The performance of the propellant depends on its energy density, which is equal to the density of the propellant multiplied by the energy of the propellant. The actual density of composite propellant can be determined by the Archimedes Principle. And the present theoretical density of composite propellant is calculated by the assumption their component is the same phase and the mixing is homogeneous. But, the apparent density (actual density divided by theoretical density) still more significant low than 100%, which means the actual density more significant difference from the theoretical density. This paper proposed the sphere packing density theory was added to improve the calculation theoretical density of composite propellant. This method produced the result of apparent density a better value close to 100%. The improvement of the theoretical calculation method for composite propellant density can be used as a reference in making a composite propellant formulation design, checking the homogeneity of the composition mixture, and improving the propellant process method.
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13 September 2021
THE 8TH INTERNATIONAL SEMINAR ON AEROSPACE SCIENCE AND TECHNOLOGY – ISAST 2020
17 November 2020
Bogor, Indonesia
Research Article|
September 13 2021
Preliminary results of the particle packing density theory for improving the theoretical density of composite propellant Available to Purchase
Bayu Prianto;
Bayu Prianto
a)
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
a)Corresponding author: [email protected]
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Henny Setyaningsih;
Henny Setyaningsih
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
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Anita Pinalia
Anita Pinalia
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
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Bayu Prianto
a)
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
Henny Setyaningsih
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
Anita Pinalia
Thermochemical Laboratory of Rocket Technology Centre, National Institute of Aeronautics and Space (LAPAN)
- Indonesia
a)Corresponding author: [email protected]
AIP Conf. Proc. 2366, 040008 (2021)
Citation
Bayu Prianto, Henny Setyaningsih, Anita Pinalia; Preliminary results of the particle packing density theory for improving the theoretical density of composite propellant. AIP Conf. Proc. 13 September 2021; 2366 (1): 040008. https://doi.org/10.1063/5.0060448
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