Combustion instabilities in liquid rocket engines: testing and development practices in Russia
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Reston, Va.
American Institute of Aeronautics and Astronautics
c2007
|
| Schriftenreihe: | Progress in astronautics and aeronautics
|
| Schlagworte: | |
| Beschreibung: | Includes bibliographical references and index |
| Beschreibung: | xix, 321 p. |
| ISBN: | 1563479214 9781563479212 9781600864711 |
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| 100 | 1 | |a Dranovsky, Mark L. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Combustion instabilities in liquid rocket engines |b testing and development practices in Russia |c Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| 264 | 1 | |a Reston, Va. |b American Institute of Aeronautics and Astronautics |c c2007 | |
| 300 | |a xix, 321 p. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b c |2 rdamedia | ||
| 338 | |b cr |2 rdacarrier | ||
| 490 | 0 | |a Progress in astronautics and aeronautics | |
| 500 | |a Includes bibliographical references and index | ||
| 505 | 0 | |a Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine | |
| 650 | 4 | |a Liquid propellant rockets | |
| 650 | 4 | |a Rocket engines |x Combustion |z Russia (Federation) |x Testing | |
| 650 | 4 | |a Liquid fuels |x Combustion |z Russia (Federation) |x Testing | |
| 650 | 4 | |a Rockets (Aeronautics) |z Russia (Federation) |x Testing | |
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| 689 | 0 | 2 | |a Entwurf |0 (DE-588)4121208-3 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Yang, Vigor |e Sonstige |4 oth | |
| 700 | 1 | |a Culick, F. |d 1933- |e Sonstige |4 oth | |
| 700 | 1 | |a Talley, Douglas G. |e Sonstige |4 oth | |
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Datensatz im Suchindex
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| any_adam_object | |
| author | Dranovsky, Mark L. |
| author_facet | Dranovsky, Mark L. |
| author_role | aut |
| author_sort | Dranovsky, Mark L. |
| author_variant | m l d ml mld |
| building | Verbundindex |
| bvnumber | BV044094878 |
| collection | ZDB-30-PAD |
| contents | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine |
| ctrlnum | (ZDB-30-PAD)EBC3111571 (ZDB-89-EBL)EBL3111571 (OCoLC)774285720 (DE-599)BVBBV044094878 |
| dewey-full | 621.43/56 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 621 - Applied physics |
| dewey-raw | 621.43/56 |
| dewey-search | 621.43/56 |
| dewey-sort | 3621.43 256 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen |
| format | Electronic eBook |
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| id | DE-604.BV044094878 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T07:43:31Z |
| institution | BVB |
| isbn | 1563479214 9781563479212 9781600864711 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029501723 |
| oclc_num | 774285720 |
| open_access_boolean | |
| physical | xix, 321 p. |
| psigel | ZDB-30-PAD |
| publishDate | 2007 |
| publishDateSearch | 2007 |
| publishDateSort | 2007 |
| publisher | American Institute of Aeronautics and Astronautics |
| record_format | marc |
| series2 | Progress in astronautics and aeronautics |
| spelling | Dranovsky, Mark L. Verfasser aut Combustion instabilities in liquid rocket engines testing and development practices in Russia Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley Reston, Va. American Institute of Aeronautics and Astronautics c2007 xix, 321 p. txt rdacontent c rdamedia cr rdacarrier Progress in astronautics and aeronautics Includes bibliographical references and index Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine Liquid propellant rockets Rocket engines Combustion Russia (Federation) Testing Liquid fuels Combustion Russia (Federation) Testing Rockets (Aeronautics) Russia (Federation) Testing Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd rswk-swf Entwurf (DE-588)4121208-3 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 s Flüssigkeitsraketentriebwerk (DE-588)4448628-5 s Entwurf (DE-588)4121208-3 s DE-604 Yang, Vigor Sonstige oth Culick, F. 1933- Sonstige oth Talley, Douglas G. Sonstige oth |
| spellingShingle | Dranovsky, Mark L. Combustion instabilities in liquid rocket engines testing and development practices in Russia Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine Liquid propellant rockets Rocket engines Combustion Russia (Federation) Testing Liquid fuels Combustion Russia (Federation) Testing Rockets (Aeronautics) Russia (Federation) Testing Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd Entwurf (DE-588)4121208-3 gnd Raketentriebwerk (DE-588)4176905-3 gnd |
| subject_GND | (DE-588)4448628-5 (DE-588)4121208-3 (DE-588)4176905-3 |
| title | Combustion instabilities in liquid rocket engines testing and development practices in Russia |
| title_auth | Combustion instabilities in liquid rocket engines testing and development practices in Russia |
| title_exact_search | Combustion instabilities in liquid rocket engines testing and development practices in Russia |
| title_full | Combustion instabilities in liquid rocket engines testing and development practices in Russia Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| title_fullStr | Combustion instabilities in liquid rocket engines testing and development practices in Russia Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| title_full_unstemmed | Combustion instabilities in liquid rocket engines testing and development practices in Russia Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| title_short | Combustion instabilities in liquid rocket engines |
| title_sort | combustion instabilities in liquid rocket engines testing and development practices in russia |
| title_sub | testing and development practices in Russia |
| topic | Liquid propellant rockets Rocket engines Combustion Russia (Federation) Testing Liquid fuels Combustion Russia (Federation) Testing Rockets (Aeronautics) Russia (Federation) Testing Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd Entwurf (DE-588)4121208-3 gnd Raketentriebwerk (DE-588)4176905-3 gnd |
| topic_facet | Liquid propellant rockets Rocket engines Combustion Russia (Federation) Testing Liquid fuels Combustion Russia (Federation) Testing Rockets (Aeronautics) Russia (Federation) Testing Flüssigkeitsraketentriebwerk Entwurf Raketentriebwerk |
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