A mathematical model for the separation behavior of a split type low-shock separation bolt. (November 2019)
- Record Type:
- Journal Article
- Title:
- A mathematical model for the separation behavior of a split type low-shock separation bolt. (November 2019)
- Main Title:
- A mathematical model for the separation behavior of a split type low-shock separation bolt
- Authors:
- Hwang, Dae-Hyun
Han, Jae-Hung
Lee, Juho
Lee, YeungJo
Kim, Dongjin - Abstract:
- Abstract: Pressure cartridge type separation devices which are widely used in fairing, stage separations of space launch systems, and many other aerospace fields generate much lower pyroshock and produce no high-speed debris compared to frangible explosive separation devices. However, because the operation is completed in a few milliseconds and the releasing mechanism is complicated, their separation behavior is difficult to experimentally identify. This paper presents a mathematical model to simulate the separation behaviors for a split-type separation bolt, one of the pressure cartridge type separation devices. The mathematical model includes a combustion model, buckling resisting model, split behavior model related to static and dynamic friction, O-ring friction model, contact force model, and slip angle model. Each composing models are obtained by mathematical formulation or numerical analysis. An efficient contact model is constructed by using virtual penetration model appropriately for complex contact phenomenon. To validate the established model, separation experiments were performed; the results are then compared with the mathematical model. Present study show that complex mechanical behaviors coupled with combustion of solid propellant charge can be efficiently simulated by the mathematical model. Highlights: Established a mathematical model for a low-shock separation device using pressure cartridge. Analyzed complicated separation behavior of the low-shockAbstract: Pressure cartridge type separation devices which are widely used in fairing, stage separations of space launch systems, and many other aerospace fields generate much lower pyroshock and produce no high-speed debris compared to frangible explosive separation devices. However, because the operation is completed in a few milliseconds and the releasing mechanism is complicated, their separation behavior is difficult to experimentally identify. This paper presents a mathematical model to simulate the separation behaviors for a split-type separation bolt, one of the pressure cartridge type separation devices. The mathematical model includes a combustion model, buckling resisting model, split behavior model related to static and dynamic friction, O-ring friction model, contact force model, and slip angle model. Each composing models are obtained by mathematical formulation or numerical analysis. An efficient contact model is constructed by using virtual penetration model appropriately for complex contact phenomenon. To validate the established model, separation experiments were performed; the results are then compared with the mathematical model. Present study show that complex mechanical behaviors coupled with combustion of solid propellant charge can be efficiently simulated by the mathematical model. Highlights: Established a mathematical model for a low-shock separation device using pressure cartridge. Analyzed complicated separation behavior of the low-shock separation device. Simulation results were well compared with separation experimental results. … (more)
- Is Part Of:
- Acta astronautica. Volume 164(2019)
- Journal:
- Acta astronautica
- Issue:
- Volume 164(2019)
- Issue Display:
- Volume 164, Issue 2019 (2019)
- Year:
- 2019
- Volume:
- 164
- Issue:
- 2019
- Issue Sort Value:
- 2019-0164-2019-0000
- Page Start:
- 393
- Page End:
- 406
- Publication Date:
- 2019-11
- Subjects:
- Pyrotechnics -- Pyroshock -- Separation bolt -- Mathematical model -- Low-shock separation mechanism
Astronautics -- Periodicals
Outer space -- Exploration -- Periodicals
Astronautics
Periodicals
629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2019.07.035 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 12132.xml