Add to ORKGThe presentation describes the ongoing technology development of a fiber reinforced ceramic rocket combustion chamber with transpiration cooling. Cooling techniques suitable for CMC material characteristics and design/manufacturing concepts for both combustion chamber and new injection concepts are explained. Finally test results from recent test campaigns at test benches of DLR Lampoldshausen are presented
The development of ceramic composites with optimized fiber architectures for application in hyperson...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
A viewgraph presentation outlines NASA's goals for the Second and Third Generation Reusable Launch V...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
The development of ceramic rocket engine thrust chambers at the German Aerospace Center (DLR) curren...
The long-term development of transpiration cooled ceramic rocket thrust chambers at the German Aero...
A new approach followed by DLR since some years is the realization of a revolutionary combustion cha...
Propulsion systems are an essential key for efficient future space transportation systems (STS) and ...
Within the "Propulsion 2010" Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
Within the ʻPropulsion 2010ʼ Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
which was signed in 2006, Astrium and DLR agreed to work jointly on Ceramic Matrix Composite (CMC) m...
Within the ʻPropulsion 2010ʼ Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
Regeneratively cooled ceramic matrix composite (CMC) structures are being considered for use along t...
Technologies for porous effusion or transpiration cooled ceramic combustion chambers are under inves...
The development of ceramic composites with optimized fiber architectures for application in hyperson...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
A viewgraph presentation outlines NASA's goals for the Second and Third Generation Reusable Launch V...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
The development of ceramic rocket engine thrust chambers at the German Aerospace Center (DLR) curren...
The long-term development of transpiration cooled ceramic rocket thrust chambers at the German Aero...
A new approach followed by DLR since some years is the realization of a revolutionary combustion cha...
Propulsion systems are an essential key for efficient future space transportation systems (STS) and ...
Within the "Propulsion 2010" Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
Within the ʻPropulsion 2010ʼ Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
which was signed in 2006, Astrium and DLR agreed to work jointly on Ceramic Matrix Composite (CMC) m...
Within the ʻPropulsion 2010ʼ Memorandum of Understanding (MoU) which was signed in 2006, Astrium and...
Regeneratively cooled ceramic matrix composite (CMC) structures are being considered for use along t...
Technologies for porous effusion or transpiration cooled ceramic combustion chambers are under inves...
The development of ceramic composites with optimized fiber architectures for application in hyperson...
The long-term development of ceramic rocket engine thrust chambers at the German Aerospace Center (D...
A viewgraph presentation outlines NASA's goals for the Second and Third Generation Reusable Launch V...