LifeRCraft Airframe - Central and Front Fuselage Sections - Design, Optimization, Manufacturing, V&V including Airworthiness Substantiation

Fuselage to be integrated with tail unit realised as part of the AIRFRAME ITD Topic 02-02 (ref. JTI-CS2-CPW-AIR-02-02; WP B4.1-2) and with wing realized in AIRFRAME ITD Topic 02-04 (ref. JTI-CS2-CPW-AIR-02-04; WP B1.1-2)

The optimized main airframe supports the wing, the main gearboxes, and the engines. It includes the cabin, the cockpit and integrates the main system of the aircraft. The activities cover the structural design according to Airbus Helicopters specification and architecture, the stress analysis, the manufacturing of the demonstrator airframe.

Please refer for the full and formal topic description to Annex I of the Clean Sky 2 Work Plan 2014-2015 (see under the tab ""Topic Conditions and Documents"")