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Design Study of a 30kN LOX/LCH4 Aerospike Rocket Engine for Lunar Lander Application

Stark, Ralf and Bartel, Sebastian and Ditsche, Florian and Esch, Thomas (2023) Design Study of a 30kN LOX/LCH4 Aerospike Rocket Engine for Lunar Lander Application. Aerospace Europe Conference 2023 / Joint 10th EUCASS – 9th CEAS Conference, 09.-13. Juli 2023, Lausanne, Schweiz. (In Press)

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Abstract

Based on lunar lander concept EL3, various LOX/CH4 aerospike engines were studied. A distinction was made between single and cluster configurations as well as ideal and non-ideal contour concepts. It could be shown that non-ideal aerospike engines promise a significant payload gain.

Item URL in elib:https://elib.dlr.de/196178/
Document Type:Conference or Workshop Item (Speech)
Title:Design Study of a 30kN LOX/LCH4 Aerospike Rocket Engine for Lunar Lander Application
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Stark, RalfUNSPECIFIEDhttps://orcid.org/0000-0003-1923-1901UNSPECIFIED
Bartel, SebastianFH AachenUNSPECIFIEDUNSPECIFIED
Ditsche, FlorianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Esch, ThomasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:12 July 2023
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:In Press
Keywords:Aerospike, Nozzle, Lunar Lander, EL3
Event Title:Aerospace Europe Conference 2023 / Joint 10th EUCASS – 9th CEAS Conference
Event Location:Lausanne, Schweiz
Event Type:international Conference
Event Dates:09.-13. Juli 2023
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 - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Stark, Dr.-Ing. Ralf
Deposited On:11 Aug 2023 11:36
Last Modified:11 Aug 2023 11:36

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