Combustion Stability Characteristics of Coax-Swirl-Injectors for Oxygen/Kerosene
- Author(s):
- S. Soller ( Technische Universität München, Garching, Germany )
- R. Wagner
- H. Kau
- P. Martin ( Astrium Space Transportation, Munich, Germany )
- C. Maeding
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-5563
- Paper no.:
- AIAA Paper 2007-5563
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200716 [CD-ROM 2007 Disc 16]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Characterisation of Main Chamber Injectors for GOX/Kerosene in a Single Element Rocket Combustor
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Combustion Stability Assessment of Double Swirl Coaxial Injectors Using Simulant Propellants
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Characterisation of Combustion and Heat Transfer using GOX/Kerosene in a Single-Element Rocket Combustor
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Parametric Study on Combustion Characteristics of Bi-Liquid Swirl Coaxial Injectors
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Design and Commissioning of a Combustion Chamber for Cooling and Material Investigations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Experimental study on combustion stability characteristics of non-swirl coaxial injectors
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Effects of LOx Post Recess on the Combustion Characteristics for Bi-Swirl Coaxial Injector
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine
American Institute of Aeronautics and Astronautics |