MFFD
Thermoplastic composites, thermoplastic advanced fibre placement (T-AFP), in-situ consolidation (ISC), flashlamp heating, continuous ultrasonic welding (cUS), resistance welding (RW), MFFD Project.
TB-Rumpf
As part of the TB-Rumpf project, the autoclave-free consolidation of thermoplastic laminates and resistance welding are being further developed and validated as technology bricks for future thermoplastic aircraft fuselages.
NACOR
Update on HLFC technology: The newly developed Tailored Skin Single Duct (TSSD) design for wing or empennage leading edges significantly reduces production costs, especially of the microperforated outer skin.
Innovative Cooling of Rocket Combustion Chambers
PROCOMP
Further development of structures made of carbon fibre-reinforced high-performance plastics for space travel.
AeroLight
AeroLight is a multidisciplinary DLR project involving different DLR-Institutes. Its aim is to use new technologies to design and build a highly loaded compressor stage consisting of a rotor and tandem stator and ultimately integrate this into a test rig.
CRISP/AGATA
CRISP Organoblech is part of the DLR project CRISPmulti for the multidisciplinary development and testing of a highly efficient counter-rotating fan stage made from CFRP for the next generation of aircraft engines with a very high bypass ratio.
CREVAD
Crash evaluation of alternative CFRP fuselage designs
ATEK
Repairing fibre-reinforced polymer structures
Effiziente und flexible Heiztechnologie mittels Induktion
Adjustment ring for compressor guide vanes
Hybrid Unison Ring for aero engine guide vanes
PulForm
Energieeffiziente Herstellung komplexer Hochleistungsfaserverbundbauteile
RoCk
Robuste CFK-Gesamtprozesskette
ATLLAS II
Aero-Thermodynamic Loads on Lightweight Advanced Structures II
AZIMUT
Automatisierung zukunftsweisender industrieller Methoden und Technologien für CFK-Rümpfe
FAST20XX
Future high-Altitude high-Speed Transport 20XX
CompTAB
Manufacturing simulation for fibre-reinforced thermoplastics
LamAiR
vertical stabiliser with less drag
Raumgleiter
REX-Free Flyer
LIBCOS
Load upon Impact Behaviour of Composite Structure
MAAXIMUS
More Affordable Aircraft through eXtended, Integrated and Mature nUmerical Sizing
EXPERT
European experimental re-entry test-bed
CELPACT
Progressive missiles technologies (FFT)
ALCAS
Outer Guide Vane in VITAL
Outer Guide Vane
DLR-Project "Combustion Chamber 2000"
Helisafe TA
FOTON-M2
Feuertaufe in der Plasmawolke
SHEFEX
Sharp Edge Flight Experiment
Nose cap of the CRV test plant X-38