Interior ballistics simulation of projectile launch system utilizing tubular solid propellant

H. Miura, Akiko Matsuo, Y. Nakamura

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

Two-dimensional axisymmetric interior ballistics simulations in the projectile launch system utilizing long slotted tubular solid propellant are carried out using solid/gas two-phase fluid dynamics code of Eulerian-Lagrangian approaches. The movement of slotted tubular solid propellant is simulated one-dimensionally by Lagrangian approach. The simulation results are compared with experimental data for validation. The histories of the breech pressure and projectile velocity under various conditions are in good agreement with the experimental data. We examine the effects of the projectile and propellant mass conditions on the energy release rate of solid propellant and the projectile kinetic energy at the muzzle. A series of the simulations by changing the mass of projectile and propellant clarifies that the launch system requires the heavier projectile for ensuring the sufficient time of the projectile staying in the launch tube to convert efficiently the propellant chemical energy to the projectile kinetic energy.

Original languageEnglish
Title of host publication44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Publication statusPublished - 2008
Event44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit - Hartford, CT, United States
Duration: 2008 Jul 212008 Jul 23

Other

Other44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
CountryUnited States
CityHartford, CT
Period08/7/2108/7/23

Fingerprint

interior ballistics
solid propellants
Solid propellants
Projectiles
Ballistics
projectiles
simulation
propellants
Propellants
kinetic energy
Kinetic energy
fluid dynamics
chemical energy
energy
propellant
Energy release rate
Fluid dynamics
histories
tubes
history

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering
  • Space and Planetary Science
  • Energy(all)
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Miura, H., Matsuo, A., & Nakamura, Y. (2008). Interior ballistics simulation of projectile launch system utilizing tubular solid propellant. In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Interior ballistics simulation of projectile launch system utilizing tubular solid propellant. / Miura, H.; Matsuo, Akiko; Nakamura, Y.

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 2008.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Miura, H, Matsuo, A & Nakamura, Y 2008, Interior ballistics simulation of projectile launch system utilizing tubular solid propellant. in 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford, CT, United States, 08/7/21.
Miura H, Matsuo A, Nakamura Y. Interior ballistics simulation of projectile launch system utilizing tubular solid propellant. In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 2008
Miura, H. ; Matsuo, Akiko ; Nakamura, Y. / Interior ballistics simulation of projectile launch system utilizing tubular solid propellant. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 2008.
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