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Design of a hovering sounding rocket stage for measurements in the high atmosphere

Naumann, K. and Kirchberger, Christoph and Drescher, Oliver and Hargarten, Dorian and Zurkaulen, Maximilian and Haubl, Alexander and Rest, S. and Niedermaier, H. and Ramsel, Jürgen (2020) Design of a hovering sounding rocket stage for measurements in the high atmosphere. 7th Edition of the Space Propulsion Conference, 2021-03-17 - 2021-03-19, virtuelle Konferenz. (Submitted)

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Abstract

In order to perform specific measurements in the high atmosphere region, the High Atmosphere Soarer (HAS) sounding rocket upper stage is under development at the German Aerospace Center and Bayern-Chemie. This paper briefly describes the scientific mission behind as well as the HAS vehicle concept. More emphasis is dedicated to the description of the trajectory, the technology of the controllable gelled propellant rocket motor and the design of the remaining key propulsion system components.

Item URL in elib:https://elib.dlr.de/140301/
Document Type:Conference or Workshop Item (Speech)
Title:Design of a hovering sounding rocket stage for measurements in the high atmosphere
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Naumann, K.Bayern-Chemie, Anschau am Inn, GermanyUNSPECIFIEDUNSPECIFIED
Kirchberger, ChristophUNSPECIFIEDhttps://orcid.org/0000-0002-7574-2581UNSPECIFIED
Drescher, OliverUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hargarten, DorianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Zurkaulen, MaximilianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Haubl, AlexanderUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Rest, S.Bayern-Chemie GmbH, Aschau/Inn, DUNSPECIFIEDUNSPECIFIED
Niedermaier, H.Bayern-Chemie GmbH, Aschau/Inn, DUNSPECIFIEDUNSPECIFIED
Ramsel, JürgenBayern-Chemie GmbH (MBDA-D), AschauUNSPECIFIEDUNSPECIFIED
Date:27 December 2020
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Submitted
Keywords:sounding rocket, high atmosphere research, controllable rocket motor, gelled propellant rocket motor, thrust vector control, cold gas reaction control, propellant tank, high pressure system
Event Title:7th Edition of the Space Propulsion Conference
Event Location:virtuelle Konferenz
Event Type:international Conference
Event Start Date:17 March 2021
Event End Date:19 March 2021
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Vorhaben Mobile Raketenbasis (MORABA) (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Space Operations and Astronaut Training > Mobile Rocket Base
Institute of Space Propulsion
Deposited By: Völk, Dr. Stefan
Deposited On:13 Jan 2021 08:45
Last Modified:24 Apr 2024 20:41

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