThough glycidyl azide polymer (GAP) is a well‐known and promising energetic polymer, propellants based on it suffer from poor mechanical and low‐temperature properties. To ...
Numerical Modelling of Shock Initiation of a HNIW‐Based Explosive
Numerical Modelling of Shock Initiation of a HNIW‐Based Explosive
AbstractTo investigate shock‐to‐detonation transition (SDT) characteristics of a HNIW‐based explosive, a rate law based on the Forest Fire model was calibrated by conducting five w...

