High-Performance Computer Modeling of the Cosmos-Iridium Collision
Abstract
This paper describes the application of a new, integrated modeling and simulation framework, encompassing the space situational awareness (SSA) enterprise, to the recent Cosmos-Iridium collision. This framework is based on a flexible, scalable architecture to enable efficient simulation of the current SSA enterprise, and to accommodate future advancements in SSA systems. In particular, the code is designed to take advantage of massively parallel, high-performance computer systems available, for example, at Lawrence Livermore National Laboratory. We will describe the application of this framework to the recent collision of the Cosmos and Iridium satellites, including (1) detailed hydrodynamic modeling of the satellite collision and resulting debris generation, (2) orbital propagation of the simulated debris and analysis of the increased risk to other satellites (3) calculation of the radar and optical signatures of the simulated debris and modeling of debris detection with space surveillance radar and optical systems (4) determination of simulated debris orbits from modeled space surveillance observations and analysis of the resulting orbital accuracy, (5) comparison of these modeling and simulation results with Space Surveillance Network observations. We will also discuss the use of this integrated modeling and simulation framework to analyze the risks and consequences of future satellite collisions andmore »
- Authors:
- Publication Date:
- Research Org.:
- Lawrence Livermore National Lab. (LLNL), Livermore, CA (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 965464
- Report Number(s):
- LLNL-CONF-416345
TRN: US200919%%586
- DOE Contract Number:
- W-7405-ENG-48
- Resource Type:
- Conference
- Resource Relation:
- Conference: Presented at: Advanced Maui Optical and Space Surveillance Conference, Wailea, HI, United States, Sep 01 - Sep 04, 2009
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 71 CLASSICAL AND QUANTUMM MECHANICS, GENERAL PHYSICS; 42 ENGINEERING; 99 GENERAL AND MISCELLANEOUS; ACCURACY; ARCHITECTURE; COMPUTERS; DETECTION; HYDRODYNAMICS; IRIDIUM; LAWRENCE LIVERMORE NATIONAL LABORATORY; OPTICAL SYSTEMS; RADAR; SATELLITES; SIMULATION; UNIVERSE
Citation Formats
Olivier, S, Cook, K, Fasenfest, B, Jefferson, D, Jiang, M, Leek, J, Levatin, J, Nikolaev, S, Pertica, A, Phillion, D, Springer, K, and De Vries, W. High-Performance Computer Modeling of the Cosmos-Iridium Collision. United States: N. p., 2009.
Web.
Olivier, S, Cook, K, Fasenfest, B, Jefferson, D, Jiang, M, Leek, J, Levatin, J, Nikolaev, S, Pertica, A, Phillion, D, Springer, K, & De Vries, W. High-Performance Computer Modeling of the Cosmos-Iridium Collision. United States.
Olivier, S, Cook, K, Fasenfest, B, Jefferson, D, Jiang, M, Leek, J, Levatin, J, Nikolaev, S, Pertica, A, Phillion, D, Springer, K, and De Vries, W. 2009.
"High-Performance Computer Modeling of the Cosmos-Iridium Collision". United States. https://www.osti.gov/servlets/purl/965464.
@article{osti_965464,
title = {High-Performance Computer Modeling of the Cosmos-Iridium Collision},
author = {Olivier, S and Cook, K and Fasenfest, B and Jefferson, D and Jiang, M and Leek, J and Levatin, J and Nikolaev, S and Pertica, A and Phillion, D and Springer, K and De Vries, W},
abstractNote = {This paper describes the application of a new, integrated modeling and simulation framework, encompassing the space situational awareness (SSA) enterprise, to the recent Cosmos-Iridium collision. This framework is based on a flexible, scalable architecture to enable efficient simulation of the current SSA enterprise, and to accommodate future advancements in SSA systems. In particular, the code is designed to take advantage of massively parallel, high-performance computer systems available, for example, at Lawrence Livermore National Laboratory. We will describe the application of this framework to the recent collision of the Cosmos and Iridium satellites, including (1) detailed hydrodynamic modeling of the satellite collision and resulting debris generation, (2) orbital propagation of the simulated debris and analysis of the increased risk to other satellites (3) calculation of the radar and optical signatures of the simulated debris and modeling of debris detection with space surveillance radar and optical systems (4) determination of simulated debris orbits from modeled space surveillance observations and analysis of the resulting orbital accuracy, (5) comparison of these modeling and simulation results with Space Surveillance Network observations. We will also discuss the use of this integrated modeling and simulation framework to analyze the risks and consequences of future satellite collisions and to assess strategies for mitigating or avoiding future incidents, including the addition of new sensor systems, used in conjunction with the Space Surveillance Network, for improving space situational awareness.},
doi = {},
url = {https://www.osti.gov/biblio/965464},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Fri Aug 28 00:00:00 EDT 2009},
month = {Fri Aug 28 00:00:00 EDT 2009}
}