Published October 1, 2017 | Version v1
Journal article

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/249/1/012015

Additional details

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