R 🔍


1980: eine XV-15 mit schwenkbaren Rotoren hebt als Senkrechtstarter ab: das maximale Startgewicht lag bei 6804 kg, die Antriebsleistung bei 1344 Kilowatt für 2 Minuten. Damit kann eine Steigrate von 16 Metern in jeder Sekunde erreicht werden. © NASA => Zurück zum Artikel


Senkrechtstarter


Bildinfo und Lizenz


Bildinfo


  • 1980: eine XV-15 mit schwenkbaren Rotoren hebt als Senkrechtstarter ab: das maximale Startgewicht lag bei 6804 kg, die Antriebsleistung bei 1344 Kilowatt für 2 Minuten. Damit kann eine Steigrate von 16 Metern in jeder Sekunde erreicht werden.
  • Technische Daten:
  • Crew: 2 on Rockwell-Columbus LW-3B ejection seats
  • Capacity: up to 9 passengers if seats fitted / 3,400 lb (1,542 kg) max. payload STOL
  • Width: 57 ft 2 in (17.42 m) overall with rotors turning
  • Height: 12 ft 8 in (3.86 m) over tail fins (15 ft 4 in (5 m) with nacelles vertical)
  • Wing area: 169 sq ft (15.7 m2)
  • Airfoil: Wings - NACA 64A015[10]
  • Empty weight: 9,570 lb (4,341 kg)
  • Gross weight: 13,000 lb (5,897 kg) VTO
  • Max takeoff weight: 15,000 lb (6,804 kg) STO
  • Fuel capacity: 229 US gal (191 imp gal; 867 l) in four wing tanks
  • Powerplant: 2 × Textron Lycoming LTC1K-4K turboshaft / turboprop engines, 1,550 shp (1,160 kW) each normal takeoff power (10 min max):1,802 shp (1,344 kW) emergency power (2 min max) (modified Lycoming T53-L-13B)
  • Main rotor diameter: 2 × 25 ft (7.6 m)
  • Main rotor area: 981.8 sq ft (91.21 m2) total
  • Blade section (original): - root: NACA 64-935/528/118; tip: NACA 64-(1.5)12/208[10]
  • Blade section (Boeing ATB): - root: V43030-1.58/VR-7; tip: Boeing VR-8[10]
  • Maximum speed: 332 kn (382 mph, 615 km/h) at 17,000 ft (5,182 m)
  • Cruise speed: 303 kn (349 mph, 561 km/h) max. at 16,500 ft (5,029 m) (200 kn (230 mph; 370 km/h) at 20,000 ft (6,096 m))
  • Never exceed speed: 364 kn (419 mph, 674 km/h)
  • Range: 445 nmi (512 mi, 824 km) with maximum fuel
  • Service ceiling: 29,000 ft (8,800 m)
  • Service ceiling OEI: 15,000 ft (4,572 m)
  • Hover ceiling IGE: 10,500 ft (3,200 m)
  • Hover ceiling OGE: 8,650 ft (2,637 m)
  • Rate of climb: 3,150 ft/min (16.0 m/s) at sea level
  • Disk loading: 15.2 lb/sq ft (74 kg/m2)
  • Power/mass: 0.45 hp/lb (1 kW/kg)[12]
  • Originalbeschriftung: XV-15 tilt rotor takeoff - first NASA Dryden flight from the U.S. Army Engineering Flight Activity hangars Edwards AFB, California
  • Das Bild ist gegenüber dem Original von links nach rechts gespiegelt.

Source


  • Created: October, 1980
  • Author: NASA

License


  • Public Domain: This image was taken from the Getty Research Institute's Open Content Program, which states the following regarding their assessment that no known copyright restrictions exist: Open content images are digital surrogates of works of art that are in the Getty's collections and in the public domain, for which we hold all rights, or for which we are not aware of any rights restrictions. While the Getty Research Institute cannot make an absolute statement on the copyright status of a given image, "Open content images can be used for any purpose without first seeking permission from the Getty."
  • This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted".

Warranty


  • No guarantee can be given as to the correctness of facts implied or explicitly stated.
  • Usage is completey at your own risk. 💣

Originalseite


  • Das Bild ist Teil eines online-Lexikons.
  • Rhetos Lernlexikon Mathematik, Aachen: