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: | Undetermined |
| Veröffentlicht: |
Köln
Wiss. Berichtswesen der DLR
1991
|
| Ausgabe: | (Als Ms. gedr.) |
| Beschreibung: | VII, 98 S. graph. Darst. |
Internformat
MARC
| LEADER | 00000nam a2200000 c 4500 | ||
|---|---|---|---|
| 001 | BV024370092 | ||
| 003 | DE-604 | ||
| 005 | 20090910 | ||
| 007 | t | ||
| 008 | 910902s1991 d||| t||| 00||| und d | ||
| 035 | |a (OCoLC)75203544 | ||
| 035 | |a (DE-599)BVBBV024370092 | ||
| 040 | |a DE-604 |b ger |e rakwb | ||
| 041 | |a und | ||
| 049 | |a DE-83 | ||
| 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 | ||
| 999 | |a oai:aleph.bib-bvb.de:BVB01-018350705 | ||
Datensatz im Suchindex
| _version_ | 1804140325597347840 |
|---|---|
| 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 | BV024370092 |
| ctrlnum | (OCoLC)75203544 (DE-599)BVBBV024370092 |
| edition | (Als Ms. gedr.) |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>00841nam a2200265 c 4500</leader><controlfield tag="001">BV024370092</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20090910 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">910902s1991 d||| t||| 00||| und d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)75203544</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV024370092</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">und</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-83</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="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-018350705</subfield></datafield></record></collection> |
| id | DE-604.BV024370092 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T21:58:11Z |
| institution | BVB |
| language | Undetermined |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-018350705 |
| oclc_num | 75203544 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | VII, 98 S. graph. Darst. |
| publishDate | 1991 |
| publishDateSearch | 1991 |
| publishDateSort | 1991 |
| publisher | Wiss. Berichtswesen der DLR |
| record_format | marc |
| 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 |
| spellingShingle | Manski, Detlef Comparison of kinetic, equilibrium and frozen rocket expansion obtained at different propulsive parameters for launcher and spacecraft engines |
| 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 |
| work_keys_str_mv | AT manskidetlef comparisonofkineticequilibriumandfrozenrocketexpansionobtainedatdifferentpropulsiveparametersforlauncherandspacecraftengines |