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Design and first results of an injector test setup for green hypergolic propellants

Lauck, Felix and Witte, Jan and Negri, Michele and Freudenmann, Dominic and Schlechtriem, Stefan (2019) Design and first results of an injector test setup for green hypergolic propellants. In: AIAA Propulsion and Energy 2019 Forum. AIAA Propulsion and Energy 2019 Forum, 19.-22. Aug. 2019, Indianapolis, Indiana, USA. DOI: 10.2514/6.2019-4279

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2019-4279

Abstract

Investigations for the development of new liquid green hypergolic propellants are carried out by the Propellants department of DLR Lampoldshausen. One part of the development includes testing of new propellants under flowing conditions to determine the ignition delay time. Therefore an injector test setup was designed and put into operation. For first hypergolic ignition tests a proven hypergolic propellant consisting of Block 0 and highly concentrated hydrogen peroxide was chosen. Drop tests with Block 0 and hydrogen peroxide were conducted. The average ignition delay time was 20.5 ms. For tests under flowing conditions a 2on1 impinging injector was designed and manufactured. The minimum ignition delay time during injector tests was 190 ms.

Item URL in elib:https://elib.dlr.de/131644/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2019-4015 Session: Flowpath Dynamics and Control
Title:Design and first results of an injector test setup for green hypergolic propellants
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lauck, FelixFelix.Lauck (at) dlr.dehttps://orcid.org/0000-0002-6599-0805
Witte, JanInstitute of Space Propulsion, DLR Lampoldshausen, DUNSPECIFIED
Negri, MicheleMichele.Negri (at) dlr.dehttps://orcid.org/0000-0003-2204-9916
Freudenmann, DominicDominic.Freudenmann (at) dlr.dehttps://orcid.org/0000-0003-4027-8878
Schlechtriem, Stefanstefan.schlechtriem (at) dlr.dehttps://orcid.org/0000-0002-3714-9664
Date:22 August 2019
Journal or Publication Title:AIAA Propulsion and Energy 2019 Forum
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2019-4279
Status:Published
Keywords:hydrogen peroxide, green propellants, hypergolic, injector, ignition
Event Title:AIAA Propulsion and Energy 2019 Forum
Event Location:Indianapolis, Indiana, USA
Event Type:international Conference
Event Dates:19.-22. Aug. 2019
Organizer:AIAA - American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):Grüne Geltreibstoffe für Raumfahrtrelevante Anwendungen (GGeRA)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Propellants
Institute of Space Propulsion > Leitungsbereich RA
Deposited By: Hanke, Michaela
Deposited On:02 Dec 2019 08:14
Last Modified:13 Jan 2020 11:15

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