Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Alexandre Mangeot"'
Autor:
Paul C. Sokoloff, Anushree Srivastava, R. Troy McMullin, Jonathan Clarke, Paul Knightly, Anastasia Stepanova, Alexandre Mangeot, Claude-Michel Laroche, Annalea Beattie, Shannon Rupert
Publikováno v:
Check List, Vol 20, Iss 5, Pp 1096-1126 (2024)
During the Mars 160 Mission in 2016 and 2017, crews at the Mars Desert Research Station (MDRS) in Utah, USA and the Flashline Mars Arctic Research Station (FMARS) on Tallurutit (Devon Island), Nunavut, Canada, conducted a collections‑based survey o
Externí odkaz:
https://doaj.org/article/43e0295eed2b4dfb8c04b52586fa88ce
Publikováno v:
Acta Astronautica
Acta Astronautica, Elsevier, 2018, 148, pp.89-98. ⟨10.1016/j.actaastro.2018.04.046⟩
Acta Astronautica, Elsevier, 2018, 148, pp.89-98. ⟨10.1016/j.actaastro.2018.04.046⟩
A numerical model was developed with CFD-ACE software to study the working condition of an oxygen-nitrogen/polyethylene hybrid rocket combustor. As a first approach, a simplified numerical model is presented. It includes a compressible transient gas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a021873b012d849588b77694ff825ca1
https://hal.archives-ouvertes.fr/hal-02057869
https://hal.archives-ouvertes.fr/hal-02057869
Publikováno v:
Journal of Analytical and Applied Pyrolysis
Journal of Analytical and Applied Pyrolysis, Elsevier, 2011, doi: 10.1016/j.jaap.2011.11.006
Journal of Analytical and Applied Pyrolysis, Elsevier, 2011, doi: 10.1016/j.jaap.2011.11.006
International audience; Hybrid rocket propulsion presents an increasing demand because of safety and cost reasons. Numerous works cover the main related areas (regression rate, oxidiser injection, grain design and additives in solid reducer). Neverth
Publikováno v:
Journal of Analytical and Applied Pyrolysis
Journal of Analytical and Applied Pyrolysis, Elsevier, 2013, pp.1-11. ⟨10.1016/j.jaap.2013.02.014⟩
Journal of Analytical and Applied Pyrolysis, Elsevier, 2013, pp.1-11. ⟨10.1016/j.jaap.2013.02.014⟩
International audience; The inert and oxidative flash pyrolysis of High Density Poly-Ethylene (HDPE) is studied up to 20 000 K.s-1, under pressure up to 3.0 MPa and at temperature ranging from 1000 K to 1500 K. These conditions are considered to repr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1cc80562afc7f46c603520671b51e28b
https://hal.archives-ouvertes.fr/hal-00796085/file/Gascoin_HDPEPyflash_R2.pdf
https://hal.archives-ouvertes.fr/hal-00796085/file/Gascoin_HDPEPyflash_R2.pdf
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.4135, ⟨10.2514/6.2013-4135⟩
Scopus-Elsevier
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.4135, ⟨10.2514/6.2013-4135⟩
Scopus-Elsevier
The high density polyethylene, as hybrid rocket fuel, has been chosen to be studied. Thermogravimetric analysis allowed to determine an Arrhenius type equation for its regression rate. A flash pyrolysis coupled to GC/MS/FID has been used to observe i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a8dc66c52c090361359040400e76a717
https://hal.archives-ouvertes.fr/hal-00868665
https://hal.archives-ouvertes.fr/hal-00868665
Publikováno v:
Journal of Analytical and Applied Pyrolysis
Journal of Analytical and Applied Pyrolysis, Elsevier, 2011, 10.1016/j.jaap.2011.12.002
Journal of Analytical and Applied Pyrolysis, Elsevier, 2011, 10.1016/j.jaap.2011.12.002
The choice of a solid reducer for hybrid propulsion is generally based on the quantity of gaseous combustible it can produce (expressed indirectly by the regression rate). For this reason, the studies focus on the use of additives or on the design of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7cedead882f445a73c0aa67584ba1870
https://hal.archives-ouvertes.fr/hal-00649386/document
https://hal.archives-ouvertes.fr/hal-00649386/document
Autor:
Alexandre Mangeot, Camille Marin, Stéphane Rouvreau, Philippe Gillard, Nicolas Gascoin, Dominique Piton, Jacques Prevost
Publikováno v:
Scopus-Elsevier
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2013, ⟨10.2514/6.2013-4047⟩
Proc IMechE Part G: J Aerospace Engineering
Proc IMechE Part G: J Aerospace Engineering, 2013, pp.1-11. ⟨10.1177/0954410013480115⟩
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.4047, ⟨10.2514/6.2013-4047⟩
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2013, ⟨10.2514/6.2013-4047⟩
Proc IMechE Part G: J Aerospace Engineering
Proc IMechE Part G: J Aerospace Engineering, 2013, pp.1-11. ⟨10.1177/0954410013480115⟩
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.4047, ⟨10.2514/6.2013-4047⟩
International audience; 8 Hybrid combustors are of increasing interest for space and civilian propulsion. A test facility has been settled to 9 investigate the high density polyethylene combustion (propellant of 0.15 m long). A parametric study has b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ccee309d456ef845aca316b4f56b61e1
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883686770&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883686770&partnerID=MN8TOARS
Publikováno v:
Scopus-Elsevier
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.3965, ⟨10.2514/6.2013-3965⟩
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.3965, ⟨10.2514/6.2013-3965⟩
Hybrid rocket technology is known since the 30's and a large number of experimental, fundamental and applied research works covers it. It still suffers from a lack of chemical description and of detailed numerical simulation of core phenomena. Severa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a93f41cae045d4d18e71113f57ccd95
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883720573&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883720573&partnerID=MN8TOARS
Publikováno v:
Scopus-Elsevier
AIAA
20th AIAA Computational Fluid Dynamics Conference
20th AIAA Computational Fluid Dynamics Conference, Jun 2011, France. pp.3212
AIAA
20th AIAA Computational Fluid Dynamics Conference
20th AIAA Computational Fluid Dynamics Conference, Jun 2011, France. pp.3212
Hybrid rocket technology is known since the 30's and it is covered by a large number of experimental, fundamental and applied research works. It still suffers from a lack of chemical description and of detailed numerical simulation of core phenomena.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3ad8262ed74d661ef845eb8642c9fe09
http://www.scopus.com/inward/record.url?eid=2-s2.0-84861614553&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84861614553&partnerID=MN8TOARS
Publikováno v:
Scopus-Elsevier
Polymer Degradation and Stability
Polymer Degradation and Stability, Elsevier, 2012, pp.2012, 1-9. ⟨10.1016/j.polymdegradstab.2012.05.008⟩
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.3969, ⟨10.2514/6.2013-3969⟩
Polymer Degradation and Stability
Polymer Degradation and Stability, Elsevier, 2012, pp.2012, 1-9. ⟨10.1016/j.polymdegradstab.2012.05.008⟩
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, France. pp.3969, ⟨10.2514/6.2013-3969⟩
International audience; High Density Poly-Ethylene (HDPE) is one of the possible solid fuels to be used in hybrid rocket propulsion, despite its low ability of rapidly producing combustible gas. This drawback may be balanced by the auto-ignition dela
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e6cffb4c7fccb9b65d07180e88dbb342
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883680313&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883680313&partnerID=MN8TOARS