Combustion instabilities in liquid rocket engines: testing and development practices in Russia
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | , , |
| Format: | Electronic eBook |
| Language: | English |
| Published: |
Reston, Va.
American Institute of Aeronautics and Astronautics
[2007]
|
| Series: | Progress in astronautics and aeronautics
221 |
| Subjects: | |
| Online Access: | UBY01 Volltext |
| Physical Description: | 1 Online-Ressource (xix, 321 Seiten) |
| ISBN: | 9781600866906 9781600864711 |
Staff View
MARC
| LEADER | 00000nmm a2200000zcb4500 | ||
|---|---|---|---|
| 001 | BV044846929 | ||
| 003 | DE-604 | ||
| 005 | 20210728 | ||
| 007 | cr|uuu---uuuuu | ||
| 008 | 180305s2007 |||| o||u| ||||||eng d | ||
| 020 | |a 9781600866906 |9 978-1-60086-690-6 | ||
| 020 | |a 9781600864711 |c Online |9 978-1-60086-471-1 | ||
| 024 | 7 | |a 10.2514/4.866906 |2 doi | |
| 035 | |a (ZDB-38-ESG)ebr10516675 | ||
| 035 | |a (ZDB-283-AERC)978-1-60086-690-6 | ||
| 035 | |a (OCoLC)774285720 | ||
| 035 | |a (DE-599)BVBBV044846929 | ||
| 040 | |a DE-604 |b ger |e aacr | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-83 |a DE-706 | ||
| 082 | 0 | |a 621.43/56 |2 23 | |
| 100 | 1 | |a Dranovskij, Mark Lʹvovič |e Verfasser |0 (DE-588)1067777962 |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 [2007] | |
| 264 | 4 | |c © 2007 | |
| 300 | |a 1 Online-Ressource (xix, 321 Seiten) | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b c |2 rdamedia | ||
| 338 | |b cr |2 rdacarrier | ||
| 490 | 1 | |a Progress in astronautics and aeronautics |v volume 221 | |
| 505 | 8 | |a Includes bibliographical references and index | |
| 505 | 8 | |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 | |
| 650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Flüssigkeitsraketentriebwerk |0 (DE-588)4448628-5 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Entwurf |0 (DE-588)4121208-3 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 0 | 1 | |a Flüssigkeitsraketentriebwerk |0 (DE-588)4448628-5 |D s |
| 689 | 0 | 2 | |a Entwurf |0 (DE-588)4121208-3 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Yang, Vigor |4 edt | |
| 700 | 1 | |a Culick, Fred E.C. |d 1933- |0 (DE-588)1089461704 |4 edt | |
| 700 | 1 | |a Talley, Douglas G. |4 edt | |
| 776 | 0 | 8 | |i Erscheint auch als |n Druck-Ausgabe |z 978-1-56347-921-2 |
| 776 | 0 | 8 | |i Erscheint auch als |n Druck-Ausgabe |z 1-56347-921-4 |
| 830 | 0 | |a Progress in astronautics and aeronautics |v 221 |w (DE-604)BV045507833 |9 221 | |
| 856 | 4 | 0 | |u http://www.doi.org/10.2514/4.866906 |x Verlag |z URL des Erstveröffentlichers |3 Volltext |
| 912 | |a ZDB-283-AERC |a ZDB-38-ESG |a ZDB-283-APAA | ||
| 999 | |a oai:aleph.bib-bvb.de:BVB01-030241790 | ||
| 966 | e | |u http://www.doi.org/10.2514/4.866906 |l UBY01 |p ZDB-283-AERC |x Verlag |3 Volltext | |
Record in the Search Index
| _version_ | 1804178359909875712 |
|---|---|
| any_adam_object | |
| author | Dranovskij, Mark Lʹvovič |
| author2 | Yang, Vigor Culick, Fred E.C. 1933- Talley, Douglas G. |
| author2_role | edt edt edt |
| author2_variant | v y vy f e c fe fec d g t dg dgt |
| author_GND | (DE-588)1067777962 (DE-588)1089461704 |
| author_facet | Dranovskij, Mark Lʹvovič Yang, Vigor Culick, Fred E.C. 1933- Talley, Douglas G. |
| author_role | aut |
| author_sort | Dranovskij, Mark Lʹvovič |
| author_variant | m l d ml mld |
| building | Verbundindex |
| bvnumber | BV044846929 |
| collection | ZDB-283-AERC ZDB-38-ESG ZDB-283-APAA |
| contents | 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 |
| ctrlnum | (ZDB-38-ESG)ebr10516675 (ZDB-283-AERC)978-1-60086-690-6 (OCoLC)774285720 (DE-599)BVBBV044846929 |
| 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 |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>03682nmm a2200601zcb4500</leader><controlfield tag="001">BV044846929</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20210728 </controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">180305s2007 |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781600866906</subfield><subfield code="9">978-1-60086-690-6</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781600864711</subfield><subfield code="c">Online</subfield><subfield code="9">978-1-60086-471-1</subfield></datafield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.2514/4.866906</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(ZDB-38-ESG)ebr10516675</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(ZDB-283-AERC)978-1-60086-690-6</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)774285720</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV044846929</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">aacr</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-83</subfield><subfield code="a">DE-706</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">621.43/56</subfield><subfield code="2">23</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Dranovskij, Mark Lʹvovič</subfield><subfield code="e">Verfasser</subfield><subfield code="0">(DE-588)1067777962</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Combustion instabilities in liquid rocket engines</subfield><subfield code="b">testing and development practices in Russia</subfield><subfield code="c">Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Reston, Va.</subfield><subfield code="b">American Institute of Aeronautics and Astronautics</subfield><subfield code="c">[2007]</subfield></datafield><datafield tag="264" ind1=" " ind2="4"><subfield code="c">© 2007</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (xix, 321 Seiten)</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="490" ind1="1" ind2=" "><subfield code="a">Progress in astronautics and aeronautics</subfield><subfield code="v">volume 221</subfield></datafield><datafield tag="505" ind1="8" ind2=" "><subfield code="a">Includes bibliographical references and index</subfield></datafield><datafield tag="505" ind1="8" ind2=" "><subfield code="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</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Liquid propellant rockets</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rocket engines</subfield><subfield code="x">Combustion</subfield><subfield code="z">Russia (Federation)</subfield><subfield code="x">Testing</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Liquid fuels</subfield><subfield code="x">Combustion</subfield><subfield code="z">Russia (Federation)</subfield><subfield code="x">Testing</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rockets (Aeronautics)</subfield><subfield code="z">Russia (Federation)</subfield><subfield code="x">Testing</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flüssigkeitsraketentriebwerk</subfield><subfield code="0">(DE-588)4448628-5</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Entwurf</subfield><subfield code="0">(DE-588)4121208-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Flüssigkeitsraketentriebwerk</subfield><subfield code="0">(DE-588)4448628-5</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="2"><subfield code="a">Entwurf</subfield><subfield code="0">(DE-588)4121208-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Yang, Vigor</subfield><subfield code="4">edt</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Culick, Fred E.C.</subfield><subfield code="d">1933-</subfield><subfield code="0">(DE-588)1089461704</subfield><subfield code="4">edt</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Talley, Douglas G.</subfield><subfield code="4">edt</subfield></datafield><datafield tag="776" ind1="0" ind2="8"><subfield code="i">Erscheint auch als</subfield><subfield code="n">Druck-Ausgabe</subfield><subfield code="z">978-1-56347-921-2</subfield></datafield><datafield tag="776" ind1="0" ind2="8"><subfield code="i">Erscheint auch als</subfield><subfield code="n">Druck-Ausgabe</subfield><subfield code="z">1-56347-921-4</subfield></datafield><datafield tag="830" ind1=" " ind2="0"><subfield code="a">Progress in astronautics and aeronautics</subfield><subfield code="v">221</subfield><subfield code="w">(DE-604)BV045507833</subfield><subfield code="9">221</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">http://www.doi.org/10.2514/4.866906</subfield><subfield code="x">Verlag</subfield><subfield code="z">URL des Erstveröffentlichers</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-283-AERC</subfield><subfield code="a">ZDB-38-ESG</subfield><subfield code="a">ZDB-283-APAA</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-030241790</subfield></datafield><datafield tag="966" ind1="e" ind2=" "><subfield code="u">http://www.doi.org/10.2514/4.866906</subfield><subfield code="l">UBY01</subfield><subfield code="p">ZDB-283-AERC</subfield><subfield code="x">Verlag</subfield><subfield code="3">Volltext</subfield></datafield></record></collection> |
| id | DE-604.BV044846929 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T08:02:44Z |
| institution | BVB |
| isbn | 9781600866906 9781600864711 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030241790 |
| oclc_num | 774285720 |
| open_access_boolean | |
| owner | DE-83 DE-706 |
| owner_facet | DE-83 DE-706 |
| physical | 1 Online-Ressource (xix, 321 Seiten) |
| psigel | ZDB-283-AERC ZDB-38-ESG ZDB-283-APAA |
| publishDate | 2007 |
| publishDateSearch | 2007 |
| publishDateSort | 2007 |
| publisher | American Institute of Aeronautics and Astronautics |
| record_format | marc |
| series | Progress in astronautics and aeronautics |
| series2 | Progress in astronautics and aeronautics |
| spelling | Dranovskij, Mark Lʹvovič Verfasser (DE-588)1067777962 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 [2007] © 2007 1 Online-Ressource (xix, 321 Seiten) txt rdacontent c rdamedia cr rdacarrier Progress in astronautics and aeronautics volume 221 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 Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd rswk-swf Entwurf (DE-588)4121208-3 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 edt Culick, Fred E.C. 1933- (DE-588)1089461704 edt Talley, Douglas G. edt Erscheint auch als Druck-Ausgabe 978-1-56347-921-2 Erscheint auch als Druck-Ausgabe 1-56347-921-4 Progress in astronautics and aeronautics 221 (DE-604)BV045507833 221 http://www.doi.org/10.2514/4.866906 Verlag URL des Erstveröffentlichers Volltext |
| spellingShingle | Dranovskij, Mark Lʹvovič Combustion instabilities in liquid rocket engines testing and development practices in Russia 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 Raketentriebwerk (DE-588)4176905-3 gnd Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd Entwurf (DE-588)4121208-3 gnd |
| subject_GND | (DE-588)4176905-3 (DE-588)4448628-5 (DE-588)4121208-3 |
| 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 Raketentriebwerk (DE-588)4176905-3 gnd Flüssigkeitsraketentriebwerk (DE-588)4448628-5 gnd Entwurf (DE-588)4121208-3 gnd |
| topic_facet | Liquid propellant rockets Rocket engines Combustion Russia (Federation) Testing Liquid fuels Combustion Russia (Federation) Testing Rockets (Aeronautics) Russia (Federation) Testing Raketentriebwerk Flüssigkeitsraketentriebwerk Entwurf |
| url | http://www.doi.org/10.2514/4.866906 |
| volume_link | (DE-604)BV045507833 |
| work_keys_str_mv | AT dranovskijmarklʹvovic combustioninstabilitiesinliquidrocketenginestestinganddevelopmentpracticesinrussia AT yangvigor combustioninstabilitiesinliquidrocketenginestestinganddevelopmentpracticesinrussia AT culickfredec combustioninstabilitiesinliquidrocketenginestestinganddevelopmentpracticesinrussia AT talleydouglasg combustioninstabilitiesinliquidrocketenginestestinganddevelopmentpracticesinrussia |