ATLLAS: M3 CAD- and mass-model

Kurzfassung

Within the ATLLAS (Aerodynamic and Thermal Load Interactions with Lightweight Advanced Materials for High Speed Flight) a 200-seat SST concept will be designed in WP 2.3 to meet an operational requirement of Mach 3 flight over a 5500 nm range. The Mach 3 speed range allows consideration of established materials and newer materials. The Mach 3 vehicle will be designed along the principles outlined in WP2.1 and WP2.2 by GDL and system mass and payload fraction will be predicted by DLR-SART and GDL respectively. DLR-SART provides the creation and the iterative adaptation of the semi-detailed CAD-representation of the Mach 3 SST-vehicle in support of the design process. The objective of this report in support of deliverable D2.3.3 is the description of the semi-detailed CAD model for the M3 configuration. In addition to this model a mass estimation is done and a calculation and the CoG shifting is analysed.