Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Jeffrey A. Cerro"'
Autor:
Jennifer Mindock, Jeff Reilly, David Rubin, Michelle Urbina, Melinda Hailey, Jeffrey A. Cerro, Andrea Hanson, Kerry McGuire, Tyler Burba, Chris Middour, Michael Krihak, David Reyes
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Human exploration missions to beyond low Earth orbit destinations such as Mars will present significant new challenges to crew health management during a mission compared to current low Earth orbit operations. For the medical system, lack of consumab
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2beb260026eca06bf45c5d44399e255a
https://doi.org/10.2514/6.2017-5236
https://doi.org/10.2514/6.2017-5236
Autor:
Jeffrey A. Cerro, Kara Latorella, Matthew A. Simon, Judith Watson, Cindy Albertson, Vincent Le Boffe
Publikováno v:
AIAA SPACE 2015 Conference and Exposition.
Over the past three years NASA has been studying the operational effectiveness and astronaut protection efficacy of numerous radiation protection shelters for use in space exploration activities outside of earth's magnetosphere. The work presented wa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81708b5bdeaa36cceb4ac5d97c8b9ec6
https://doi.org/10.2514/6.2015-4402
https://doi.org/10.2514/6.2015-4402
Publikováno v:
AIAA SPACE 2013 Conference and Exposition.
In order to enable long-duration human exploration beyond low-Earth orbit, the risks associated with exposure of astronaut crews to space radiation must be mitigated with practical and affordable solutions. The space radiation environment beyond the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7116238dba59ce9752fc982fb705e826
https://doi.org/10.2514/6.2013-5435
https://doi.org/10.2514/6.2013-5435
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Non-optimum factors are used during aerospace conceptual and preliminary design to account for the increased weights of as-built structures due to future manufacturing and design details. Use of higher-fidelity non-optimum factors in these early stag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b0447b474fb92a170270d6b5791f2e5
https://doi.org/10.2514/6.2013-814
https://doi.org/10.2514/6.2013-814
Publikováno v:
Journal of Aircraft. 32:1382-1389
A combined loads test machine used to test aircraft primary structures such as fuselage and wing sections is described. The design features of a D-box test fixture that provides a simple test setup with the flexibility to accommodate curved stiffened
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e07103fea06216ce0c55dc54497c959d
https://doi.org/10.2514/3.46889
https://doi.org/10.2514/3.46889
Autor:
Cécile M. Burg, Lawrence L. Green, Jeffrey A. Cerro, Clyde R. Gumbert, Natalia Alexandrov, Sherilyn A. Brown, Michael R. Sorokach
Publikováno v:
11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
This paper is one of a set of papers, developed simultaneously and presented within a single conference session, that are intended to highlight systems analysis and design capabilities within the Systems Analysis and Concepts Directorate (SACD) of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2ab420231162cd4d4953e68ed30a27c
https://doi.org/10.2514/6.2006-7028
https://doi.org/10.2514/6.2006-7028
Autor:
R. Frank Vause, Charles L. Blackburn, Jonathan C. Stevenst, Jeffrey A. Cerro, David E. Glass, Lockheed Martin
Publikováno v:
8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
A cryogenic pressure box (cryobox) was designed and fabricated for use at NASA Langley Research Center (LaRC) to subject 76 in. x 65 in. curved panels to elevated and cryogenic temperatures and biaxial tensile mechanical loads. The cryobox is capable
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b73f68d9a9de39b70f4f0763cbdf1485
https://doi.org/10.2514/6.1998-1507
https://doi.org/10.2514/6.1998-1507
Publikováno v:
35th Structures, Structural Dynamics, and Materials Conference.
A combined loads test machine used to test aircraft primary structures such as fuselage and wing sections is described. The design features of a D-box test fixture that provides a simple test setup with the flexibility to accommodate curved stiffened
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5ba4aa111f0908e99f46e3a516d4df7
https://doi.org/10.2514/6.1994-1345
https://doi.org/10.2514/6.1994-1345
Publikováno v:
Aircraft Design and Operations Meeting.
A conceptual/preliminary level structural design system has been developed for structural integrity analysis and weight estimation of advanced space transportation vehicles. The system includes a three-dimensional interactive geometry modeler, a fini
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6826db08b0d34ce575a895aa20b8ccd3
https://doi.org/10.2514/6.1989-2130
https://doi.org/10.2514/6.1989-2130
Periodical
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.