Paper information

Paper code

IAC-18,C4,2,8,x42795

Date

2018-10-02

Time

11:45

Order

8

Room

ZARM 5

Title

Characterization of Regression Rate and Combustion Process in a High-Pressure 2D Hybrid Rocket Engine with Optical Access

abstract

View PDF

Session

2. Propulsion System (2)

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-18

Type of presentation

oral

Main author

Mr. Georg Poppe, German Aerospace Center (DLR), Germany

Co-authors

Prof. Ognjan Božić, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

Mr. Stefan May, German Aerospace Center (DLR), Germany;

Mrs. Nora M. Bierwagen, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

Mr. Rolfes Steffen, Germany;

Mr. Patrick Koch, Germany;