short takeoff and landing aircraft

Short Takeoff And Landing Aircraft - The abbreviation STOL is used in aviation as an abbreviation for take-off and landing and refers to the length of runway, land or water required for take-off and landing. A STOL aircraft is located on a small body of water or a suitable area for take-off and landing.

A significant amount of energy is spent on minimum airspeed (also known as stall speed) to reduce the required runway length. Because the STOL series is more related to this number. In terms of flight, the large power-to-weight ratio and low drag help the aircraft accelerate into flight. On the other hand, runway requirements are reduced by strong brakes, low airspeeds, and rollbacks or crashes.

Short Takeoff And Landing Aircraft

STOL performance is generally a measure of the length of runway required to land or take off, whichever is longer. STOL performance for the Viking Twin Otter Series 400 is tabulated here.

Stol Aircraft Editorial Photo. Image Of Rough, Avionics

The Twin Otter is the only utility turbine offering STOL performance with a flight range of 1,200 feet (366 meters).

Google Translate is provided as a free tool to improve the usability of the Viking Air website. Therefore, Viking is not responsible for Google Translate™. A short takeoff and landing (STOL) aircraft is a conventional winged aircraft with short takeoff and landing requirements. Most STOL aircraft have various configurations for use in extreme weather conditions (such as high altitude or ice). STOL aircraft, including those used by scheduled passenger airlines, are operated at STOLports that include short runways.

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Most winged STOL aircraft are stealth aircraft, some such as the De Gavilland Canada Dash-7 are designed for use at ready airfields; likewise, PAC is the manufacturer of many STOL aircraft, with exceptions such as the P-750 XSTOL, Quest Kodiak, de Gavilland Canada DHC-6 Twin Otter, and Peterson 260SE. Autogyros also have STOL capability, needing a short ground range to get airborne but capable of landing on the ground.

Mojave Short Takeoff And Landing Uas, Usa

The runway length requirement is a quadratic function of the minimum takeoff speed (slump speed) and most design effort is spent on reducing this number. The high power-to-weight ratio and low drag help the aircraft accelerate on takeoff. Stalls are reduced by strong brakes, low landing speed, thrust reversers or scrapers (less common). STOL performance is generally determined by the length of runway required for landing or takeoff, whichever is longer.

Equally important to sprinting is the ability to overcome obstacles such as hills for takeoff and landing. The high power-to-weight ratio at takeoff and low air resistance result in the high climb required to overcome obstacles. Drag to land allows the aircraft to land straight down the runway, resulting in a longer runway. Drag is increased by flaps (devices on the wings) and forward thrust (which causes the air to fly slightly sideways to allow the aircraft to climb).

A STOL aircraft will typically have a large wing for its weight. These wings often use aerodynamic devices such as flaps, slats, slats, and vortex generators.

Aircraft design for STOL performance typically reduces top speed but does not reduce payload capacity. Cargo transport is critical because many small, isolated communities rely on STOL aircraft as their only transport link to the outside world for passengers or cargo; examples include many communities in northern Canada and Alaska.

Light General Aviation Airplane With Smoke Coming Out The Exhaust System During Engine Start. Small Yellow Plane With Stol (short Takeoff And Landing Stock Photo

Most STOL aircraft can land on or off the airport. Off-airport landing areas include snow or ice (using ice), fields or wet riverbanks (often using special oil, low-pressure tundra tires) and water (using floats): these areas are often very short and covered with tall trees. creates an obstacle. or hills. Wheel skids and amphibious floats combine wheels with skids or floats, allowing the choice of landing on snow/water or a prepared runway.

STOLports are not common but can be found for example at London City Airport in London, England. There were several STOLports in the United States that were used for scheduled passenger flights, but are no longer available.

CESTOL Efficient Short Takeoff and Landing (CESTOL) aircraft with very short runway and high cruise speed (greater than Mach 0.8) requirements.

Many different STOL definitions have been used by different authorities and nations at different times and for many regulatory and military purposes.

Short Takeoff And Landing (stol) Aircraft

Short takeoff and landing: (DOD/NATO) Ability of aircraft to clear an obstacle within 1,500 feet (450 meters) of a 50-foot (15-meter) obstacle within 1,500 feet (450 meters) of a 50-foot (15-meter) obstacle after passing . Also STOL.—Defense Dictionary of Military and Allied Terms (JP 1-02) [17]

STOL (Short take-off and landing). Aircraft STOL performance is the aircraft's ability to negotiate and clear a 50-meter obstacle within 1,500 meters of takeoff. It must also be able to stop at 1,500 feet after clearing a 50-foot landing obstacle. - Glossary of terms in the field of aviation [18]

Aircraft capable of operating from a designated STOL runway within an approved operating weight and meeting STOL specifications and airworthiness, operational, noise and pollution standards means any aircraft capable of "flying" with atmospheric support - Transport Canada [19] [20] and Arizona Department of Transportation [21]

A STOL aircraft is an aircraft with a certified performance capability to conduct an approach angle of 6 degrees or more in vertical glide and a 15:1 missed approach safe height at sea level with a rate of climb of 15:1... The STOL runway is specifically designed for STOL operation of aircraft and with a form developed and maintained according to established and defined standards. - US Federal Aviation Administration [22]

What It's Like To Land On The World's Shortest Commercial Runway

Heavier aircraft that cannot take off and land vertically, but can operate in tighter spaces than required by aircraft of the same size. Taken from short takeoff and landing aircraft. - McGraw-Hill Dictionary of Words and Technical Terms [23]

Short take-off and landing (STOL) aircraft, a heavier aircraft capable of taking off and landing only with a short runway, but not vertically. The exact definition of a STOL aircraft is not universally agreed upon. However, only 1,000 feet (305 m) of runway was required for takeoff, and 50 feet (15 m) of that distance was defined as the aircraft being able to clear the obstacle and being cleared after landing. Same obstacle and terrain at 1,000 feet. - Columbia Encyclopedia [16]

STOL flight mode is the speed at which the aircraft is controlled to climb or land and operated at an airspeed lower than the stall speed. - Lt. Col. Walter P. Meyersperger, USAF (Ret) [24]

In addition, some aircraft manufacturers market their products as STOL without demonstrating that the aircraft meets the accepted definition.

Advanced Air Mobility: Using A Short Takeoff And Landing Aircraft Design

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