[HTML][HTML] On the need to assess and mitigate the risk from uncontrolled re-entries of artificial space objects in view of the current and future developments in space …
Abstract From 1 January 2010 to 24 August 2023, 566 orbital stages and 511 spacecraft with
a radar cross section> 1 m 2 have re-entered without control the Earth's atmosphere. The …
a radar cross section> 1 m 2 have re-entered without control the Earth's atmosphere. The …
A multifidelity framework for aerothermodynamic modeling and simulation of destructive atmospheric entry
F Morgado, S Abhishek Peddakotla, J Graham… - AIAA Journal, 2024 - arc.aiaa.org
The aerothermodynamic environment surrounding bodies undergoing destructive
atmospheric entry is characterized by multiple interacting shock waves generated by the …
atmospheric entry is characterized by multiple interacting shock waves generated by the …
A numerical approach to evaluate temperature-dependent peridynamics damage model for destructive atmospheric entry of spacecraft
The evaluation of the on-ground casualty risk assessments due to a controlled or
uncontrolled re-entry is highly sensitive to the accurate prediction of fragmentation events …
uncontrolled re-entry is highly sensitive to the accurate prediction of fragmentation events …
Plasma preheating technology for replicating planetary re-entry surface temperatures
DO Iyinomen - The Aeronautical Journal, 2022 - cambridge.org
Arc-jet facilities have been the norm for ablation experiments used to calibrate
computational models to date. However, the arc jet has a few major limitations and …
computational models to date. However, the arc jet has a few major limitations and …
Plasma Preheating Technology for Ablation Studies of Hypersonic Reentry Vehicles
DO Iyinomen - Hypersonic Vehicles-Applications, Recent …, 2022 - books.google.com
Measurements of mass ablation rates in hypersonic flows are used to calibrate
computational models. A novel plasma technique for preheating axisymmetric samples of …
computational models. A novel plasma technique for preheating axisymmetric samples of …
МОДЕЛЮВАННЯ ПРОЦЕСІВ АЕРОДИНАМІЧНОГО НАГРІВУ І ПЛАВЛЕННЯ КОСМІЧНИХ ОБ'ЄКТІВ В АТМОСФЕРІ ЗЕМЛІ
АЮ Дреус, ММ Дронь, ОІ Губін… - System design and …, 2022 - rocketsdesign.dp.ua
Наведено результати моделювання процесів термічного руйнування великогабаритних
об'єктів космічного сміття внаслідок аеродинамічного нагрівання й плавлення в верхніх …
об'єктів космічного сміття внаслідок аеродинамічного нагрівання й плавлення в верхніх …
Design for Minimum Casualty Area–The IXPE Case
C Ostrom, J Marichalar, B Greene… - … : Managing Risk in …, 2021 - ntrs.nasa.gov
The Imaging X-Ray Polarimetry Explorer (IXPE) is a new international space observatory in
NASA's Small Explorer program, designed in a collaboration between the Italian Space …
NASA's Small Explorer program, designed in a collaboration between the Italian Space …