2018
DOI: 10.1016/j.ijimpeng.2018.05.008
|View full text |Cite
|
Sign up to set email alerts
|

Hypervelocity impact flash and plasma on electrically biased spacecraft surfaces

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
5
0

Year Published

2019
2019
2024
2024

Publication Types

Select...
9
1

Relationship

0
10

Authors

Journals

citations
Cited by 30 publications
(8 citation statements)
references
References 15 publications
0
5
0
Order By: Relevance
“…In [10,11], simulation and analysis of the possibility of using an explosive accelerator to simulate the impact of cosmic dust stream on spacecraft materials in ground conditions. [12][13][14][15][16] presented modelling and experimental data on the interaction of high-speed bodies and particles with spacecraft materials. The authors of [17][18][19] present methods of high-speed dust particle streams acceleration.…”
Section: Sdp Modelsmentioning
confidence: 99%
“…In [10,11], simulation and analysis of the possibility of using an explosive accelerator to simulate the impact of cosmic dust stream on spacecraft materials in ground conditions. [12][13][14][15][16] presented modelling and experimental data on the interaction of high-speed bodies and particles with spacecraft materials. The authors of [17][18][19] present methods of high-speed dust particle streams acceleration.…”
Section: Sdp Modelsmentioning
confidence: 99%
“…In the third stage, the Debye length λ D is much larger than the cloud size R c ; the plasma enters the single particle motion regime, so the particles can freely expand away from the impact site. Spacecraft potential relative to the ambient plasma can suppress or enhance the escape of particles, depending on the polarities (Hew et al, ). Electrons escape faster than ions, creating two fronts of escaping charges.…”
Section: Impact Ionization and Plasma Cloud Expansionmentioning
confidence: 99%
“…A number of experimental investigations of the spectral content of the impact flash have been performed ( 13 , 15 , 17–19 ) at high impact velocities (5–7 km ). At impact velocities in excess of 10–15 km s projectiles may be shock vaporized entirely, and the radiation dynamics and expansion of the vapor and plasma dominate the impact flash ( 20 , 21 ). The study of orbital and planetary impacts being a common motivation for such work, laboratory hypervelocity experiments often utilize low-density and lower strength materials to more closely resemble the dynamics of real-life impacts despite the velocity limitations of launch systems.…”
Section: Introductionmentioning
confidence: 99%