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payload-structure-fuel ratio

Толкование Перевод

1 payload-structure-fuel ratio

Космонавтика: соотношение весов полезной нагрузки, конструкции и топлива

Универсальный англо-русский словарь > payload-structure-fuel ratio
2 payload-structure-fuel ratio

соотношение весов полезной нагрузки, конструкции и топлива (ЛА)

Englsh-Russian aviation and space dictionary > payload-structure-fuel ratio
3 payload-structure-fuel weight ratio

< aerospace> ■ Nutzlast-Aufbau-Kraftstoff-Verhältnis n

English-german technical dictionary > payload-structure-fuel weight ratio
4 ratio

отношение, соотношение, пропорция; степень; коэффициент, см. тж. coefficient; передаточное число [отношение]

all-out level/stalling speed ratio — относительный диапазон скоростей полёта (отношение максимальной скорости горизонтального полёта к скорости сваливания)

base(-altltude, -height) ratio — отношение величины базиса фотографирования к высоте

best power mixture ratio — качество смеси для режима оптимальной мощности

burning (surface)-to-throat (area) ratio — отношение поверхности горения к площади критического сечения сопла (в РДТТ)

chamber volume-to-throat area ratio — приведенная [характеристическая] длина камеры сгорания

critical fiber length-to-diameter ratio — критическое относительное удлинение волокна

envelope-bulk to weight ratio — отношение объёма, занимаемого двигателем, к его сухому весу

exhaust nozzle area ratio — степень уширения или сужения выхлопного сопла

lift-(over, to-)drag ratio — аэродинамическое качество

main rotor/engine r.p.m. ratio — степень редукции между двигателем, и несущим винтом, соотношение чисел оборотов несущего винта и вала двигателя

maintenance (man hours)-to-flight (hours) ratio — соотношение объёма работ по наземному обслуживанию (в человеко-часах) и налёта

mixing ratio of moist air — метео. влагосодержаиие

port(-to-)throat ratio — относительная свободная площадь (отношение свободной площади к площади критического сечения сопла)

ratio of specific heats — отношение удельных теплоёмкостей, показатель адиабаты

solid-propel lant mixture ratio — соотношение компонентов твёрдого ракетного топлива

stoichiometric (equivalence, mixture) ratio — стехиометрическое соотношение компонентов топлива, стехиометрический коэффициент состава топлива

vertical tail area ratio — относительная площадь вертикального оперения

— advance ratio

— advance-diameter ratio

— aileron-span ratio

— air density ratio

— airframe-to-fuel weight ratio

— air-to-fuel ratio

— area ratio

— area-moment ratio

— aspect ratio

— augmented thrust ratio

— average mixture ratio

— best glide ratio

— best lift/drag ratio

— blade-width ratio

— boost ratio

— bore-stroke ratio

— boss ratio

— bypass ratio ten

— bypass ratio

— California bearing ratio

— chamber-area ratio

— chamber-to-throat area ratio

— charge-to-mass ratio

— charge-to-weight ratio

— charge-weight ratio

— chemically-correct mixture ratio

— combat loss ratio

— compression ratio

— compressive strength-weight ratio

— compressor pressure ratio

— contraction ratio

— control gear ratio

— control-to-wing area ratio

— convergence ratio

— critical pressure ratio

— cruise pressure ratio

— density ratio

— design mixture ratio

— deviation ratio

— diffuser area ratio

— disc flow ratio

— divergence ratio

— drag-to-lift ratio

— drag-weight ratio

— effective aspect ratio

— ellipticity ratio

— endurance ratio

— engine pressure ratio

— equivalence ratio

— erosion ratio

— exit pressure ratio

— expansion ratio

— extreme mixture ratio

— fan compression ratio

— fan pressure ratio

— fatigue-strength-to-density ratio

— feed-back ratio

— fineness ratio

— finite pressure ratio

— flight mixture ratio

— frequency ratio

— front-to-back ratio

— fuel-air equivalence ratio

— fuel-structure ratio

— fuel-to-airframe ratio

— fuel-to-oxldlzer ratio

— fuel-to-tank ratio

— fuel-weight ratio

— gas-generator mixture ratio

— gearing ratio

— geometric aspect ratio

— glide ratio

— high-fineness ratio

— horizontal-tail volume ratio

— humidity mixing ratio

— hydraulic mixture ratio

— hypersonic density ratio

— hypersonic Hft-to-drag ratio

— I/W ratio

— impulse-to-volume ratio

— impulse-to-weight ratio

— inflow ratio

— inlet compression ratio

— instantaneous mixture ratio

— internal area ratio

— kill ratio

— L/D ratio

— launch success ratio

— length-diameter ratio

— length-to-beam ratio

— length-to-web ratio

— linkage ratio

— load ratio

— local mixture ratio

— mass ratio

— mass-to-drag ratio

— mean mixture ratio

— mechanical advantage ratio

— metal parts-weight ratio

— missile length-diameter ratio

— missile mass ratio

— missile-to-target speed ratio

— mixing ratio

— mixture ratio

— modulus-to-density ratio

— modulus-to-weight ratio

— nozzle area ratio

— nozzle ratio

— nozzle-contraction area ratio

— nozzle-expansion area ratio

— off-mixture ratio

— offset ratio

— operating mixture ratio

— optimum expansion ratio

— optimum mixture ratio

— optimum stage-weight ratio

— over-all impulse-to-weight ratio

— over-all mixture ratio

— over-all payload ratio

— oxidant-to-fuel ratio

— oxidizer-to-fuel ratio

— oxigen-nitrogen mixture ratio

— panel taper ratio

— payloadratio

— payload-stage length ratio

— payload-structure-fuel ratio

— payload-structure-propellant weight ratio

— payload-to-launch ratio

— pedal-to-rudder gear ratio

— pitch ratio

— pitch-damping ratio

— power-plant mixture ratio

— power-to-weight ratio

— preselected mixture ratio

— pressure ratio

— primary mixture ratio

— progressivity ratio

— propellant loaded ratio

— propellant loading ratio

— propellant mixture ratio

— propellant ratio ratio

— propellant utilization ratio

— propellant-to-engine weight ratio

— propellant-weight ratio

— propeller solidity ratio

— ratio of inertias

— ratio of propellants

— reactant ratio

— reinforcement-to-matrix ratio

— restorability ratio

— roll/yaw ratio

— roll-damping ratio

— roll-to-sideslip ratio

— rotor solidity ratio

— semispan-length ratio

— servo gear ratio

— shutdown mixture ratio

— signal-to-noise ratio

— slenderness ratio

— slip ratio

— solidity ratio

— span ratio

— specific heat ratio

— speed ratio

— stage mass ratio

— stage-weight ratio

— starting mixture ratio

— static gearing ratio

— static mixture ratio

— stick gear ratio

— stick-stabilizer travel ratio

— stiffness/weight ratio

— strength-to-density ratio

— strength-to-weight ratio

— structural ratio

— structure/weight ratio

— structure-to-fuel weight ratio

— subsonic lift-to-drag ratio

— supercharger compression ratio

— supersonic lift-to-drag ratio

— surface-to-port area ratio

— system impulse-to-welght ratio

— system mixture ratio

— T/W ratio

— tail taper ratio

— tail volume ratio

— tail-area ratio

— takeoff pressure ratio

— taper ratio

— temperature ratio

— theoretical mixture ratio

— thermal diffusion ratio

— thickness-to-chord ratio

— throat-to-port area ratio

— thrust ratio

— thrust-chamber mixture ratio

— thrust-to-area ratio

— thrust-to-drag ratio

— thrust-to-weight ratio

— tip-speed ratio

— total mixture ratio

— total propeller-width ratio

— - to-thrust ratio

— transfer ratio

— ultimate tensile-stress-to-density ratio

— unpowered glide ratio

— variable gearing ratio

— vehicle lift-drag ratio

— velocity ratio

— vertical thrust/weight ratio

— vertical-tail-volume ratio

— volume O/F ratio

— volumetric ratio

— weight O/F ratio

— weight ratio

— weight-to-power ratio

— welght-to-payload ratio

— wheel gear ratio

— wing thickness-to-chord ratio

— yaw-damping ratio

Englsh-Russian aviation and space dictionary > ratio

См. также в других словарях:

Payload (air and space craft) — In military aircraft or space exploration, the payload is the carrying capacity of an aircraft or space ship, including as cargo, munitions, scientific instruments or experiments. External fuel, when optionally carried, is also considered part of … Wikipedia
Thrust-to-weight ratio — is, as its name suggests, the ratio of instantaneous thrust to weight (where weight means weight at the Earth’s surfaceSutton (7th edition pg 442) thrust to weight ratio F/Wg is a dimensionless parameter that is identical to the acceleration of… … Wikipedia
Rocket — This article is about vehicles powered by rocket engines. For other uses, see Rocket (disambiguation). A Soyuz U, at Baikonur Site 1/5 A rocket is a missile, spacecraft, aircraft or other vehicle which obtains thrust from a rocket engi … Wikipedia
Single-stage-to-orbit — The VentureStar was a proposed SSTO spaceplane. A single stage to orbit (or SSTO) vehicle reaches orbit from the surface of a body without jettisoning hardware, expending only propellants and fluids. The term usually, but not exclusively, refers… … Wikipedia
Space Shuttle — STS redirects here. For other uses, see STS (disambiguation). This article is about the NASA Space Transportation System vehicle. For the associated NASA STS program, see Space Shuttle program. For other shuttles and aerospace vehicles, see… … Wikipedia
Mathematics and Physical Sciences — ▪ 2003 Introduction Mathematics Mathematics in 2002 was marked by two discoveries in number theory. The first may have practical implications; the second satisfied a 150 year old curiosity. Computer scientist Manindra Agrawal of the… … Universalium
Scramjet — Part of a series on Aircraft propulsion Shaft engines (to drive pr … Wikipedia
Non-rocket spacelaunch — Non rocket space launch (NRS) is a launch into space where some or all needed speed and altitude is provided by non rocket means, rather than simply using conventional chemical rockets from the ground. A number of alternatives to rockets have… … Wikipedia
Spacecraft propulsion — A remote camera captures a close up view of a Space Shuttle Main Engine during a test firing at the John C. Stennis Space Center in Hancock County, Mississippi Spacecraft propulsion is any method used to accelerate spacecraft and artificial… … Wikipedia
Physical Sciences — ▪ 2009 Introduction Scientists discovered a new family of superconducting materials and obtained unique images of individual hydrogen atoms and of a multiple exoplanet system. Europe completed the Large Hadron Collider, and China and India took… … Universalium
Rocket engine — RS 68 being tested at NASA s Stennis Space Center. The nearly transparent exhaust is due to this engine s exhaust being mostly superheated steam (water vapor from its propellants, hydrogen and oxygen) … Wikipedia

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