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Keywords: SPACE DEBRIS
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Proceedings Papers

Assessment and Validation of Collision “Consequence” Method of Assessing Orbital Regime Risk Posed by Potential Satellite Conjunctions

Travis F. Lechtenberg, Matthew D. Hejduk
Proc. ASME. HVIS2019, 2019 15th Hypervelocity Impact Symposium, V001T05A006, April 14–19, 2019
Publisher: American Society of Mechanical Engineers
Paper No: HVIS2019-061
https://doi.org/10.1115/HVIS2019-061
... the possible consequences of a prospective collision. COLLISIONS RISK ASSESSMENT PROBABILITY THEORY SPACE DEBRIS SATELLITE ORBITS ATMOSPHERIC DENSITY DRAG COEFFICIENTS RISK MANAGEMENT Proceedings of the 2019 Hypervelocity Impact Symposium HVIS2019 April 14-19, 2019, Destin, FL, USA HVIS2019-061...
View Paper titled, Assessment and Validation of Collision “Consequence” Method of Assessing Orbital Regime Risk Posed by Potential Satellite Conjunctions
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Topics: Collisions (Physics), Risk, Risk assessment, Risk management, Satellites
Proceedings Papers

Numerical study of dynamic behavior of foams subjected to high- to hyper-velocity impact

Xiaotian Zhang, Ruiqing Wang, Q.M. Li
Proc. ASME. HVIS2019, 2019 15th Hypervelocity Impact Symposium, V001T10A013, April 14–19, 2019
Publisher: American Society of Mechanical Engineers
Paper No: HVIS2019-071
https://doi.org/10.1115/HVIS2019-071
... E-mail address : zhangxiaotian@buaa.edu.cn . Abstract Hypervelocity tests and numerical studies have been reported in the literature for aluminum foam to show its potential applications in spacecraft shielding against space debris based on “shielding set-up”. Meanwhile the “forward...
View Paper titled, Numerical study of dynamic behavior of foams subjected to high- to hyper-velocity impact
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Topics: Aluminum, Computer simulation, Deformation, Erosion, Failure, Failure mechanisms, Foamed materials, Foams (Chemistry), Hydrodynamics, Particulate matter
Proceedings Papers

A rupture limit equation for COPVs following a perforating MMOD impact

William P. Schonberg
Proc. ASME. HVIS2019, 2019 15th Hypervelocity Impact Symposium, V001T10A003, April 14–19, 2019
Publisher: American Society of Mechanical Engineers
Paper No: HVIS2019-026
https://doi.org/10.1115/HVIS2019-026
.... space debris COPV MMOD tank rupture hypervelocity impact composite material pressure vessel Proceedings of the 2019 Hypervelocity Impact Symposium HVIS2019 April 14-19, 2019, Destin, FL, USA HVIS2019-026 501 A rupture limit equation for COPVs following a perforating MMOD impact William P...
View Paper titled, A rupture limit equation for COPVs following a perforating MMOD impact
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Topics: Composite materials, Pressure vessels, Rupture
Proceedings Papers

Investigation on Sustained Discharge of Satellite’s Power Harness Due to Plasma from Space Debris Impact

Yuki Mando, Koji Tanaka, Takayuki Hirai, Shirou Kawakita, Masumi Higashide, Hirohisa Kurosaki, Sunao Hasegawa, Kumi Nitta
Proc. ASME. HVIS2019, 2019 15th Hypervelocity Impact Symposium, V001T10A002, April 14–19, 2019
Publisher: American Society of Mechanical Engineers
Paper No: HVIS2019-019
https://doi.org/10.1115/HVIS2019-019
... E-mail address : mando.yuki@ac.jaxa.jp Abstract Space debris travels at a velocity of 7-8 km/s in low Earth orbit (LEO) and at 3 km/s in geostationary Earth orbit (GEO). An impact between space debris and spacecraft will result in tremendous damage. In particular, particles less than...
View Paper titled, Investigation on Sustained Discharge of Satellite’s Power Harness Due to Plasma from <span class="search-highlight">Space</span> <span class="search-highlight">Debris</span> Impact
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Topics: Plasmas (Ionized gases), Circuits, Particulate matter, Risk, Aluminum, Damage, Power systems (Machinery), Projectiles, Satellites, Solar cell arrays