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tail rotor<br />

zontal tail, to increase system capacity and, esp., to<br />

control longitudinal trim without drag.<br />

tail rotor Helicopter anti-torque rotor, rotating at tail<br />

about more or less horizontal axis. Not used for rear<br />

tandem rotor.<br />

tailscrape See tailstrike.<br />

tail setting angle The acute angle between chord lines of<br />

wing and tailplane (1).<br />

tailsitter VTOL aerodyne whose fuselage is approximately<br />

perpendicular at takeoff, in hovering mode and at<br />

landing, today preferably called Vatol.<br />

tailskid Projection, usually a sprung lever with endshoe,<br />

supporting tail of aerodyne on ground, esp. one<br />

whose c.g. is well aft of main landing gear.<br />

tailskid shoe Replaceable pad on end of tailskid which<br />

slides on ground.<br />

tailslide Transient flight condition of fixed-wing aerodyne<br />

in which relative wind is from astern, eg in stall from<br />

near-vertical climbing attitude.<br />

tailspin Spin (arch.).<br />

tailstander Tailsitter.<br />

tailstrike Scraping rear fuselage on runway on rotation.<br />

Hence, * indicator, frangible foil which causes a bright<br />

flash on EICAS.<br />

tailstrike protection Any of several systems which<br />

prevent a tailstrike, usually by limiting authority of horizontal<br />

tail.<br />

tail surface Any aerofoil forming part of tail (2).<br />

tail turret Defensive gun turret, usually power-driven,<br />

forming the tail end of the fuselage, today becoming rare.<br />

tail undercarriage Rearmost unit of tailwheel-type<br />

landing gear (rare, suggest arch.).<br />

tail unit Complete tail (2) of horizontal, vertical and/or<br />

canted surfaces, often including ventral fins or strakes.<br />

Also called empennage.<br />

tail-up procedure Final closure of production at end of<br />

need for spares or support.<br />

tail view Tail-on view showing object from directly<br />

astern; not normal aspect for layout drawing.<br />

tail volume See V¯¯.<br />

tailwagging 1 Lateral flexure of fuselage.<br />

2 Flat turns, esp. to steepen glide.<br />

tail warning radar Aft-facing radar, usually of active<br />

type, intended to detect other aircraft (and possibly<br />

SAMs) intercepting from behind.<br />

tailwheel 1 Rear wheel of * type landing gear, supporting<br />

tail on ground.<br />

2 Auxiliary wheel under tail of aircraft with nosewheeltype<br />

landing gear (eg Albemarle); fitted in place of tail<br />

bumper.<br />

tailwheel landing gear Landing gear comprising<br />

left/right main units ahead of c.g. and tailwheel at rear.<br />

tailwind Wind blowing approximately from astern of<br />

aircraft and thus increasing groundspeed.<br />

TAIMS Three-axis inertial measurement system.<br />

TAINS, Tains Tercom and, or Tercom-aided, inertial<br />

navigation system.<br />

TAIR Terminal-area instrumentation radar.<br />

TAIRCW Tactical air control wing.<br />

TAIS 1 Tactical air intelligence systems.<br />

2 Technology application information system (SDI).<br />

3 Tactical airspace integration system.<br />

4 Thermal active intervention system.<br />

Take 5 Traffic crossing airway must maintain<br />

takeoff thrust<br />

prescribed separation of 5 nm horizontally and 5,000 ft<br />

vertically from any GAT track in airway.<br />

takeoff 1 Procedure in which aerodyne becomes<br />

airborne; not normally used for launch of glider (except<br />

on aerotow) or high-acceleration launch of missile or<br />

RPV, and never for any ballistic vertical-liftoff vehicle. In<br />

author’s opinion verb is best as two words, noun and<br />

adjective as single word without hyphen.<br />

2 Moment or place at which aerodyne leaves ground or<br />

water.<br />

3 Net flightpath from brakes-release to screen height.<br />

4 Power * for extraction of shaft power.<br />

take off To perform a takeoff.<br />

takeoff boost Boost pressure permitted for takeoff,<br />

usually 2 minute limit.<br />

takeoff cone Airspace occupied by aircraft in first<br />

minutes of flight.<br />

takeoff distance, TOD Field length measured from<br />

brake-release to reference zero (at screen); can be longer<br />

than runway and extreme limit TOD a = entire runway +<br />

stopway + clearway = TOR a × 1.5. For multi-engine aeroplanes<br />

usually factored according to number of operative<br />

engines, thus TOD 4 or TOD 3 . TOD 1 = TOD required for<br />

particular aircraft and WAT, not normally to exceed 0.87<br />

TOD a .<br />

takeoff distance available Actual distance at particular<br />

time, not necessarily length of runway.<br />

takeoff distance ratio TOD into wind divided by TOD<br />

downwind [with tailwind], usually expressed as<br />

percentage.<br />

takeoff/liftoff area Heliport area, a square with side<br />

equal to main-rotor diameter (FAA).<br />

takeoff limit No general meaning.<br />

takeoff mass Not normal term; for rocket or space<br />

launcher usually liftoff mass or launch mass.<br />

takeoff noise Measured on extended runway centreline<br />

3.5 nm (strictly 6,485.5 m, but taken as 6.5 km) from<br />

brakes-release. A second reference point, not used for<br />

certification, is at side or runway opposite supposed start<br />

of run 1 nm from centreline.<br />

takeoff power Power authorized for piston engine or<br />

turboprop for takeoff, usually 2½-minute rating for<br />

turbine engines. In case of turboshaft, a lower rating than<br />

2½-minute contingency.<br />

takeoff rating 1 Boost/manifold pressure/rpm figures<br />

authorized for piston engine at takeoff.<br />

2 Thrust published for turbojet or turbofan at takeoff,<br />

normally achieved by engine control system rather than<br />

set directly by pilot, and subject to ATR or FTO techniques.<br />

takeoff rocket See rocket-assisted takeoff.<br />

takeoff run 1 Loosely, distance travelled over land or<br />

water in aeroplane or aerotow-glider takeoff to point of<br />

becoming airborne.<br />

2 TOR, field length measured from brake-release to end<br />

of ground run plus one-third of airborne distance to<br />

screen height. TOR a = TOR available = length of runway;<br />

TOR 4 , TOR 3 are factored for engine-out cases, and TOR r<br />

= TOR required.<br />

takeoff safety speed V 2 , lowest speed at which aeroplane<br />

complies with required handling criteria for climb-out<br />

following engine failure at takeoff.<br />

takeoff speed Not defined but loosely = unstick speed.<br />

takeoff thrust Takeoff rating (2).<br />

681

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