session 3

Title: Impact-Induced Mission Effects and Risk Assessments
type: oral
Description: This session addresses disruptions of spacecraft operations induced by hypervelocity impacts including spacecraft anomalies, perturbation of operations, and component failures up to mission loss. It includes risk assessments for impact vulnerability studies and corresponding system tools. Further topics are spacecraft impact protection and shielding studies, laboratory impact experiments, numerical simulations, and on-board diagnostics to characterize impacts such as impact sensors, accelerometers, etc.
Date: 2018-10-03
Time: 09:45
Room: ZARM 1

IPC members

Co-Chair: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;
Co-Chair: Dr. Norman Fitz-Coy, University of Florida, United States;
Rapporteur: Dr. Darren McKnight, LeoLabs, United States;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	experimental study on performances for the different graded-impedance distribution materials	18	confirmed	Dr. Guangming Song	China Academy of Space Technology (CAST)	China
2	Characteristics of Microwave Emissions from Hypervelocity Impacts on Pure Aluminum and Various Aluminum Alloy Plates	18	confirmed	Mr. Yuki Mando	The Graduate University for Advanced Studies	Japan
3	Orbital Debris Risk Assessment of Harnessing: Comparing Aluminum Plate Ballistic Limit Equation Predictions to Test Data	18	confirmed	Mr. James Chinn	Jet Propulsion Laboratory - California Institute of Technology	United States
4	Characterizing DebriSat Fragments -- Preliminary Results	18	confirmed	Ms. Samantha Allen	University of Florida	United States
5	Measuring impact craters on the ISS Columbus Module	18	confirmed	Mr. Robin Putzar	Fraunhofer EMI	Germany
6	Research on the Analysis Method of Failure Probability Caused by the Impact of Space Debris	18	confirmed	Dr. Sen Liu	China Aerodynamics Research and Development Center (CARDC)	China
7	Experimental characterization of multi-layer 3D-printed shields for microsatellites	18	confirmed	Dr. Lorenzo Olivieri	CISAS "G. Colombo" - University of Padova	Italy
8	Cross-validation of the Meteoroid and Orbital Debris Risk and Damage Assessment Tools ESABASE2/Debris and BUMPER	18	confirmed	Mr. Anatoli Miller	Etamax Space GmbH	Germany
9	CST: a new semi-empirical tool for simulating spacecraft collisions in orbit	18	confirmed	Prof. Alessandro Francesconi	University of Padova - DII/CISAS	Italy
10	Modeling of the impact micrometeoroid and orbital debris on the Micrometeoroids and Debris Protection System for inflatable modules for lunar orbital application	18	confirmed	Dr. Natalia Goldenko	TSNIIMASH	Russian Federation
–	Enhanced Orbital Debris Shielding Structure With Impedance-Graded Materials		confirmed	Prof. Zizheng Gong	Beijing Institute of Spacecraft Environment Engineering, China Academy of Space Technology (CAST)	China
–	How to Effectively Map Space Debris Impact Crater Distribution and Morphology on Spacecraft Hulls			Dr. Max Gulde	Fraunhofer EMI	Germany
–	Performance Characteristics of DebriSat Imaging Systems			Mr. Bungo Shiotani	University of Florida	United States

session 3

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