LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -

Génin, C. and Schneider, Dirk and Tomita, T. and Takahashi, H. (2015) LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -. 51st AIAA Joint Propulsion Conference, 27. - 29. Jul. 2015, Orlando, FL, USA. doi: 10.2514/6.2015-4155.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/99606/

Document Type:

Conference or Workshop Item (Speech)

Title:

LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Génin, C.	UNSPECIFIED	UNSPECIFIED
Schneider, Dirk	UNSPECIFIED	https://orcid.org/0000-0002-4785-4244
Tomita, T.	JAXA Kakuda, Japan	UNSPECIFIED
Takahashi, H.	JAXA Kakuda, Japan	UNSPECIFIED

Date:

2015

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

DOI:

10.2514/6.2015-4155

Status:

Published

Keywords:

Dual Bell Nozzle

Event Title:

51st AIAA Joint Propulsion Conference

Event Location:

Orlando, FL, USA

Event Type:

international Conference

Event Dates:

27. - 29. Jul. 2015

Organizer:

AIAA

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transportation

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Space Transportation

DLR - Research theme (Project):

R - Antriebsystemtechnik - Schubkammertechnologie (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion

Deposited By:

Hanke, Michaela

Deposited On:

20 Nov 2015 09:11

Last Modified:

01 Dec 2018 19:51

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