Chemical rockets: performance prediction and internal ballistics design
The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimiz...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Cham, Switzerland
Springer
[2020]
|
| Schriftenreihe: | Springer aerospace technology
|
| Schlagworte: | |
| Zusammenfassung: | The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance.While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones. Both are detailed in the book's second part for the prediction of ignition and tail-off transients, and equilibrium operation.Computer codes, adopting the incremental analysis along with erosive burning effect, are included. The material is encouraged to be used and presented at lectures. Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership |
| Beschreibung: | xi, 538 Seiten Diagramme 235 mm |
| ISBN: | 9783030269678 |
Internformat
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Datensatz im Suchindex
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| id | DE-604.BV046951432 |
| illustrated | Not Illustrated |
| index_date | 2024-07-03T15:41:17Z |
| indexdate | 2024-07-10T08:58:25Z |
| institution | BVB |
| isbn | 9783030269678 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-032359941 |
| oclc_num | 1227479011 |
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| physical | xi, 538 Seiten Diagramme 235 mm |
| publishDate | 2020 |
| publishDateSearch | 2020 |
| publishDateSort | 2020 |
| publisher | Springer |
| record_format | marc |
| series2 | Springer aerospace technology |
| spelling | Krishnan, Subramaniam Verfasser aut Chemical rockets performance prediction and internal ballistics design Subramaniam Krishnan, Jeenu Raghavan Cham, Switzerland Springer [2020] xi, 538 Seiten Diagramme 235 mm txt rdacontent n rdamedia nc rdacarrier Springer aerospace technology The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance.While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones. Both are detailed in the book's second part for the prediction of ignition and tail-off transients, and equilibrium operation.Computer codes, adopting the incremental analysis along with erosive burning effect, are included. The material is encouraged to be used and presented at lectures. Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership Aerospace engineering Astronautics Engineering design Thermodynamics Heat engineering Heat transfer Mass transfer Fluid mechanics Applied mathematics Engineering mathematics Engineering Hardcover, Softcover / Technik/Luftfahrttechnik, Raumfahrttechnik Raghavan, Jeenu Verfasser aut Erscheint auch als Online-Ausgabe 978-3-030-26965-4 |
| spellingShingle | Krishnan, Subramaniam Raghavan, Jeenu Chemical rockets performance prediction and internal ballistics design Aerospace engineering Astronautics Engineering design Thermodynamics Heat engineering Heat transfer Mass transfer Fluid mechanics Applied mathematics Engineering mathematics Engineering |
| title | Chemical rockets performance prediction and internal ballistics design |
| title_auth | Chemical rockets performance prediction and internal ballistics design |
| title_exact_search | Chemical rockets performance prediction and internal ballistics design |
| title_exact_search_txtP | Chemical rockets performance prediction and internal ballistics design |
| title_full | Chemical rockets performance prediction and internal ballistics design Subramaniam Krishnan, Jeenu Raghavan |
| title_fullStr | Chemical rockets performance prediction and internal ballistics design Subramaniam Krishnan, Jeenu Raghavan |
| title_full_unstemmed | Chemical rockets performance prediction and internal ballistics design Subramaniam Krishnan, Jeenu Raghavan |
| title_short | Chemical rockets |
| title_sort | chemical rockets performance prediction and internal ballistics design |
| title_sub | performance prediction and internal ballistics design |
| topic | Aerospace engineering Astronautics Engineering design Thermodynamics Heat engineering Heat transfer Mass transfer Fluid mechanics Applied mathematics Engineering mathematics Engineering |
| topic_facet | Aerospace engineering Astronautics Engineering design Thermodynamics Heat engineering Heat transfer Mass transfer Fluid mechanics Applied mathematics Engineering mathematics Engineering |
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