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Motor glider

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270: 672: 315: 578: 75: 255: 611: 39: 499: 350:, the propeller folds into the nose cone, and is connected to the rear-mounted engine with a drive shaft. It also has two retractable main wheels, allowing it to be taxied without assistance, and to soar with low drag. These features make it a cross-over between the touring and retractable propeller motor gliders. It does not have a tow-hook, so it must self-launch. The S10-VT variant has a two-position 550: 147: 126:, so the engine is started by "wind-milling" the propeller in flight. The propeller may be a rigid 2-blade design, or may have more than two blades that fold at the hub when the engine is retracted. The propeller hub is usually attached directly to the crankshaft, but there is at least one example of a sustainer with a belt reduction drive, the DG-1000T. 701:
logbook of the pilot to authorize the launch method, which may be by airplane towing, ground launch (winches, bungee, auto tow), or, in the case of a suitable motor glider, by self-launching. In the US, motor gliders are classified as gliders, and may be operated by a glider pilot without the medical certificate required to operate an airplane.
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on the ground without a wing walker. While some TMGs have only one main wheel, with auxiliary trolley wheels on the wings for taxiing, it is becoming more common to find them being manufactured with tricycle and conventional (two fixed main wheels – i.e. a "tail-dragger") landing gear configurations.
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In Canada, a glider pilot license allows the pilot to fly unpowered gliders. For self-launching motor gliders (including motor gliders and gliders with retractable engines or propellers), and sustainer motor gliders an aeroplane permit or licence is required. An instructor must provide instruction
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Touring motor gliders are seldom used in competition, but they can be useful in training for cross-country flights. After take-off, the engine is switched off, and the trainee flies the aircraft as a glider. Landings in unfamiliar fields can be practiced while the motor idles. If the trainee chooses
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The presence of an engine can increase the safety of gliding, as a powerplant increases the ability of the pilot to avoid storms and off-airport landings. An opposing view is that motor gliders are against the spirit of the sport, and, more importantly, that they sometimes give pilots a false sense
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Gliders without an engine are lighter and, as they do not need a safety margin for an engine-start, they can safely thermal at lower altitudes in weaker conditions. So, pilots in unpowered gliders may complete competition flights when some powered competitors cannot. Conversely, motor glider pilots
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used in motor gliders must have a noise sensor that allows recording the sound level along with position and altitude. In many competitions, the rules require that the pilot start the engine at the beginning of the flight, before starting the task, to ensure an engine start later in the flight will
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Unlike TMGs, most gliders with retractable propellers are also fitted with a tow-hook for aero-towing or ground launch. They have a single-axle retractable main wheel on the fuselage like most unpowered gliders, so they do require assistance during ground operations. The two-stroke engines commonly
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Self-launching engines are equipped with a throttle that allows the engine power to be adjusted for ground operations. Self-launching engines are typically in the range of 50–60 hp (38–45 kW). The higher engine output power requires liquid cooling with a separate radiator mounted on the
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Internal combustion engines can benefit from mounting in the fuselage, rather than on the propeller mast. This allows them to be connected to a larger muffler for reduced noise when operating, something which is mostly relevant to European operation. It also allows the belt tension to be relieved
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Self-launching retractable propeller motor gliders have sufficient thrust and initial climb rate to take off without assistance, or they may be launched as with a conventional glider. The engines also have a starter motor and a large battery to allow the engine to be started on the ground, and an
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In the United States, a private glider pilot certificate allows the pilot to fly unpowered gliders, self-launching motor gliders (including touring motor gliders and gliders with retractable engines or propellers), and sustainer motor gliders. An instructor must provide instruction and sign the
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The engine cannot always be relied upon to start in flight, so the pilot must allow for this possibility. The generally accepted practice is to get in position for landing at a suitable airport, or off-airport out-landing field, before extending the propeller and attempting an engine start. This
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For types that use a pylon, lower drag and sink rate are achieved with the pylon extended and the motor not running, as there is no radiator as required to cool a gasoline engine. For FES systems, the drag from the folded propeller in the nose is negligible if the engine does not start. For safe
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Faster and more reliable transition from gliding to powered flight, as the time and risk required to start and warm up an internal combustion engine is eliminated. For example, the Antares 20E transitions from gliding to powered flight in under 12 seconds. With a FES system maximum power can be
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Most TMGs are designed with engines of 80 to 100 hp (75 kW) and typically cruise (under power) at 85–100 knots (190 km/h). Most have fuel tanks capable of holding between 50 and 100 liters (13 to 26 US gallons) of fuel, giving a range under power of up to 450 nautical miles
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In the United States, a powered glider may be certificated for up to two occupants, up to 850 kg maximum weight, and with a maximum ratio of weight to wing span squared of 3 kg/m. Similar requirements exist in European JAA/EASA regulations, at a maximum weight of 750 kg.
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operation, the "Engine out and not running" performance is used to plan in-air restarts in the event of a problem (even for electrics). The reduced sink-rate of electric-powered motor-gliders "engine out and not running" allows a lower altitude for a safe in-air restart.
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and wing carry-through structure. The fuselage has engine bay doors that open and close automatically, similar to landing gear doors. The engine may be near the top or bottom of the mast, and newer designs have the engine fixed in the fuselage to reduce noise and drag.
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when the engine is retracted to extend the life of the belt and bearings. The drawback of this arrangement is that engines fixed low in fuselages are more difficult to pre-flight and service, and highly stressed power transmission belts should not be bent or twisted.
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For types that use a pylon, belt reduction drive and associated reliability issues are eliminated. As an electric motor can turn at a lower RPM than typical gasoline engines, it can be mounted at the top of the mast without a reduction system, eliminating belt-drive
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The smaller sustainer engines are usually not equipped with a throttle, but instead have a cable to open decompression valves in each cylinder to allow the engine to turn freely for starting. Sustainer engines are typically
514:. The jet engine was mounted inside the fuselage behind the wing, with fixed intake and exhaust ducts coupled to the outside air stream for engine operation. Since then a new generation of jets have been offered for the 589:
can start the engine to extend a flight if conditions will no longer support soaring, while unpowered gliders will have to land out, away from the home airfield, requiring retrieval by road using the glider's trailer.
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used are not efficient at reduced power for level cruising flight, and instead must use a "saw-tooth" flight profile where the glider climbs at full power, then glides with the propeller retracted.
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Gliders with pylon-mounted electric motors are slightly heavier than those with gasoline engines due to the batteries. An FES system weighs about the same as a two-stroke engine.
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Sustainer motor gliders must be launched like an unpowered glider, but can climb slowly to extend a flight once the engine is deployed and started. They generally do not have an
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Increased cost. While electric motors are comparably inexpensive, low-weight batteries suitable for motor-gliders are a little more expensive than gasoline engines.
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or the Phoenix, can also be supplied with interchangeable wings or wingtips so that they can be flown as a standard touring aircraft as well as a TMG.
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In South Africa, Touring Motor Glider (TMG) is an independent National Pilots License category under Recreation Aviation, Part 62, subpart 17.
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Motor with fixed or full feathering propellers are generally classified as Touring Motor Gliders (TMGs). TMGs can take off and cruise like an
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in the range of 18–30 hp (14–22 kW). They are lighter in weight, and simpler to operate than self-launching powerplants.
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In Europe, powered gliders are categorized into gliders with retractable propellers/engines, which can be flown with an ordinary
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self-launching motor glider, with the engine mast extended. A Stemme S10 is in the background with the nose cone extended.
433:. Some types use a pylon behind the cockpit to extend a propeller. 11 different types, from 7 manufacturers, such as the 162:, Germany. Counter-clockwise from top left: propeller hub, mast with belt guide, radiator, Wankel engine, muffler shroud. 1088: 916: 658: 240:. Tow hooks are unnecessary, since aircraft with self-launch ability do not require access to winch or tow plane for 155: 640: 468:
Reduced range or climb altitude, as the energy stored per unit weight for available batteries is less than gasoline.
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of the stopped propeller and landing gear reduces their gliding performance, TMGs are seldom used in competition.
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an inappropriate field, or misjudges the approach, the instructor can apply power and climb away safely.
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performance, not as good as that of unpowered gliders. However TMGs are more efficient than conventional
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alternator to recharge the battery. A two-blade propeller is typically coupled to the engine via a belt
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Greatly reduced noise, allowing take-off from locations where other powered aircraft are not permitted.
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Electric sustainer systems (with power to sustain flight but not self-launch) are optional for the
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on the engine, which allows the aircraft to cruise at altitudes up to 30,000 feet (9,000 m).
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The retractable propeller is usually mounted on a mast that rotates up and forward out of the
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Some TMGs are equipped with folding wings to allow them to fit in standard small airplane
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Disadvantages of current electric powered motor-gliders as compared to gasoline include:
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that offers the advantage of a smaller opening in the fuselage to retract the engine.
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configuration on TMGs usually incorporates two fixed main wheels, allowing it to be
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They are fitted with front-mounted engines, similar to a small airplane. The large
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In 1935, an occasional or auxiliary motor that could be retracted was suggested by
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allows for a safe landing in the event that the engine cannot be started in time.
422: 314: 248: 207: 168: 83: 1067: 577: 381:, a number of electric-powered self-launchers have been developed including the 241: 298: 222: 63: 709:
and sign the logbook of the pilot to authorize the pilot to carry passengers.
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E self-launching motor glider, mounted on a test stand for maintenance at
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that first flew on 8 August of the same year. A later version of the
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equipped with a means of propulsion (MoP), capable of sustained
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The first production self-launching motor glider fitted with a
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are capable of higher speeds and longer range under power.
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flight without thrust from the means of propulsion.
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Other self-launching types include the experimental
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Advantages of electric power over gasoline include:
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that can be flown with or without engine power. The
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Index

Self-launching sailplane
Glider (sailplane)

fixed-wing aircraft
FAI Gliding Commission
aerodyne
soaring

Sir John Carden
Carden-Baynes Auxiliary
Budig glider
propeller
AMS-Flight Carat
alternator
starter motor
two-stroke
air-cooled engines

Schleicher ASH 26
Alexander Schleicher
Poppenhausen
reduction drive
single-blade propeller
two-stroke piston engines
Wankel rotary engines
airplane
glider
wingspans
gliding
light aircraft

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