Propellant Vaporization as a design criterion for rocket-engine combustian chambers:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | Undetermined |
| Veröffentlicht: |
Washington, DC
U.S. Government Printing Office
1960
|
| Schriftenreihe: | Technical report / National Aeronautics and Space Administration
R-67 |
| Beschreibung: | 55 S. graph. Darst. |
Internformat
MARC
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| 088 | |a NASA TR R 67 | ||
| 100 | 1 | |a Priem, Richard J. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Propellant Vaporization as a design criterion for rocket-engine combustian chambers |c by Richard J. Priem and Marcus F. Heidmann |
| 264 | 1 | |a Washington, DC |b U.S. Government Printing Office |c 1960 | |
| 300 | |a 55 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Technical report / National Aeronautics and Space Administration |v R-67 | |
| 700 | 1 | |a Heidmann, Marcus F. |e Verfasser |4 aut | |
| 940 | 1 | |q TUB-nve | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-018549872 | ||
Datensatz im Suchindex
| _version_ | 1804140586977984512 |
|---|---|
| any_adam_object | |
| author | Priem, Richard J. Heidmann, Marcus F. |
| author_facet | Priem, Richard J. Heidmann, Marcus F. |
| author_role | aut aut |
| author_sort | Priem, Richard J. |
| author_variant | r j p rj rjp m f h mf mfh |
| building | Verbundindex |
| bvnumber | BV024576365 |
| ctrlnum | (OCoLC)312835911 (DE-599)BVBBV024576365 |
| format | Book |
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| id | DE-604.BV024576365 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T22:02:20Z |
| institution | BVB |
| language | Undetermined |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-018549872 |
| oclc_num | 312835911 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | 55 S. graph. Darst. |
| psigel | TUB-nve |
| publishDate | 1960 |
| publishDateSearch | 1960 |
| publishDateSort | 1960 |
| publisher | U.S. Government Printing Office |
| record_format | marc |
| series2 | Technical report / National Aeronautics and Space Administration |
| spelling | Priem, Richard J. Verfasser aut Propellant Vaporization as a design criterion for rocket-engine combustian chambers by Richard J. Priem and Marcus F. Heidmann Washington, DC U.S. Government Printing Office 1960 55 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Technical report / National Aeronautics and Space Administration R-67 Heidmann, Marcus F. Verfasser aut |
| spellingShingle | Priem, Richard J. Heidmann, Marcus F. Propellant Vaporization as a design criterion for rocket-engine combustian chambers |
| title | Propellant Vaporization as a design criterion for rocket-engine combustian chambers |
| title_auth | Propellant Vaporization as a design criterion for rocket-engine combustian chambers |
| title_exact_search | Propellant Vaporization as a design criterion for rocket-engine combustian chambers |
| title_full | Propellant Vaporization as a design criterion for rocket-engine combustian chambers by Richard J. Priem and Marcus F. Heidmann |
| title_fullStr | Propellant Vaporization as a design criterion for rocket-engine combustian chambers by Richard J. Priem and Marcus F. Heidmann |
| title_full_unstemmed | Propellant Vaporization as a design criterion for rocket-engine combustian chambers by Richard J. Priem and Marcus F. Heidmann |
| title_short | Propellant Vaporization as a design criterion for rocket-engine combustian chambers |
| title_sort | propellant vaporization as a design criterion for rocket engine combustian chambers |
| work_keys_str_mv | AT priemrichardj propellantvaporizationasadesigncriterionforrocketenginecombustianchambers AT heidmannmarcusf propellantvaporizationasadesigncriterionforrocketenginecombustianchambers |