Boman, A. und Häggander, J. und Hass, J. (1999) Laser Welded Channel Wall Nozzle Design, Manufacturing and Hot Gas Testing. 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-24, 1999.
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Kurzfassung
A sub-scale laser welded channel wall nozzle has been designed and manufactured by Volvo Aero Corp., Trollhättan. Eight hot gas tests at the P8 test facility in Lampoldshausen were performed during December 1998 - January 1999. The nozzle test objectives were met. A hydrogen coolant pressure level of 200 bar at a combustion chamber pressure level of 100 bar was reached. The major objectives of the test campaign was reached; the qualification of DLR's model D combustor, the simultaneous regulation of the combustion chamber and the nozzle extension via two supply lines and the qualification of VAC's welded channel wall nozzle.
elib-URL des Eintrags: | https://elib.dlr.de/1399/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=1999, | ||||||||||||||||
Titel: | Laser Welded Channel Wall Nozzle Design, Manufacturing and Hot Gas Testing | ||||||||||||||||
Autoren: |
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Datum: | 1999 | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
Herausgeber: |
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Status: | veröffentlicht | ||||||||||||||||
Veranstaltungstitel: | 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-24, 1999 | ||||||||||||||||
Veranstalter : | AIAA | ||||||||||||||||
HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||
HGF - Programm: | Weltraum (alt) | ||||||||||||||||
HGF - Programmthema: | W RP - Raumtransport | ||||||||||||||||
DLR - Schwerpunkt: | Weltraum | ||||||||||||||||
DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | E - keine Zuordnung | ||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe | ||||||||||||||||
Hinterlegt von: | Lohmiller, Monika | ||||||||||||||||
Hinterlegt am: | 16 Sep 2005 | ||||||||||||||||
Letzte Änderung: | 06 Jan 2010 13:43 |
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