Zobrazeno 1 - 10
of 26
pro vyhledávání: '"Michel H. Lefebvre"'
Publikováno v:
Energies, Vol 14, Iss 6794, p 6794 (2021)
Energies, 14 (20
Energies; Volume 14; Issue 20; Pages: 6794
Energies, 14 (20
Energies; Volume 14; Issue 20; Pages: 6794
At Université Libre de Bruxelles (ULB), research was performed on a 1 kN lab-scale Hybrid Rocket Motor (the ULB-HRM). It has a single-port solid paraffin fuel grain and uses liquid N2 O as an oxidizer. The first Computational Fluid Dynamics (CFD) mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::71debc17a12ac30c7cef16c4d2aa6252
https://www.mdpi.com/1996-1073/14/20/6794
https://www.mdpi.com/1996-1073/14/20/6794
Publikováno v:
Journal of Energetic Materials. 38:1-19
Nitrocellulose (NC) and nitroglycerin (NG) are conventional energetic ingredients of solid double-base gun propellants. NC and NG are aliphatic nitrate ester compounds that are manufactured...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cb2497a2f2cbf19c037165614bc5f7d
https://doi.org/10.1080/07370652.2019.1657204
https://doi.org/10.1080/07370652.2019.1657204
Autor:
Michel H. Lefebvre, Patrick Hendrick, Mohammed Bouziane, Praskovia Milova, Artur Elias de Morais Bertoldi
Publikováno v:
Aerospace Science and Technology. 89:392-406
To investigate the effects of oxidizer injection on the performance of hybrid rocket motors (HRMs), we have designed, manufactured and tested four types of injector: showerhead (SH), hollow-cone (HC), pressure-swirl (PSW) and vortex (VOR). This study
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dde512129790c34b0004b3d5ae9c448d
https://doi.org/10.1016/j.ast.2019.04.009
https://doi.org/10.1016/j.ast.2019.04.009
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cccd4f33ebcaf6910f4f0edfd371dc1f
https://doi.org/10.2514/6.2021-3493
https://doi.org/10.2514/6.2021-3493
Publikováno v:
Materials Research and Applications ISBN: 9789811592225
The impregnation in surface with combustion moderator (also called deterrent) is usually applied to improve the ballistic properties, for example in the case of deterred spherical propellant which is largely employed in defense applications. The disa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78368be7334084169f0bedfa14e056ef
https://doi.org/10.1007/978-981-15-9223-2_3
https://doi.org/10.1007/978-981-15-9223-2_3
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f9f234c09249095a59c2fe79f2c6de7
https://doi.org/10.2514/6.2020-3763
https://doi.org/10.2514/6.2020-3763
Publikováno v:
Carbon
Carbon, Elsevier, 2020, 164, pp.129-132. ⟨10.1016/j.carbon.2020.03.061⟩
Carbon, Elsevier, 2020, 164, pp.129-132. ⟨10.1016/j.carbon.2020.03.061⟩
International audience; A novel energetic material based on nanoporous carbons as main ingredient is herein reported for thefirst time. Prepared byfilling the pores of nanoporous carbons with an oxidizer, its energetic character isdemonstrated. The d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6eadfdf5b53cc52d23c7add007495066
https://hal.archives-ouvertes.fr/hal-02612620
https://hal.archives-ouvertes.fr/hal-02612620
Publikováno v:
Central European Journal of Energetic Materials. 14:952-965
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a311fe0b73ed049ea33a4e9464b37a4
https://doi.org/10.22211/cejem/71213
https://doi.org/10.22211/cejem/71213
Publikováno v:
Central European Journal of Energetic Materials. 14:90-104
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e1f9c03cfddef6221864dcb58b905af
https://doi.org/10.22211/cejem/67538
https://doi.org/10.22211/cejem/67538
Publikováno v:
Innovative Energetic Materials: Properties, Combustion Performance and Application ISBN: 9789811548307
The objective of this study is to assess two different methods used to determine the burning rates of solid rocket propellants and to find a convenient correlation of the measured data. The well-known strand burner test (Crawford test) and the closed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0fc6ec3930988a7a6a161b4286d307f3
https://doi.org/10.1007/978-981-15-4831-4_12
https://doi.org/10.1007/978-981-15-4831-4_12