The control moment distribution for the Do 31 hovering rig:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Paris
AGARD
1965
|
| Schriftenreihe: | NATO, Advisory Group for Aerospace Research and Development Report
522 |
| Schlagworte: | |
| Beschreibung: | V, 25 S. Ill., graph. Darst. |
Internformat
MARC
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| 040 | |a DE-604 |b ger | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-706 | ||
| 088 | |a Report 522 | ||
| 100 | 1 | |a Schweizer, G. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a The control moment distribution for the Do 31 hovering rig |c by G. Schweizer and H. Seelmann |
| 264 | 1 | |a Paris |b AGARD |c 1965 | |
| 300 | |a V, 25 S. |b Ill., graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a Report / NATO, Advisory Group for Aerospace Research and Development |v 522 | |
| 650 | 0 | 7 | |a Senkrechtstarter |0 (DE-588)4077369-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Flugmanöver |0 (DE-588)4442557-0 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Steuerungstechnik |0 (DE-588)4116615-2 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Flugerprobung |0 (DE-588)4352769-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Do 31 |0 (DE-588)7602116-6 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Do 31 |0 (DE-588)7602116-6 |D s |
| 689 | 0 | 1 | |a Senkrechtstarter |0 (DE-588)4077369-3 |D s |
| 689 | 0 | 2 | |a Flugerprobung |0 (DE-588)4352769-3 |D s |
| 689 | 0 | 3 | |a Flugmanöver |0 (DE-588)4442557-0 |D s |
| 689 | 0 | 4 | |a Steuerungstechnik |0 (DE-588)4116615-2 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Seelmann, H. |e Verfasser |4 aut | |
| 800 | 1 | |a NATO, Advisory Group for Aerospace Research and Development |t Report |v 522 |w (DE-604)BV006657616 |9 522 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-025193590 | ||
Datensatz im Suchindex
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| any_adam_object | |
| author | Schweizer, G. Seelmann, H. |
| author_facet | Schweizer, G. Seelmann, H. |
| author_role | aut aut |
| author_sort | Schweizer, G. |
| author_variant | g s gs h s hs |
| building | Verbundindex |
| bvnumber | BV040339299 |
| ctrlnum | (OCoLC)812197815 (DE-599)GBV517178419 |
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| id | DE-604.BV040339299 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T00:21:58Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-025193590 |
| oclc_num | 812197815 |
| open_access_boolean | |
| owner | DE-706 |
| owner_facet | DE-706 |
| physical | V, 25 S. Ill., graph. Darst. |
| publishDate | 1965 |
| publishDateSearch | 1965 |
| publishDateSort | 1965 |
| publisher | AGARD |
| record_format | marc |
| series | NATO, Advisory Group for Aerospace Research and Development Report |
| series2 | Report / NATO, Advisory Group for Aerospace Research and Development |
| spelling | Schweizer, G. Verfasser aut The control moment distribution for the Do 31 hovering rig by G. Schweizer and H. Seelmann Paris AGARD 1965 V, 25 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Report / NATO, Advisory Group for Aerospace Research and Development 522 Senkrechtstarter (DE-588)4077369-3 gnd rswk-swf Flugmanöver (DE-588)4442557-0 gnd rswk-swf Steuerungstechnik (DE-588)4116615-2 gnd rswk-swf Flugerprobung (DE-588)4352769-3 gnd rswk-swf Do 31 (DE-588)7602116-6 gnd rswk-swf Do 31 (DE-588)7602116-6 s Senkrechtstarter (DE-588)4077369-3 s Flugerprobung (DE-588)4352769-3 s Flugmanöver (DE-588)4442557-0 s Steuerungstechnik (DE-588)4116615-2 s DE-604 Seelmann, H. Verfasser aut NATO, Advisory Group for Aerospace Research and Development Report 522 (DE-604)BV006657616 522 |
| spellingShingle | Schweizer, G. Seelmann, H. The control moment distribution for the Do 31 hovering rig NATO, Advisory Group for Aerospace Research and Development Report Senkrechtstarter (DE-588)4077369-3 gnd Flugmanöver (DE-588)4442557-0 gnd Steuerungstechnik (DE-588)4116615-2 gnd Flugerprobung (DE-588)4352769-3 gnd Do 31 (DE-588)7602116-6 gnd |
| subject_GND | (DE-588)4077369-3 (DE-588)4442557-0 (DE-588)4116615-2 (DE-588)4352769-3 (DE-588)7602116-6 |
| title | The control moment distribution for the Do 31 hovering rig |
| title_auth | The control moment distribution for the Do 31 hovering rig |
| title_exact_search | The control moment distribution for the Do 31 hovering rig |
| title_full | The control moment distribution for the Do 31 hovering rig by G. Schweizer and H. Seelmann |
| title_fullStr | The control moment distribution for the Do 31 hovering rig by G. Schweizer and H. Seelmann |
| title_full_unstemmed | The control moment distribution for the Do 31 hovering rig by G. Schweizer and H. Seelmann |
| title_short | The control moment distribution for the Do 31 hovering rig |
| title_sort | the control moment distribution for the do 31 hovering rig |
| topic | Senkrechtstarter (DE-588)4077369-3 gnd Flugmanöver (DE-588)4442557-0 gnd Steuerungstechnik (DE-588)4116615-2 gnd Flugerprobung (DE-588)4352769-3 gnd Do 31 (DE-588)7602116-6 gnd |
| topic_facet | Senkrechtstarter Flugmanöver Steuerungstechnik Flugerprobung Do 31 |
| volume_link | (DE-604)BV006657616 |
| work_keys_str_mv | AT schweizerg thecontrolmomentdistributionforthedo31hoveringrig AT seelmannh thecontrolmomentdistributionforthedo31hoveringrig |