Advances in Hybrid Rocket Technology and Related Analysis Methodologies
The book is an amazing collection of technical papers dealing with hybrid rockets. Once perceived as a niche technology, for about a decade, hybrid rockets have enjoyed renewed interest from both the propulsion technical community and industry. Hybrid motors can be used in practically all applicatio...
Wedi'i Gadw mewn:
| Fformat: | Online |
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| Iaith: | Saesneg |
| Cyhoeddwyd: |
MDPI - Multidisciplinary Digital Publishing Institute
2021
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| Pynciau: | |
| Mynediad Ar-lein: | ONIX_20210501_9783039433902_1133 |
| Tagiau: |
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!
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| _version_ | 1869517792381763584 |
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| collection | Directory of Open Access Books |
| description | The book is an amazing collection of technical papers dealing with hybrid rockets. Once perceived as a niche technology, for about a decade, hybrid rockets have enjoyed renewed interest from both the propulsion technical community and industry. Hybrid motors can be used in practically all applications where a rocket is employed, but there are certain cases where they present a superior fit, such as sounding rockets, tactical missile systems, launch boosters and the emerging field of commercial space transportation. The novel space tourism business, indeed, will benefit from their safety and lower recurrent development costs. The subjects addressed in the book include the cutting edge technology employed to push forward this relatively new propulsion concept, spanning systems to improve fuel regression rate, control of the mixture ratio to optimize performance, computational fluid dynamics applied to the simulation of the internal ballistics, and some other novel system applications. |
| format | Online |
| id | doab-20.500.12854ir-69387 |
| institution | Directory of Open Access Books |
| language | eng |
| publishDate | 2021 |
| publishDateRange | 2021 |
| publishDateSort | 2021 |
| publisher | MDPI - Multidisciplinary Digital Publishing Institute |
| publisherStr | MDPI - Multidisciplinary Digital Publishing Institute |
| record_format | ojs |
| spelling | doab-20.500.12854ir-693872024-04-11T15:11:31Z Advances in Hybrid Rocket Technology and Related Analysis Methodologies Carmicino, Carmine hybrid rocket marine propulsion rupture disc idling operation underwater environment hybrid rocket engines multidisciplinary design optimization robust optimization electric feed system ballistic reconstruction technique fuel regression nozzle erosion c∗ efficiency hybrid regression rate self-disintegration HTPB paraffin low-energy polymer magnesium fuel regression rate internal ballistics computational fluid dynamics hybrid rocket propulsion swirl oxidizer injection feedback loop control error propagation analysis resistor-based sensors rocket regression Marxman diffusion-limited blowing factor 3D printing fuel grain hybrid combustion modeling and simulation hybrid propulsion paraffin-based fuel oxygen combustion testing nano-sized aluminum micron-sized aluminum fluoropolymer mechanically activated aluminum coated aluminum fuel-rich composite powder aluminum aggregation aluminum agglomeration mass burning rate n/a “green” propellants nitrous oxide decomposition energy of activation 3-D printing hybrid rocket engine sounding rocket carbon fiber composite engine test total impulse lightweight design ignition system gas torch methane-oxygen combustion vortex combustion chamber hybrid rocket motor ramjet motor thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology The book is an amazing collection of technical papers dealing with hybrid rockets. Once perceived as a niche technology, for about a decade, hybrid rockets have enjoyed renewed interest from both the propulsion technical community and industry. Hybrid motors can be used in practically all applications where a rocket is employed, but there are certain cases where they present a superior fit, such as sounding rockets, tactical missile systems, launch boosters and the emerging field of commercial space transportation. The novel space tourism business, indeed, will benefit from their safety and lower recurrent development costs. The subjects addressed in the book include the cutting edge technology employed to push forward this relatively new propulsion concept, spanning systems to improve fuel regression rate, control of the mixture ratio to optimize performance, computational fluid dynamics applied to the simulation of the internal ballistics, and some other novel system applications. 2021-05-01T15:48:27Z 2021-05-01T15:48:27Z 2020 book ONIX_20210501_9783039433902_1133 9783039433902 9783039433919 https://directory.doabooks.org/handle/20.500.12854/69387 eng application/octet-stream Attribution 4.0 International https://mdpi.com/books/pdfview/book/3180 https://mdpi.com/books/pdfview/book/3180 MDPI - Multidisciplinary Digital Publishing Institute 10.3390/books978-3-03943-391-9 10.3390/books978-3-03943-391-9 46cabcaa-dd94-4bfe-87b4-55023c1b36d0 9783039433902 9783039433919 352 Basel, Switzerland open access |
| spellingShingle | hybrid rocket marine propulsion rupture disc idling operation underwater environment hybrid rocket engines multidisciplinary design optimization robust optimization electric feed system ballistic reconstruction technique fuel regression nozzle erosion c∗ efficiency hybrid regression rate self-disintegration HTPB paraffin low-energy polymer magnesium fuel regression rate internal ballistics computational fluid dynamics hybrid rocket propulsion swirl oxidizer injection feedback loop control error propagation analysis resistor-based sensors rocket regression Marxman diffusion-limited blowing factor 3D printing fuel grain hybrid combustion modeling and simulation hybrid propulsion paraffin-based fuel oxygen combustion testing nano-sized aluminum micron-sized aluminum fluoropolymer mechanically activated aluminum coated aluminum fuel-rich composite powder aluminum aggregation aluminum agglomeration mass burning rate n/a “green” propellants nitrous oxide decomposition energy of activation 3-D printing hybrid rocket engine sounding rocket carbon fiber composite engine test total impulse lightweight design ignition system gas torch methane-oxygen combustion vortex combustion chamber hybrid rocket motor ramjet motor thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title | Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title_full | Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title_fullStr | Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title_full_unstemmed | Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title_short | Advances in Hybrid Rocket Technology and Related Analysis Methodologies |
| title_sort | advances in hybrid rocket technology and related analysis methodologies |
| topic | hybrid rocket marine propulsion rupture disc idling operation underwater environment hybrid rocket engines multidisciplinary design optimization robust optimization electric feed system ballistic reconstruction technique fuel regression nozzle erosion c∗ efficiency hybrid regression rate self-disintegration HTPB paraffin low-energy polymer magnesium fuel regression rate internal ballistics computational fluid dynamics hybrid rocket propulsion swirl oxidizer injection feedback loop control error propagation analysis resistor-based sensors rocket regression Marxman diffusion-limited blowing factor 3D printing fuel grain hybrid combustion modeling and simulation hybrid propulsion paraffin-based fuel oxygen combustion testing nano-sized aluminum micron-sized aluminum fluoropolymer mechanically activated aluminum coated aluminum fuel-rich composite powder aluminum aggregation aluminum agglomeration mass burning rate n/a “green” propellants nitrous oxide decomposition energy of activation 3-D printing hybrid rocket engine sounding rocket carbon fiber composite engine test total impulse lightweight design ignition system gas torch methane-oxygen combustion vortex combustion chamber hybrid rocket motor ramjet motor thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology |
| topic_facet | hybrid rocket marine propulsion rupture disc idling operation underwater environment hybrid rocket engines multidisciplinary design optimization robust optimization electric feed system ballistic reconstruction technique fuel regression nozzle erosion c∗ efficiency hybrid regression rate self-disintegration HTPB paraffin low-energy polymer magnesium fuel regression rate internal ballistics computational fluid dynamics hybrid rocket propulsion swirl oxidizer injection feedback loop control error propagation analysis resistor-based sensors rocket regression Marxman diffusion-limited blowing factor 3D printing fuel grain hybrid combustion modeling and simulation hybrid propulsion paraffin-based fuel oxygen combustion testing nano-sized aluminum micron-sized aluminum fluoropolymer mechanically activated aluminum coated aluminum fuel-rich composite powder aluminum aggregation aluminum agglomeration mass burning rate n/a “green” propellants nitrous oxide decomposition energy of activation 3-D printing hybrid rocket engine sounding rocket carbon fiber composite engine test total impulse lightweight design ignition system gas torch methane-oxygen combustion vortex combustion chamber hybrid rocket motor ramjet motor thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology |
| url | ONIX_20210501_9783039433902_1133 |