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FIRST RESULTS OF REGRESSION RATE MEASUREMENTS ON ULTRASONIC BASIS IN THE AHRES HYBRID ROCKET MOTOR

Porrmann, Dennis and Wilken, Jascha and Bozic, Ognjan and Lancelle, Daniel (2014) FIRST RESULTS OF REGRESSION RATE MEASUREMENTS ON ULTRASONIC BASIS IN THE AHRES HYBRID ROCKET MOTOR. Space Propulsion 2014, 19.-22. May 2014, Köln, Deutschland.

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Abstract

The project “Advanced Hybrid Rocket Engine Simulation” (AHRES) aims to develop software for hybrid rocket engine performance calculation. The German Aerospace Center (DLR) has equipped a hybrid rocket testbed with an ultrasonic regression rate measurement system, which can track the regression rate at 2 points of the fuel grain. Within this paper the ultrasonic system is described in detail. The problem of calibrating the ultrasonic system and the correction of errors due to heat profile and pressure is discussed. The results of a 10 s hot test run are presented.

Item URL in elib:https://elib.dlr.de/90839/
Document Type:Conference or Workshop Item (Speech)
Title:FIRST RESULTS OF REGRESSION RATE MEASUREMENTS ON ULTRASONIC BASIS IN THE AHRES HYBRID ROCKET MOTOR
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Porrmann, DennisUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wilken, JaschaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Bozic, OgnjanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Lancelle, DanielUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:May 2014
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybrid Rocket Ahres Ultrasonic HTPB hydrogen peroxide H2O2
Event Title:Space Propulsion 2014
Event Location:Köln, Deutschland
Event Type:international Conference
Event Dates:19.-22. May 2014
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 - Vorhaben AHRES (old)
Location: Braunschweig , Stuttgart
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Technical Physics > Studies and Concepts
Deposited By: Porrmann, Dennis
Deposited On:07 Oct 2014 13:16
Last Modified:31 Jul 2019 19:48

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