Messerschmitt ME-70 Corvenius

Official name: ME-70 Corvenius

Based on IFX-45B Cygnus (two seater version) airframe [link] , it's role as a demonstrator aircraft, testing the experimental Hybrid Turbo Fan - Pulse Detonation Hybrid / Scramjet engines, also enhanced Stealth from titanium-ceramic composite skin, and enhanced fighter maneuverability. The major differences are reinforced cockpit canopy, short tail boom, enlarge Delta Wing, horizontal stabilizers, small fixed front canard, and Dorsal Engine Air Intakes.

The weapon bay has been used for extra fuel tanks, contains experimental catalized A-1 metane, used for the Pulse Detonation engines .

General Spesification:

Crew: Two (Pilot, and Data Gathering Officer)
Powerplant: 2× Lambda Power LTF 3000V-3D afterburning with three dimensional thrust-vectored turbofans of 350 kN each. Combined with 4 x Argus II experimental Pulse Detonation/Scramjet engines.
Maximum speed: Mach 5+
Range: Classified
Service ceiling: >50,000 ft (15,000 m)

The two center wing Pods has been removed for redesigned aerolastic delta wing.

Avionics
Euroradar CAPTOR-S AESA Radar.
Passive Infra-Red Airborne Tracking Equipment (PIRATE).
Lambda Electronic Division AN/AAQ-78 Distributed Aperture System (DAS) missile warning system.
Sentry Alliance AN/ASQ-539 (Sentinel) electronic warfare system.
EADS Multifunction Advanced Data Link (MADL) communication system.

Commission for anw-rev [link]