Zobrazeno 1 - 8
of 8
pro vyhledávání: '"James L. Hyde"'
Publikováno v:
2019 15th Hypervelocity Impact Symposium.
Risk from micrometeoroid and orbital debris (MMOD) impacts on space vehicles is often quantified in terms of the probability of no penetration (PNP). However, for large spacecraft, especially those with multiple compartments, a penetration may have a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da601da2adf6870869337380c4d77ca3
https://doi.org/10.1115/hvis2019-018
https://doi.org/10.1115/hvis2019-018
Publikováno v:
2019 15th Hypervelocity Impact Symposium.
A well-known hazard associated with exposure to the space environment is the risk of vehicle failure due to an impact from a micrometeoroid and orbital debris (MMOD) particle. Among the vehicles of importance to NASA is the extravehicular mobility un
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13499b3c5f1cbeb8bb1e60db9ff23fb9
https://doi.org/10.1115/hvis2019-058
https://doi.org/10.1115/hvis2019-058
Autor:
James L. Hyde, M. A. Garcia, E. L. Berger, O. M. Oliveras, P. A. Enriquez, B.A. Davis, K.D. Deighton, Eric L. Christiansen, J.E. Miller, W.E. Bohl
Publikováno v:
Procedia Engineering. 204:460-467
The principal mechanism for developing orbital debris environment models, is to make observations of larger pieces of debris in the range of several centimeters and greater using radar and optical techniques. For particles that are smaller than this
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17e471b3d32bdf214b27c8d84678a900
https://doi.org/10.1016/j.proeng.2017.09.741
https://doi.org/10.1016/j.proeng.2017.09.741
Publikováno v:
Procedia Engineering. 103:246-253
The Shuttle Hypervelocity Impact Database documents damage features on each Orbiter from micrometeoroids (MM) and orbital debris (OD). Data is divided into tables for crew module windows, payload bay door radiators and thermal protection systems alon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::934c782896fdee6f177fd2ccf849b34b
Publikováno v:
International Journal of Impact Engineering. 17:57-68
When Orbiter Vehicles (OV) are placed in low-Earth orbit (LEO) the exposed surface is subjected to hypervelocity collision with small particles of meteoroids and man-made orbital debris (M&OD). The external shell of the orbiter is specifically design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::552339a03d53f577fd48c7c9498b7bb4
https://doi.org/10.1016/0734-743x(95)99835-f
https://doi.org/10.1016/0734-743x(95)99835-f
Publikováno v:
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper documents the data collected from two hypervelocity micro-meteoroid & orbital debris (MMOD) impact events where the shuttle payload bay door radiator sandwich panel was completely perforated; i.e., the MMOD impact created a hole in both th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1859752ef2a960f7b62d68510cb69be
https://doi.org/10.2514/6.2009-2361
https://doi.org/10.2514/6.2009-2361
Publikováno v:
57th International Astronautical Congress.
Discussion includes recent enhancements to the BUMPER-II program and input files in support of Shuttle Return to Flight. Improvements to the mesh definitions of the finite element input model will be presented. A BUMPER-II analysis process that was u
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46c7841ae141990535cae2b2f5cae4c5
https://doi.org/10.2514/6.iac-06-b6.3.03
https://doi.org/10.2514/6.iac-06-b6.3.03
Publikováno v:
PROTECTION OF MATERIALS AND STRUCTURES FROM THE SPACE ENVIRONMENT ISBN: 9781402042812
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::606153c2caa7dc861255435a6cb85af9
https://doi.org/10.1007/1-4020-4319-8_17
https://doi.org/10.1007/1-4020-4319-8_17
