Abstract The Combustion Dynamics group in the Rocket Propulsion Department at the
German Aerospace Center (DLR), Lampoldshausen, strives to advance the understanding …

This paper reports the results of a test campaign of a laser-ignited combustion chamber with
15 shear coaxial injectors for the propellant combination LOX/methane. 259 ignition tests …

This paper reports the investigation of acoustic combustion instability experienced during
repetitive ignition testing of a sub-scale LOX-methane rocket thrust chamber. The …

Ammonium dinitramide (ADN)-based energetic ionic liquid propellants (ADN-EILPs) present
considerable potential as monopropellants due to high energy density, high …

During the last years the CTR HiPoLas ignition system, originally developed for the ignition
of automotive engines, has reached a sufficiently high level of stability and miniaturization to …

R ignition of the combustion chamber is essential for the functioning of a rocket engine and
in consequence for the complete launcher system. A failed ignition leads to the loss of the …

This paper reports the investigation of the laser ignition of a breadboard thruster with a
porous injector head. Ignition tests were performed for 80 and 980 mbar combustion …

Up to the present, no studies have been published to investigate the ignition process in air
heater. In this paper, spray combustion flow field during ignition process in air heater was …

In order to investigate into the laser ignition process for a multi-injector configuration under
low pressure conditions, a test campaign at the M3. 1 test bench of the DLR Institute of …

Laser Ignition of Cryogenic Propellants in Space Propulsion Page 1 AW3I.7.pdf CLEO 2019 ©
OSA 2019 Laser Ignition of Cryogenic Propellants in Space Propulsion Robert Stützer …