Wird es wieder zivilen Überschallluftverkehr geben?? 26
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Ja! Die Fortschritte die gemacht wurden erlauben dies! (11) 42%
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Nein! Schon alleine wegen der Umwelt! (10) 38%
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Wenn ja , dann nur unter extremen Auflagen! (5) 19%
Die Specs der Aerion
Webseite von Aerion!
ZitatAlles anzeigenMaximum cruise speed: 1.6 Mach
Long range cruise (supersonic): 1.5 Mach
No boom cruise (supersonic): ~1.1 to 1.2 Mach
High speed cruise (subsonic): .99 Mach
Long range cruise (subsonic): .95 Mach
Maximum takeoff weight: 90,000 pounds
Basic operating weight: 45,100 pounds
Maximum fuel: 45,400 pounds
Engines: Two PW JT8D-219
Thrust: Flat rated to 19,600
Wing area: 1,200 sq. ft.
Approach speed: 120 kts*
Balanced Field length < 6,000 feet
Landing distance, wet runway: 3,460 feet
Range (NBAA IFR): > 4,000 nm
Ceiling: 51,000 feet
* Typical end of mission weight
Hat so ein Flieger ne Zukunft, wenn man die technischen Fortschritte in Betracht zieht??
Was meint ihr??
Es hat doch was, in FL 510 Alles stehen zu lassen, was nicht militärischer Flugverkehr ist.........
Nach diesen Fortschritten??
ZitatTwo of the biggest names in aerospace, Boeing and Lockheed Martin, have both submitted designs to NASA for possible supersonic jets–like the Concorde, but without the noise.
The designs are not entirely dissimilar from the Concorde, with very long and narrow bodies and possibly a dipped nose, but also have a few key differences the designers and engineers hope will lessen the supersonic boom the Concorde created.
The Concorde’s supersonic boom was created when the shock wave from the plane’s high speed collided with the ground. It was so loud that the Concorde was actually forbidden from flying over land in the continental United States, with rare exceptions.
Designers and engineers have been working for years on a solution to this problem. Both the Boeing and Lockheed Martin designs place the engines on top of the wing, rather than underneath, hoping that the wing itself will reduce the volume of the boom. Lockheed Martin also has an odd, inverted-V-shaped tail that might lessen the boom through airflow control.