Nothing Special   »   [go: up one dir, main page]
Wikipedia

V/STOL

(Redirected from Vertical/Short Takeoff and Landing)
Not to be confused with STOVL.

A vertical and/or short take-off and landing (V/STOL) aircraft is an airplane able to take-off or land vertically or on short runways. Vertical takeoff and landing (VTOL) aircraft are a subset of V/STOL craft that do not require runways at all. Generally, a V/STOL aircraft needs to be able to hover. Helicopters are not considered under the V/STOL classification as the classification is only used for aeroplanes, aircraft that achieve lift (force) in forward flight by planing the air, thereby achieving speed and fuel efficiency that is typically greater than the capability of helicopters.

RAF Harrier GR9 arrives at RIAT 2008
A U.S. Marine Corps MV-22 Osprey prepares to land aboard a ship

Most V/STOL aircraft types were experiments or outright failures from the 1950s to 1970s. V/STOL aircraft types that have been produced in large numbers include the F-35B Lightning II, Harrier and V-22 Osprey.

A rolling takeoff, sometimes with a ramp (ski-jump), reduces the amount of thrust required to lift an aircraft from the ground (compared with vertical takeoff), and hence increases the payload and range that can be achieved for a given thrust. For instance, the Harrier is incapable of taking off vertically with full weapons and fuel load. Hence V/STOL aircraft generally use a runway if it is available. I.e. short takeoff and vertical landing (STOVL) or conventional takeoff and landing (CTOL) operation is preferred to VTOL operation.

V/STOL was developed to allow fast jets to be operated from clearings in forests, from very short runways, and from small aircraft carriers that would previously only have been able to carry helicopters.

The main advantage of V/STOL aircraft is closer basing to the enemy, which reduces response time and tanker support requirements. In the case of the Falklands War, it also permitted high-performance fighter air cover and ground attack without a large aircraft carrier equipped with aircraft catapult.

Lists of V/STOL aircraft

edit

This is a partial list; there have been many designs for V/STOL aircraft.

Vectored thrust

edit

Tilt-jet

edit

Tilt-rotor

edit

Tilt-wing

edit

Separate thrust and lift

edit

Supersonic

edit

Although many aircraft have been proposed and built, with a few being tested, the F-35B is the first and only supersonic V/STOL aircraft to have reached operational service, having entered service in 2016.[1]

  • Bell D-188A Mach 2 swivelling engines, mockup stage
  • EWR VJ 101 Mach 2 fighter, flown to Mach 1.04 but not operational
  • Dassault Mirage IIIV Delta wing Mach 2 fighter with lift engines, first VTOL capable of supersonic and Mach 2 flight (Mach 2.03 during tests), not operational
  • Hawker Siddeley HS 138 Strike fighter with lift fans, It was not completed
  • Hawker Siddeley P.1017 Lift engines with thrust vectoring. It was not completed
  • Hawker Siddeley P.1154 M1.7 Supersonic Harrier. It was not completed
  • Hawker Siddeley P.1184-16 Dash 18
  • Hawker Siddeley P.1217
  • Republic AP-100 strike fighter concept
  • Convair Model 200 Lift engines plus swivel tailpipe, not built
  • Rockwell XFV-12 Built with complex "window blind" wings but could not lift its own weight
  • Yakovlev Yak-141 Lift engines plus swivel tailpipe
  • Lockheed Martin X-35B / F-35B uses a vectored-thrust tailpipe (the Pratt & Whitney F135) plus a shaft-driven lifting fan. It is the first aircraft capable of demonstrating transition from short take-off to supersonic flight to vertical landing on the same sortie.[2]

References

edit
  1. ^ "Report: F-35 Work Falls Behind Two More Years." Archived 2009-07-27 at the Wayback Machine CQ Politics, 23 July 2009.
  2. ^ Kjelgaard, Chris (Senior Editor). "From Supersonic to Hover: How the F-35 Flies." space.com, 21 December 2007.
edit
 
Wikimedia Commons has media related to V/STOL aircraft.
Retrieved from "https://en.wikipedia.org/w/index.php?title=V/STOL&oldid=1221559105"