Rocket propulsion:
"This text is intended to provide undergraduate and first year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fl...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Cambridge
Cambridge University Press
2019
|
| Schlagworte: | |
| Zusammenfassung: | "This text is intended to provide undergraduate and first year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fluid flow in addition to a background in chemistry at least to the college freshman level. Fundamentally, the text has been developed as a compilation of resources from two courses offered at Purdue University: AAE439, Rocket Propulsion and AAE539, Advanced Rocket Propulsion. The former course is taught at the Senior level, while the latter is targeted to Seniors and first year graduate students. The primary emphasis of the text is placed in the area of chemical rocket propulsion systems, the realm that includes solid rocket motors, liquid rocket propulsion devices and hybrid systems that utilize one liquid propellant and one solid propellant. Electric and nuclear propulsion devices are not discussed in detail, but are highlighted briefly within this chapter to place them within the broad context of existing or future rocket propulsion devices. Specifically, this book places emphasis on the propellant systems, combustion processes and thermodynamic and fluid flow processes occurring within the rocket combustion chamber and nozzle. In addition, overall system sizing is presented as well as the interaction of propulsion system performance with vehicle trajectory calculations. Control and structural aspects of a rocket are not considered in detail in this course, but structural issues and sizing considerations are discussed at a mainly conceptual level"... |
| Beschreibung: | Includes bibliographical references |
| Beschreibung: | xiii, 574 Seiten Illustrationen, Diagramme |
| ISBN: | 9781108422277 |
Internformat
MARC
| LEADER | 00000nam a2200000 c 4500 | ||
|---|---|---|---|
| 001 | BV045511625 | ||
| 003 | DE-604 | ||
| 005 | 20190507 | ||
| 007 | t | ||
| 008 | 190314s2019 xxua||| |||| 00||| eng d | ||
| 010 | |a 018036914 | ||
| 020 | |a 9781108422277 |9 978-1-108-42227-7 | ||
| 035 | |a (OCoLC)1090777401 | ||
| 035 | |a (DE-599)BVBBV045511625 | ||
| 040 | |a DE-604 |b ger |e rda | ||
| 041 | 0 | |a eng | |
| 044 | |a xxu |c US | ||
| 049 | |a DE-858 |a DE-83 |a DE-706 | ||
| 050 | 0 | |a TL782 | |
| 082 | 0 | |a 621.43/56 |2 23 | |
| 084 | |a ZO 8150 |0 (DE-625)157874: |2 rvk | ||
| 100 | 1 | |a Heister, Stephen D. |4 aut | |
| 245 | 1 | 0 | |a Rocket propulsion |c Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne) |
| 264 | 1 | |a Cambridge |b Cambridge University Press |c 2019 | |
| 300 | |a xiii, 574 Seiten |b Illustrationen, Diagramme | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 500 | |a Includes bibliographical references | ||
| 520 | |a "This text is intended to provide undergraduate and first year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fluid flow in addition to a background in chemistry at least to the college freshman level. Fundamentally, the text has been developed as a compilation of resources from two courses offered at Purdue University: AAE439, Rocket Propulsion and AAE539, Advanced Rocket Propulsion. The former course is taught at the Senior level, while the latter is targeted to Seniors and first year graduate students. The primary emphasis of the text is placed in the area of chemical rocket propulsion systems, the realm that includes solid rocket motors, liquid rocket propulsion devices and hybrid systems that utilize one liquid propellant and one solid propellant. Electric and nuclear propulsion devices are not discussed in detail, but are highlighted briefly within this chapter to place them within the broad context of existing or future rocket propulsion devices. Specifically, this book places emphasis on the propellant systems, combustion processes and thermodynamic and fluid flow processes occurring within the rocket combustion chamber and nozzle. In addition, overall system sizing is presented as well as the interaction of propulsion system performance with vehicle trajectory calculations. Control and structural aspects of a rocket are not considered in detail in this course, but structural issues and sizing considerations are discussed at a mainly conceptual level"... | ||
| 650 | 4 | |a Rockets (Aeronautics) | |
| 650 | 4 | |a Jet propulsion | |
| 650 | 4 | |a Rocket engines | |
| 650 | 0 | 7 | |a Luftstrahltriebwerk |0 (DE-588)4128278-4 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Rakete |0 (DE-588)4124022-4 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Rakete |0 (DE-588)4124022-4 |D s |
| 689 | 0 | 1 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 0 | 2 | |a Luftstrahltriebwerk |0 (DE-588)4128278-4 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Anderson, William E. |4 aut | |
| 700 | 1 | |a Pourpoint, Timothée L. |4 aut | |
| 700 | 1 | |a Cassady, R. Joseph |4 aut | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-030896111 | ||
Datensatz im Suchindex
| _version_ | 1804179455540723712 |
|---|---|
| any_adam_object | |
| author | Heister, Stephen D. Anderson, William E. Pourpoint, Timothée L. Cassady, R. Joseph |
| author_facet | Heister, Stephen D. Anderson, William E. Pourpoint, Timothée L. Cassady, R. Joseph |
| author_role | aut aut aut aut |
| author_sort | Heister, Stephen D. |
| author_variant | s d h sd sdh w e a we wea t l p tl tlp r j c rj rjc |
| building | Verbundindex |
| bvnumber | BV045511625 |
| callnumber-first | T - Technology |
| callnumber-label | TL782 |
| callnumber-raw | TL782 |
| callnumber-search | TL782 |
| callnumber-sort | TL 3782 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 8150 |
| ctrlnum | (OCoLC)1090777401 (DE-599)BVBBV045511625 |
| 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 Verkehr / Transport |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>03393nam a2200493 c 4500</leader><controlfield tag="001">BV045511625</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20190507 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">190314s2019 xxua||| |||| 00||| eng d</controlfield><datafield tag="010" ind1=" " ind2=" "><subfield code="a">018036914</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781108422277</subfield><subfield code="9">978-1-108-42227-7</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)1090777401</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV045511625</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rda</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="044" ind1=" " ind2=" "><subfield code="a">xxu</subfield><subfield code="c">US</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-858</subfield><subfield code="a">DE-83</subfield><subfield code="a">DE-706</subfield></datafield><datafield tag="050" ind1=" " ind2="0"><subfield code="a">TL782</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">621.43/56</subfield><subfield code="2">23</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">ZO 8150</subfield><subfield code="0">(DE-625)157874:</subfield><subfield code="2">rvk</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Heister, Stephen D.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Rocket propulsion</subfield><subfield code="c">Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne)</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Cambridge</subfield><subfield code="b">Cambridge University Press</subfield><subfield code="c">2019</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">xiii, 574 Seiten</subfield><subfield code="b">Illustrationen, Diagramme</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">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Includes bibliographical references</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">"This text is intended to provide undergraduate and first year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fluid flow in addition to a background in chemistry at least to the college freshman level. Fundamentally, the text has been developed as a compilation of resources from two courses offered at Purdue University: AAE439, Rocket Propulsion and AAE539, Advanced Rocket Propulsion. The former course is taught at the Senior level, while the latter is targeted to Seniors and first year graduate students. The primary emphasis of the text is placed in the area of chemical rocket propulsion systems, the realm that includes solid rocket motors, liquid rocket propulsion devices and hybrid systems that utilize one liquid propellant and one solid propellant. Electric and nuclear propulsion devices are not discussed in detail, but are highlighted briefly within this chapter to place them within the broad context of existing or future rocket propulsion devices. Specifically, this book places emphasis on the propellant systems, combustion processes and thermodynamic and fluid flow processes occurring within the rocket combustion chamber and nozzle. In addition, overall system sizing is presented as well as the interaction of propulsion system performance with vehicle trajectory calculations. Control and structural aspects of a rocket are not considered in detail in this course, but structural issues and sizing considerations are discussed at a mainly conceptual level"...</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rockets (Aeronautics)</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Jet propulsion</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rocket engines</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Luftstrahltriebwerk</subfield><subfield code="0">(DE-588)4128278-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Rakete</subfield><subfield code="0">(DE-588)4124022-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</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="689" ind1="0" ind2="0"><subfield code="a">Rakete</subfield><subfield code="0">(DE-588)4124022-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><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="2"><subfield code="a">Luftstrahltriebwerk</subfield><subfield code="0">(DE-588)4128278-4</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">Anderson, William E.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Pourpoint, Timothée L.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Cassady, R. Joseph</subfield><subfield code="4">aut</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-030896111</subfield></datafield></record></collection> |
| id | DE-604.BV045511625 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T08:20:08Z |
| institution | BVB |
| isbn | 9781108422277 |
| language | English |
| lccn | 018036914 |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030896111 |
| oclc_num | 1090777401 |
| open_access_boolean | |
| owner | DE-858 DE-83 DE-706 |
| owner_facet | DE-858 DE-83 DE-706 |
| physical | xiii, 574 Seiten Illustrationen, Diagramme |
| publishDate | 2019 |
| publishDateSearch | 2019 |
| publishDateSort | 2019 |
| publisher | Cambridge University Press |
| record_format | marc |
| spelling | Heister, Stephen D. aut Rocket propulsion Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne) Cambridge Cambridge University Press 2019 xiii, 574 Seiten Illustrationen, Diagramme txt rdacontent n rdamedia nc rdacarrier Includes bibliographical references "This text is intended to provide undergraduate and first year graduate students with an introduction to the principles governing the design and performance of rocket propulsion systems. Readers of the text are expected to have a good working knowledge of thermodynamics and the principles of fluid flow in addition to a background in chemistry at least to the college freshman level. Fundamentally, the text has been developed as a compilation of resources from two courses offered at Purdue University: AAE439, Rocket Propulsion and AAE539, Advanced Rocket Propulsion. The former course is taught at the Senior level, while the latter is targeted to Seniors and first year graduate students. The primary emphasis of the text is placed in the area of chemical rocket propulsion systems, the realm that includes solid rocket motors, liquid rocket propulsion devices and hybrid systems that utilize one liquid propellant and one solid propellant. Electric and nuclear propulsion devices are not discussed in detail, but are highlighted briefly within this chapter to place them within the broad context of existing or future rocket propulsion devices. Specifically, this book places emphasis on the propellant systems, combustion processes and thermodynamic and fluid flow processes occurring within the rocket combustion chamber and nozzle. In addition, overall system sizing is presented as well as the interaction of propulsion system performance with vehicle trajectory calculations. Control and structural aspects of a rocket are not considered in detail in this course, but structural issues and sizing considerations are discussed at a mainly conceptual level"... Rockets (Aeronautics) Jet propulsion Rocket engines Luftstrahltriebwerk (DE-588)4128278-4 gnd rswk-swf Rakete (DE-588)4124022-4 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Rakete (DE-588)4124022-4 s Raketentriebwerk (DE-588)4176905-3 s Luftstrahltriebwerk (DE-588)4128278-4 s DE-604 Anderson, William E. aut Pourpoint, Timothée L. aut Cassady, R. Joseph aut |
| spellingShingle | Heister, Stephen D. Anderson, William E. Pourpoint, Timothée L. Cassady, R. Joseph Rocket propulsion Rockets (Aeronautics) Jet propulsion Rocket engines Luftstrahltriebwerk (DE-588)4128278-4 gnd Rakete (DE-588)4124022-4 gnd Raketentriebwerk (DE-588)4176905-3 gnd |
| subject_GND | (DE-588)4128278-4 (DE-588)4124022-4 (DE-588)4176905-3 |
| title | Rocket propulsion |
| title_auth | Rocket propulsion |
| title_exact_search | Rocket propulsion |
| title_full | Rocket propulsion Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne) |
| title_fullStr | Rocket propulsion Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne) |
| title_full_unstemmed | Rocket propulsion Stephen D. Heister (Purdue University, Indiana), William E. Anderson (Purdue University, Indiana), Timothee Pourpoint (Purdue University, Indiana), R. Joseph Cassady (Aerojet Rocketdyne) |
| title_short | Rocket propulsion |
| title_sort | rocket propulsion |
| topic | Rockets (Aeronautics) Jet propulsion Rocket engines Luftstrahltriebwerk (DE-588)4128278-4 gnd Rakete (DE-588)4124022-4 gnd Raketentriebwerk (DE-588)4176905-3 gnd |
| topic_facet | Rockets (Aeronautics) Jet propulsion Rocket engines Luftstrahltriebwerk Rakete Raketentriebwerk |
| work_keys_str_mv | AT heisterstephend rocketpropulsion AT andersonwilliame rocketpropulsion AT pourpointtimotheel rocketpropulsion AT cassadyrjoseph rocketpropulsion |