Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander

Schmierer, C. and Tomilin, K. and Kobald, Mario and Steelant, Johan and Schlechtriem, S. (2016) Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander. Space Propulsion 2016, 02.-06. Mai 2016, Rom, Italien.

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Item URL in elib:

https://elib.dlr.de/105038/

Document Type:

Conference or Workshop Item (Speech)

Title:

Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Schmierer, C.	christian.schmierer (at) dlr.de	UNSPECIFIED
Tomilin, K.	konstantin.tomilin (at) dlr.de	UNSPECIFIED
Kobald, Mario	Mario.Kobald (at) dlr.de	https://orcid.org/0000-0002-1708-3944
Steelant, Johan	ESA-ESTEC, NL	UNSPECIFIED
Schlechtriem, S.	Stefan.Schlechtriem (at) dlr.de	UNSPECIFIED

Date:

2 May 2016

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

Hybrid rocket Propulsion, lunar lander, H2O2, LOX, Paraffin fuel

Event Title:

Space Propulsion 2016

Event Location:

Rom, Italien

Event Type:

international Conference

Event Dates:

02.-06. Mai 2016

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 - Raketenantriebtests (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Propellants

Deposited By:

Kobald, Dr. Mario

Deposited On:

04 Jul 2016 09:48

Last Modified:

01 Dec 2018 19:52

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