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1 unstable missile
Космонавтика: неустойчивая в полёте ракета, неустойчивая ракета -
2 unstable missile
неустойчивая ( в полете) ракетаEnglsh-Russian aviation and space dictionary > unstable missile
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3 unstable missile
adj нестійка в польоті ракета -
4 longitudinally-unstable missile
Универсальный англо-русский словарь > longitudinally-unstable missile
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5 longitudinally unstable missile
? повздовжньо нестійка ракетаEnglish-Ukrainian military dictionary > longitudinally unstable missile
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6 missile
ракета; реактивный снаряд, см. тж. rocketatomic(-armed, -capable, -equipped, -tipped) missile — ракета с ядерной боевой частью
delayed impact space missile — орбитальная [космическая] ракета с запрограммированным по времени отделением головной или боевой части
ECM carrying missile — ракета радиопротиводействия, ракета — постановщик помех; противорадиолокационная ракета
infrared(-guided, -homing) missile — ракета с тепловой головкой самонаведения
land-based(-borne, -launched) missile — ракета, запускаемая с земли, ракета наземного базирования
liquid(-fuel, -fueled, -propellant) missile — ракета с ЖРД, жидкостная ракета
lock a missile on the target — наводить ракету на цель; захватывать цель головкой самонаведения ракеты
nuclear(-armed, -capability) missile — ракета с ядерной боевой частью
place missile on target — накрывать [поражать] цель ракетой
production(-line, -type) missile — серийная ракета, ракета серийного образца
rocket(-powered, -propelled) missile — ракета
solid(-fueled, -propellant) missile — твердотопливная ракета, ракета с РДТТ
trigger off a missile — производить пуск ракеты; подрывать ракету или боевую часть ракеты
warm up the missile — подготавливать ракету к пуску; прогревать аппаратуру ракеты
— - ship missile -
7 aircraft
воздушное судно [суда], атмосферный летательный аппарат [аппараты]; самолёт (ы) ; вертолёты); авиация; авиационный; см. тж. airplane, boostaircraft in the barrier — самолёт, задержанный аварийной (аэродромной) тормозной установкой
aircraft off the line — новый [только что построенный] ЛА
B through F aircraft — самолёты модификаций B, C, D, E и F
carrier(-based, -borne) aircraft — палубный ЛА; авианосная авиация
conventional takeoff and landing aircraft — самолёт с обычными взлетом и посадкой (в отличие от укороченного или вертикального)
keep the aircraft (headed) straight — выдерживать направление полёта ЛА (при выполнении маневра); сохранять прямолинейный полет ЛА
keep the aircraft stalled — сохранять режим срыва [сваливания] самолёта, оставлять самолёт в режиме срыва [сваливания]
nearly wing borne aircraft — верт. ЛА в конце режима перехода к горизонтальному полёту
pull the aircraft off the deck — разг. отрывать ЛА от земли (при взлете)
put the aircraft nose-up — переводить [вводить] ЛА на кабрирование [в режим кабрирования]
put the aircraft through its paces — определять предельные возможности ЛА, «выжимать все из ЛА»
reduced takeoff and landing aircraft — самолёт укороченного взлета и посадки (с укороченным разбегом и пробегом)
rocket(-powered, -propelled) aircraft — ракетный ЛА, ЛА с ракетным двигателем
roll the aircraft into a bank — вводить ЛА в крен, накренять ЛА
rotate the aircraft into the climb — увеличивать угол тангажа ЛА для перехода к набору высоты, переводить ЛА в набор высоты
short takeoff and landing aircraft — самолёт короткого взлета и посадки (с коротким разбегом и пробегом)
single vertical tail aircraft — ЛА с одинарным [центральным] вертикальным оперением
strategic(-mission, -purpose) aircraft — ЛА стратегического назначения; стратегический самолёт
take the aircraft throughout its entire envelope — пилотировать ЛА во всем диапазоне полётных режимов
trim the aircraft to fly hands-and-feet off — балансировать самолёт для полёта с брошенным управлением [с брошенными ручкой и педалями]
turbofan(-engined, -powered) aircraft — ЛА с турбовентиляторными двигателями, ЛА с ТРДД
turbojet(-powered, -propelled) aircraft — ЛА с ТРД
undergraduate navigator training aircraft — учебно-тренировочный самолёт для повышенной лётной подготовки штурманов
water(-based, takeoff and landing) aircraft — гидросамолёт
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8 configuration
1. конфигурация; схема; компоновка; форма; комбинация2. структура3. вариант <ЛА>10x8 configuration15% unstable configurationactuator configurationaero-balanced configurationaeroelastic configurationaeromedical configurationaft CG configurationair defence configurationair-combat configurationair-to-air configurationaircraft configurationaircraft-like configurationairfoil-spoiler-flap configurationairframe-inlet configurationall-cargo configurationall-economy configurationall-freight configurationall-wing configurationanti-ice configurationapproach-flap configurationarrow-wing configurationas delivered configurationas-built configurationasymmetrical missile configurationback-staggered configurationbaseline configurationbenchmark configurationblade configurationblade/hub configurationblowing configurationbroad-brush configurationbutterfly configurationcabin configurationcanard configurationcanard-tail configurationcanard-wing configurationcanard-wing-body configurationcanardless configurationcargo-loading configurationchine configurationchined configurationcircular configurationclean configurationclose-coupled canard configurationclose-coupled wing-canard configurationclosed-loop configurationcoaxial configurationcockpit configurationconstant gain configurationcontrol configurationcontrol law configurationcontrol surface configurationcontrol system configurationcritical configurationcruise configurationdelta-canard configurationdelta-winged configurationdeparture resistant configurationdeployed configurationdisplay configurationdouble-delta configurationdownstop configurationdual cargo-hook configurationdual-console configurationeconomy class configurationejector-lift and vectored-thrust configurationelectronic reconnaissance configurationempennage configurationenergy-conservative configurationengine configurationevaluation configurationfairing configurationfighter-like configurationfilter configurationfinned configurationflap configurationflapped configurationflaps-up configurationflying boom configurationforebody configurationforebody off configurationforebody removed configurationforward-swept configurationforward-swept-wing configurationfour-blade configurationfour-engine configurationfree-turbine configurationgeometric configurationglide configurationglove-fuselage configurationgo-around configurationheavy store configurationhigh-angle-of-attack configurationhigh-control-effectiveness configurationhigh-altitude configurationhigh-density configurationhigh-fineness-ratio configurationhigh-lift configurationhigh-overshoot configurationhigh-wing configurationhorizontal ellipse configurationhypersonic configurationin-flight configurationin-line configurationinboard-jointed configurationinertially slender configurationinlet configurationinversely derived configurationiron bird configurationjet balanced configurationjoined wing configurationlanding configurationLEX configurationlifting body configurationlighting configurationlow-bypass configurationlow-drag configurationlow-fineness-ratio configurationlow-overshoot configurationlow-signature configurationlow-speed configurationmaneuver configurationmidwing configurationminimum drag configurationmixed-class configurationmultisurface configurationmultibody configurationmultiengine configurationmultiple-jet configurationnormal-shock configurationnose-boom-off configurationnose-boom-on configurationoblique-wing configurationopen-loop configurationordnance configurationover-the-wing configurationpanelized configurationparcel-freighter configurationpartial-freight configurationpassenger configurationpayload configurationpitch control configurationpitch attitude-tracking configurationpitch-only configurationpitch rate command configurationpodded configurationpole-zero configurationpoor RSS configurationpower approach configurationpower-on aircraft configurationpowered configurationpowerplant configurationpre-production configurationproduction configurationpropulsor configurationpusher configurationratchet configurationreal configurationrear-loading configurationrotor plus wing configurationrotor-airframe configurationrotor-fuselage configurationrotor-winglet configurationrotorcraft configurationseating configurationsensor configurationside-by-side configurationsimulation configurationsingle-jet configurationsingle-body configurationsingle-engine configurationsingle-fuselage configurationsingle-pilot configurationsingle-rotor configurationsingle-shaft configurationsized configurationslat configurationsoft in-plane configurationspoiler configurationstable configurationstall-resistant configurationstarting configurationsteady flight configurationstiff in-plane configurationSTOL configurationstore configurationSTOVL configurationstraight-wing configurationstrake off configurationstrake-wing configurationsupersonic cruise configurationsymmetrical missile configurationT-tail configurationtail configurationtail control configurationtail-aft configurationtailed configurationtailed-delta configurationtailless configurationtakeoff configurationtandem configurationtandem-wing configurationtandem-rotor configurationtest configurationthree shaft configurationthree-engine configurationthree-shock configurationthrust-down configurationthrust-up configurationthrust-vectored configurationtilt-rotor configurationtilting engine configurationtip-jointed configurationtractor configurationtrailing-edge configurationTrefftz-plane configurationtunnel-supported configurationturbojet-powered configurationturboprop configurationturboshaft configurationturning configurationtwin-lift helicopter configurationtwo-bladed configurationtwo-cabin configurationtwo-engine configurationtwo-shaft configurationtwo-stage configurationtwo-surface configurationunder-the-wing configurationunslatted configurationunstable configurationunstick configurationup and away configurationupper-surface-blowing configurationupper-surface-blown configurationUSB configurationV/STOL configurationvariable-bypass-ratio configurationvariable-geometry configurationVATOL configurationvectored-engine-over-wing configurationVEO-wing configurationvertical ellipse configurationVTOL configurationwidely spaced pod configurationWild Weasel configurationwing configurationwing mounted configurationwing-body-nacelle configurationwing-body-tail configurationwing-canard configurationwing-fence configurationwing-flap configurationwing-spoiler-flap configurationwing-tail-fuselage configurationwing-store configurationyaw vane configurationzig-zag configuration -
9 length
длина; протяжение; отрезок -
10 area
площадь; участок; пространство; область, район, зона; поверхность"gold-plated" area of instrument panel — наиболее легко обозреваемый (лётчиком) участок приборной доски
area of high pressure — метео. область высокого давления, антициклон
area of low pressure — метео. область низкого давления, циклон
assembly and test area — ркт. сборочно-проверочная площадка
booster (engine) disposal area — район сброса [падения] стартовых двигателей [ускорителей]
booster (engine) impact area — район сброса [падения] стартовых двигателей [ускорителей]
disc area of main rotor — верт. площадь диска несущего винта
exhaust jet area — площадь выходного сечения сопла; площадь сечения струи истекающих газов
floor area between the ramps — площадь пола грузовой кабины между (передним и задним) грузовыми трапами
guidance and control area — ркт. площадка управления пуском и наведением
— fin area— VFR area -
11 body
тело; корпус; основная часть; фюзеляж; светило, небесное телоbody of the report — основная часть отчёта [донесения]
sonic boom overpressure body — тело или ЛА — генератор звукового удара
— MHD body— tip body -
12 position
положение; место ЛА; рабочее место ( члена экипажа) ; позиция; устанавливать в ( требуемое) положение1/2 position — положение, соответствующее выпуску закрылков наполовину
20-deg. sweep position — положение (крыла) с углом стреловидности 20°
actual dead reckoning position — действительные координаты счислимой точки (в отличие от приближенных)
air inlet spike position — положение «иглы» [конуса] воздухозаборника
air intake spike position — положение «иглы» [конуса] воздухозаборника
feel device no-load position — положение автомата загрузки, соответствующее нулевому усилию на рычагах управления, сбалансированное положение автомата загрузки
flip to inverted position — мгновенно переворачиваться «на спину» (о самолёте)
hold in the central position — удерживать (рули) в нейтрали [в нейтральном положении]
in a 60-deg. reclining position — в отклонённом назад под углом 60° положении (о лётчике)
in the No 2 engine position — на месте двигателя № 2
minimum afterburner throttle position — положение РУД, соответствующее минимальной форсажной тяге
position position of minimum reception — положение минимального приёма (приёма сигналов с наименьшей слышимостью)
primary flight instrument positions — места расположения [позиции] основных пилотажных приборов
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13 propellant
ракетное топливо; реактивное топливоaniline red fuming nitric acid propellant — ракетное топливо, состоящее из анилина и красной дымящей азотной кислоты
condensation colloid propellant for electrostatic propulsion — конденсационное коллоидное ракетное топливо для ионных ракетных двигателей
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14 Bode, Hendrik Wade
[br]b. 24 December 1905 Madison, Wisconsin, USAd. 21 June 1982 Cambridge, Massachusetts, USA[br]American engineer who developed an extensive theoretical understanding of the behaviour of electronic circuits.[br]Bode received his bachelor's and master's degrees from Ohio State University in 1924 and 1926, respectively, and his PhD from Columbia University, New York, in 1935. In 1926 he joined the Bell Telephone Laboratories, where he made many theoretical contributions to the understanding of the behaviour of electronic circuits and, in particular, in conjunction with Harry Nyquist, of the conditions under which amplifier circuits become unstable.During the Second World War he worked on the design of gun control systems and afterwards was a member of a team that worked with Douglas Aircraft to develop the Nike anti-aircraft missile. A member of the Bell Laboratories Mathematical Research Group from 1929, he became its Director in 1952, and then Director of Physical Sciences. Finally he became Vice-President of the Laboratories, with responsibility for systems engineering, and a director of Bellcomm, a Bell company involved in the Moon-landing programme. When he retired from Bell in 1967, he became Professor of Systems Engineering at Harvard University.[br]Principal Honours and DistinctionsPresidential Certificate of Merit 1946. Institute of Electrical and Electronics Engineers Edison Medal 1969.Bibliography1940, "Relation between attenuation and phase in feedback amplifier design", Bell System Technical Journal 19:421.1945, Network Analysis and Feedback Amplifier Design, New York: Van Nostrand.1950, with C.E.Shannon, "A simplified derivation of linear least squares smoothing and prediction theory", Proceedings of the Institute of Radio Engineers 38:417.1961, "Feedback. The history of an idea", Proceedings of the Symposium on Active Networks and Feedback Systems, Brooklyn Polytechnic.1971, Synergy: Technical Integration and Technical Innovation in the Bell System Bell Laboratories, Bell Telephone Laboratories (provides background on his activities at Bell).Further ReadingP.C.Mahon, 1975, Mission Communications, Bell Telephone Laboratories. See also Black, Harold Stephen; Shannon, Claude Elwood.KF
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