Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | German |
| Veröffentlicht: |
Köln
Wiss. Berichtswesen der DLR
1991
|
| Ausgabe: | (Als Ms. gedr.) |
| Schriftenreihe: | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung
1991,2 |
| Schlagworte: | |
| Beschreibung: | Zsfassung in dt. Sprache |
| Beschreibung: | VII, 98 S. graph. Darst. |
Internformat
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV004457742 | ||
| 003 | DE-604 | ||
| 005 | 19981203 | ||
| 007 | t | ||
| 008 | 910705s1991 gw d||| t||| 00||| ger d | ||
| 035 | |a (OCoLC)75203544 | ||
| 035 | |a (DE-599)BVBBV004457742 | ||
| 040 | |a DE-604 |b ger |e rakddb | ||
| 041 | 0 | |a ger | |
| 044 | |a gw |c DE | ||
| 049 | |a DE-12 |a DE-91G |a DE-210 |a DE-706 | ||
| 088 | |a DLR Mitt. 91 02 | ||
| 100 | 1 | |a Manski, Detlef |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |c Detlef Manski |
| 250 | |a (Als Ms. gedr.) | ||
| 264 | 1 | |a Köln |b Wiss. Berichtswesen der DLR |c 1991 | |
| 300 | |a VII, 98 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung |v 1991,2 | |
| 500 | |a Zsfassung in dt. Sprache | ||
| 650 | 7 | |a Expansion |2 swd | |
| 650 | 7 | |a Impuls |2 swd | |
| 650 | 7 | |a Kinetik |2 swd | |
| 650 | 7 | |a Raketentriebwerk |2 swd | |
| 650 | 7 | |a Raumfahrzeug |2 swd | |
| 650 | 7 | |a Strömung |2 swd | |
| 830 | 0 | |a Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung |v 1991,2 |w (DE-604)BV011753181 |9 1991,2 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-002763669 | ||
Datensatz im Suchindex
| _version_ | 1804118627392159744 |
|---|---|
| any_adam_object | |
| author | Manski, Detlef |
| author_facet | Manski, Detlef |
| author_role | aut |
| author_sort | Manski, Detlef |
| author_variant | d m dm |
| building | Verbundindex |
| bvnumber | BV004457742 |
| ctrlnum | (OCoLC)75203544 (DE-599)BVBBV004457742 |
| edition | (Als Ms. gedr.) |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01342nam a2200385 cb4500</leader><controlfield tag="001">BV004457742</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">19981203 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">910705s1991 gw d||| t||| 00||| ger d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)75203544</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV004457742</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rakddb</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">ger</subfield></datafield><datafield tag="044" ind1=" " ind2=" "><subfield code="a">gw</subfield><subfield code="c">DE</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-12</subfield><subfield code="a">DE-91G</subfield><subfield code="a">DE-210</subfield><subfield code="a">DE-706</subfield></datafield><datafield tag="088" ind1=" " ind2=" "><subfield code="a">DLR Mitt. 91 02</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Manski, Detlef</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines</subfield><subfield code="c">Detlef Manski</subfield></datafield><datafield tag="250" ind1=" " ind2=" "><subfield code="a">(Als Ms. gedr.)</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Köln</subfield><subfield code="b">Wiss. Berichtswesen der DLR</subfield><subfield code="c">1991</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">VII, 98 S.</subfield><subfield code="b">graph. Darst.</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="490" ind1="1" ind2=" "><subfield code="a">Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung</subfield><subfield code="v">1991,2</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Zsfassung in dt. Sprache</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Expansion</subfield><subfield code="2">swd</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Impuls</subfield><subfield code="2">swd</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Kinetik</subfield><subfield code="2">swd</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Raketentriebwerk</subfield><subfield code="2">swd</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Raumfahrzeug</subfield><subfield code="2">swd</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Strömung</subfield><subfield code="2">swd</subfield></datafield><datafield tag="830" ind1=" " ind2="0"><subfield code="a">Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung</subfield><subfield code="v">1991,2</subfield><subfield code="w">(DE-604)BV011753181</subfield><subfield code="9">1991,2</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-002763669</subfield></datafield></record></collection> |
| id | DE-604.BV004457742 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T16:13:18Z |
| institution | BVB |
| language | German |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-002763669 |
| oclc_num | 75203544 |
| open_access_boolean | |
| owner | DE-12 DE-91G DE-BY-TUM DE-210 DE-706 |
| owner_facet | DE-12 DE-91G DE-BY-TUM DE-210 DE-706 |
| physical | VII, 98 S. graph. Darst. |
| publishDate | 1991 |
| publishDateSearch | 1991 |
| publishDateSort | 1991 |
| publisher | Wiss. Berichtswesen der DLR |
| record_format | marc |
| series | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung |
| series2 | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung |
| spelling | Manski, Detlef Verfasser aut Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines Detlef Manski (Als Ms. gedr.) Köln Wiss. Berichtswesen der DLR 1991 VII, 98 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung 1991,2 Zsfassung in dt. Sprache Expansion swd Impuls swd Kinetik swd Raketentriebwerk swd Raumfahrzeug swd Strömung swd Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung 1991,2 (DE-604)BV011753181 1991,2 |
| spellingShingle | Manski, Detlef Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Mitteilung Expansion swd Impuls swd Kinetik swd Raketentriebwerk swd Raumfahrzeug swd Strömung swd |
| title | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| title_auth | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| title_exact_search | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| title_full | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines Detlef Manski |
| title_fullStr | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines Detlef Manski |
| title_full_unstemmed | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines Detlef Manski |
| title_short | Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| title_sort | comparison of kinetic equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| topic | Expansion swd Impuls swd Kinetik swd Raketentriebwerk swd Raumfahrzeug swd Strömung swd |
| topic_facet | Expansion Impuls Kinetik Raketentriebwerk Raumfahrzeug Strömung |
| volume_link | (DE-604)BV011753181 |
| work_keys_str_mv | AT manskidetlef comparisonofkineticequilibriumandfrozenrocketexpansionobtainedatdifferentpropulsiveparametersforlauncherandspacecraftengines |