Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Gerhard Kroupa"'
Publikováno v:
Laser Technology for Defense and Security XVII.
Autor:
Gerhard Kroupa, Michael Börner
Publikováno v:
International Conference on Space Optics — ICSO 2018.
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 enable competitive operation on space craft engines 1. The f
Autor:
Chiara Manfletti, Michael Börner, Dmitry Suslov, Michael Oschwald, Justin Hardi, Gerhard Kroupa
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 were performed for sea-level conditions. The igniter based on a mon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb38d127ec263a553f2ccb78639189f8
https://elib.dlr.de/123955/
https://elib.dlr.de/123955/
In search of reliable and light-weight ignition systems for re-ignitable upper stage engines, a laser ignition system was adapted and tested on an experimental combustion chamber for propellant injection into low combustion chamber pressures at 50–
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1fa15d81ebce465db4d0ef47516217eb
https://doi.org/10.1007/s12567-017-0161-9
https://doi.org/10.1007/s12567-017-0161-9
This paper reports on the repetitive laser ignition by optical breakdown within an experimental rocket combustion chamber. Ignition was performed by focusing a laser pulse generated by a miniaturized diode-pumped Nd:YAG laser system. The system, whic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b1c42ba24731b921b7aae28163cf4b10
https://doi.org/10.1007/s12567-017-0163-7
https://doi.org/10.1007/s12567-017-0163-7
Publikováno v:
Laser Ignition Conference 2017.
Promising a number of advantages compared to existing ignition systems, the use of focused laser light to generate a spark for ignition in rocket combustion chambers has been studied around the world for several years now. At Airbus Safran Launchers,
Laser Ignition for Aerospace Applications using the Rugged Miniaturized HiPoLas® Nd-YAG Laser System
Publikováno v:
Laser Ignition Conference 2017.
We present an overview on requirements on a laser igniter for aerospace applications. A summary on the development history of the CTR HiPoLas ignition system is given and performance data of the latest generation including testing under harsh environ
Autor:
Chiara Manfletti, Gerhard Kroupa
Publikováno v:
Optics express. 21
An experimental study has been conducted to assess the feasibility of implementing laser ignition in cryogenic reaction and control and orbital manouvering thrusters. A experimental thruster with a single-coaxial injector element combustion chamber f
Autor:
Mario Villa, Gerhard Kroupa, Gudrun Bruckner, M. Hainbuchner, Matthias Baron, Helmut Rauch, Heinz Amenitsch, E. Seidl
Publikováno v:
Journal of Applied Crystallography. 33:851-854
In 1998, the combined Interferometer and Ultra Small Angle Neutron Scattering (USANS) instrument S18 at the 58 MW High Flux Reactor at the Institute Laue-Langevin in Grenoble (France) started operation. The instrument has been upgraded to allow more
Publikováno v:
Optical Engineering. 48:014202
A robust, miniaturized, diode-pumped high-energy neodymium doped yttrium aluminium garnet (Nd:YAG) laser with passive Q-switch generating 25 mJ at 3 ns has been demonstrated at repetition rates of up to 150 Hz. The device is designed for ignition of