Visualization of Projectile Flying at High Speed in Dusty Atmosphere
- 1. Department of Advanced Energy, Graduate School of Frontier Sciences, The University of Tokyo, 5-1-5 Kashiwanoha, Kashiwa, Chiba 277-8561 (Japan)
- 2. Department of Aeronautics and Astronautics, Graduate School of Engineering, The University of Tokyo, 7-3-1 Hongo, Bunkyo, Tokyo 113-8656 (Japan)
Description
Considering a spacecraft that encounters particle-laden environment, such as dust particles flying up over the regolith by the jet of the landing thruster, high-speed flight of a projectile in such environment was experimentally simulated by using the ballistic range. At high-speed collision of particles on the projectile surface, they may be reflected with cracking into smaller pieces. On the other hand, the projectile surface will be damaged by the collision. To obtain the fundamental characteristics of such complicated phenomena, a projectile was launched at the velocity up to 400 m/s and the collective behaviour of particles around projectile was observed by the high-speed camera. To eliminate the effect of the gas-particle interaction and to focus on only the effect of the interaction between the particles and the projectile's surface, the test chamber pressure was evacuated down to 30 Pa. The particles about 400μm diameter were scattered and formed a sheet of particles in the test chamber by using two-dimensional funnel with a narrow slit. The projectile was launched into the particle sheet in the tangential direction, and the high-speed camera captured both projectile and particle motions. From the movie, the interaction between the projectile and particle sheet was clarified. (paper)
Availability note (English)
Available from http://dx.doi.org/10.1088/1757-899X/249/1/012015Additional details
Identifiers
Publishing Information
- Journal Title
- IOP Conference Series. Materials Science and Engineering (Online)
- Journal Volume
- 249
- Journal Issue
- 1
- Journal Page Range
- [9 p.]
- ISSN
- 1757-899X
Conference
- Title
- 14. international conference on fluid control, measurements and visualization
- Acronym
- FLUCOME 2017
- Dates
- 8-12 Oct 2017
- Place
- Notre Dame, IN (United States)
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 50054044
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- ATMOSPHERES; CAMERAS; COLLISIONS; CRACKING; DAMAGE; DUSTS; JETS; PARTICLE INTERACTIONS; PARTICLES; PROJECTILES; SHEETS; SIMULATION; SPACE VEHICLES; SURFACES; THRUSTERS; VELOCITY
- Descriptors DEC
- CHEMICAL REACTIONS; DECOMPOSITION; INTERACTIONS; PYROLYSIS; THERMOCHEMICAL PROCESSES; VEHICLES