Glossary of aerospace engineering

Most of the terms listed in Wikipedia glossaries are already defined and explained within Wikipedia itself. However, glossaries like this one are useful for looking up, comparing and reviewing large numbers of terms together. You can help enhance this page by adding new terms or writing definitions for existing ones.

This glossary of aerospace engineering terms pertains specifically to aerospace engineering and its sub-disciplines. For a broad overview of engineering, see glossary of engineering.

Part of a series on
Science
Formal Formal logic Mathematics Mathematical statistics Theoretical computer science Game theory Decision theory Actuarial science Information theory Systems theory Control theory
Physical Physics Classical Modern Applied Theoretical Experimental Computational Mechanics (classical analytical continuum fluid solid) Electromagnetism Thermodynamics Molecular Atomic Nuclear Particle Condensed matter Plasma Quantum mechanics (introduction) Quantum field theory Special relativity General relativity String theory Chemistry Inorganic Organic Analytical Physical Acid-base Supramolecular Solid-state Nuclear Environmental Sustainable ("green") Theoretical Astrochemistry Biochemistry Crystallography Food chemistry Geochemistry Materials science Photochemistry Radiochemistry Stereochemistry Surface science Earth science Climatology Edaphology Environmental science Geodesy Geography (physical) Geology Geomorphology Geophysics Glaciology Hydrology Limnology Meteorology Mineralogy Oceanography Paleoclimatology Paleoecology Palynology Pedology Volcanology Astronomy Astrophysics Cosmology Galactic astronomy Planetary geology Planetary science Stellar astronomy
Life Biology Anatomy Astrobiology Biochemistry Biogeography Biological engineering Biomechanics Biophysics Biotechnology Botany Cell biology Conservation biology Cryobiology Developmental biology Ecology Ethology Evolutionary biology (introduction) Genetics (introduction) Immunology Microbiology Molecular anthropology Molecular biology Nanobiology Neuroscience Paleontology Parasitology Physiology Quantum biology Theoretical biology Toxicology Zoology
Social Anthropology Archaeology Criminology Demography Economics Geography (human) History International relations Jurisprudence Linguistics Pedagogy Political science Psychology Sociology
Applied Engineering Aerospace Agricultural Applied physics Biological Biomedical Chemical Civil Computer science / engineering Electrical Fire protection Genetic Industrial Information Mechanical Military Mining Nuclear Operations research Robotics Software Web Healthcare Medicine Veterinary Dentistry Midwifery Epidemiology Pharmacy Nursing
Interdisciplinary Artificial intelligence Bioethics Bioinformatics Biostatistics Cognitive science Complex systems Computational linguistics Cultural studies Cybernetics Environmental science Environmental social science Environmental studies Ethnic studies Evolutionary psychology Forensics Forestry Library science Mathematical / theoretical biology Mathematical physics Military science Network science Neural engineering Science studies Scientific modelling Semiotics Sociobiology Statistics Systems science Urban planning Web science
Philosophy History Basic research Citizen science Fringe science Protoscience Pseudoscience Freedom Policy Funding Method Sociology Technoscience
Glossaries of science and engineering Aerospace engineering Archaeology Architecture Artificial intelligence Astronomy Biology Botany Calculus Chemistry Civil engineering Clinical research Computer science Ecology Economics Electrical and electronics engineering Engineering Entomology Environmental science Genetics Geography Geology Machine vision Mechanical engineering Medicine Meteoritics Meteorology Physics Probability and statistics Robotics Speciation Structural engineering
Outline Portal Category

A

• Above ground level — In aviation, atmospheric sciences and broadcasting, a height above ground level (AGL) is a height measured with respect to the underlying ground surface. This is as opposed to altitude/elevation above mean sea level (AMSL), or (in broadcast engineering) height above average terrain (HAAT). In other words, these expressions (AGL, AMSL, HAAT) indicate where the "zero level" or "reference altitude" is located.
• Absolute humidity — describes the water content of air and is expressed in either grams per cubic meter or grams per kilogram.
• Absolute value — In mathematics, the absolute value or modulus |x| of a real number x is the non-negative value of x without regard to its sign. Namely, |x| = x for a positive x, |x| = −x for a negative x (in which case −x is positive), and |0| = 0. For example, the absolute value of 3 is 3, and the absolute value of −3 is also 3. The absolute value of a number may be thought of as its distance from zero.
• Acceleration — In physics, acceleration is the rate of change of velocity of an object with respect to time. An object's acceleration is the net result of any and all forces acting on the object, as described by Newton's Second Law. The SI unit for acceleration is metre per second squared (m s⁻²). Accelerations are vector quantities (they have magnitude and direction) and add according to the parallelogram law. As a vector, the calculated net force is equal to the product of the object's mass (a scalar quantity) and its acceleration.
• Acquisition of signal — A pass, in spaceflight and satellite communications, is the period in which a satellite or other spacecraft is above the local horizon and available for radio communication with a particular ground station, satellite receiver, or relay satellite (or, in some cases, for visual sighting). The beginning of a pass is termed acquisition of signal; the end of a pass is termed loss of signal. The point at which a spacecraft comes closest to a ground observer is the time of closest approach.
• Action — In physics, action is an attribute of the dynamics of a physical system from which the equations of motion of the system can be derived. It is a mathematical functional which takes the trajectory, also called path or history, of the system as its argument and has a real number as its result. Generally, the action takes different values for different paths. Action has the dimensions of [energy]⋅[time] or [momentum]⋅[length], and its SI unit is joule-second.
• ADF —Automatic direction finder
• Advanced Space Vision System — The Advanced Space Vision System (also known as the Space Vision System or by its acronym SVS) is a computer vision system designed primarily for International Space Station (ISS) assembly. The system uses regular 2D cameras in the Space Shuttle bay, on the Canadarm, or on the ISS along with cooperative targets to calculate the 3D position of an object.
• Aeroacoustics — Is a branch of acoustics that studies noise generation via either turbulent fluid motion or aerodynamic forces interacting with surfaces. Noise generation can also be associated with periodically varying flows. A notable example of this phenomenon is the Aeolian tones produced by wind blowing over fixed objects.
• Aerobraking — is a spaceflight maneuver that reduces the high point of an elliptical orbit (apoapsis) by flying the vehicle through the atmosphere at the low point of the orbit (periapsis). The resulting drag slows the spacecraft. Aerobraking is used when a spacecraft requires a low orbit after arriving at a body with an atmosphere, and it requires less fuel than does the direct use of a rocket engine.
• Aerocapture — is an orbital transfer maneuver used to reduce the velocity of a spacecraft from a hyperbolic trajectory to an elliptical orbit around the targeted celestial body.
• Aerodynamics — is the study of the motion of air, particularly its interaction with a solid object, such as an airplane wing. It is a sub-field of fluid dynamics and gas dynamics, and many aspects of aerodynamics theory are common to these fields.
• Aeroelasticity — is the branch of physics and engineering that studies the interactions between the inertial, elastic, and aerodynamic forces that occur when an elastic body is exposed to a fluid flow. Although historical studies have been focused on aeronautical applications, recent research has found applications in fields such as energy harvesting and understanding snoring. The study of aeroelasticity may be broadly classified into two fields: static aeroelasticity, which deals with the static or steady response of an elastic body to a fluid flow; and dynamic aeroelasticity, which deals with the body's dynamic (typically vibrational) response. Aeroelasticity draws on the study of fluid mechanics, solid mechanics, structural dynamics and dynamical systems. The synthesis of aeroelasticity with thermodynamics is known as aerothermoelasticity, and its synthesis with control theory is known as aeroservoelasticity.
• Aeronautics — Is the science or art involved with the study, design, and manufacturing of air flight capable machines, and the techniques of operating aircraft and rockets within the atmosphere.
• Aerospace architecture — is broadly defined to encompass architectural design of non-habitable and habitable structures and living and working environments in aerospace-related facilities, habitats, and vehicles. These environments include, but are not limited to: science platform aircraft and aircraft-deployable systems; space vehicles, space stations, habitats and lunar and planetary surface construction bases; and Earth-based control, experiment, launch, logistics, payload, simulation and test facilities. Earth analogs to space applications may include Antarctic, desert, high altitude, underground, undersea environments and closed ecological systems.
• Aerospace bearing — Aerospace bearings are the bearings installed in aircraft and aerospace systems including commercial, private, military, or space applications.
• Aerospace engineering — is the primary field of engineering concerned with the development of aircraft and spacecraft. It has two major and overlapping branches: Aeronautical engineering and Astronautical Engineering. Avionics engineering is similar, but deals with the electronics side of aerospace engineering.
• Aerospace materials — are materials, frequently metal alloys, that have either been developed for, or have come to prominence through, their use for aerospace purposes. These uses often require exceptional performance, strength or heat resistance, even at the cost of considerable expense in their production or machining. Others are chosen for their long-term reliability in this safety-conscious field, particularly for their resistance to fatigue.
• Aerospike engine — is a type of rocket engine that maintains its aerodynamic efficiency across a wide range of altitudes. It belongs to the class of altitude compensating nozzle engines. A vehicle with an aerospike engine uses 25–30% less fuel at low altitudes, where most missions have the greatest need for thrust.
• Aerostat — is a lighter than air aircraft that gains its lift through the use of a buoyant gas. Aerostats include unpowered balloons and powered airships.
• Aerostructure — is a component of an aircraft's airframe. This may include all or part of the fuselage, wings, or flight control surfaces.
• Aft-crossing trajectory — is an alternate flight path for a rocket. The rocket's rotation (induced by the deployment from the aircraft) is slowed by a small parachute attached to its tail, then ignited once the carrier aircraft has passed it. It is ignited before it is pointing fully vertically, however it will turn to do so, and accelerates to pass behind the carrier aircraft.
• AGL — Above ground level
• Aileron — is a hinged flight control surface usually forming part of the trailing edge of each wing of a fixed-wing aircraft. Ailerons are used in pairs to control the aircraft in roll (or movement around the aircraft's longitudinal axis), which normally results in a change in flight path due to the tilting of the lift vector. Movement around this axis is called 'rolling' or 'banking'.
• Air-augmented rocket —
• Aircraft — is a machine that is able to fly by gaining support from the air. It counters the force of gravity by using either static lift or by using the dynamic lift of an airfoil, or in a few cases the downward thrust from jet engines. Common examples of aircraft include airplanes, helicopters, airships (including blimps), gliders, and hot air balloons.
• Aircraft flight control systems — A conventional fixed-wing aircraft flight control system consists of flight control surfaces, the respective cockpit controls, connecting linkages, and the necessary operating mechanisms to control an aircraft's direction in flight. Aircraft engine controls are also considered as flight controls as they change speed.
• Aircraft flight mechanics —
• Airfoil — An airfoil (American English) or aerofoil (British English) is the cross-sectional shape of a wing, blade (of a propeller, rotor, or turbine), or sail (as seen in cross-section).
• Airlock — is a device which permits the passage of people and objects between a pressure vessel and its surroundings while minimizing the change of pressure in the vessel and loss of air from it. The lock consists of a small chamber with two airtight doors in series which do not open simultaneously.
• Airship — An airship or dirigible balloon is a type of aerostat or lighter-than-air aircraft that can navigate through the air under its own power. Aerostats gain their lift from large gas bags filled with a lifting gas that is less dense than the surrounding air.
• Albedo — is the measure of the diffuse reflection of solar radiation out of the total solar radiation received by an astronomical body (e.g. a planet like Earth). It is dimensionless and measured on a scale from 0 (corresponding to a black body that absorbs all incident radiation) to 1 (corresponding to a body that reflects all incident radiation).
• Anemometer — is a device used for measuring wind speed, and is also a common weather station instrument. The term is derived from the Greek word anemos, which means wind, and is used to describe any wind speed instrument used in meteorology.
• Angle of attack — In fluid dynamics, angle of attack (AOA, or $\alpha$) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is moving. Angle of attack is the angle between the body's reference line and the oncoming flow.
• Angular momentum — In physics, angular momentum (rarely, moment of momentum or rotational momentum) is the rotational equivalent of linear momentum. It is an important quantity in physics because it is a conserved quantity—the total angular momentum of a system remains constant unless acted on by an external torque.
• Angular velocity — In physics, the angular velocity of a particle is the rate at which it rotates around a chosen center point: that is, the time rate of change of its angular displacement relative to the origin (i.e. in layman's terms: how quickly an object goes around something over a period of time - e.g. how fast the earth orbits the sun). It is measured in angle per unit time, radians per second in SI units, and is usually represented by the symbol omega (ω, sometimes Ω). By convention, positive angular velocity indicates counter-clockwise rotation, while negative is clockwise.
• Anticyclone — An anticyclone (that is, opposite to a cyclone) is a weather phenomenon defined by the United States National Weather Service's glossary as "a large-scale circulation of winds around a central region of high atmospheric pressure, clockwise in the Northern Hemisphere, counterclockwise in the Southern Hemisphere".
• Antimatter rocket — is a proposed class of rockets that use antimatter as their power source. There are several designs that attempt to accomplish this goal. The advantage to this class of rocket is that a large fraction of the rest mass of a matter/antimatter mixture may be converted to energy, allowing antimatter rockets to have a far higher energy density and specific impulse than any other proposed class of rocket.
• Apsis — is an extreme point in the orbit of an object. The word comes via Latin from Greek and is cognate with apse. For elliptic orbits about a larger body, there are two apsides, named with the prefixes peri- (from περί (peri), meaning 'near') and ap-/apo- (from ἀπ(ό) (ap(ó)), meaning 'away from') added to a reference to the body being orbited.
• Arcjet rocket — or arcjet thruster is a form of electrically powered spacecraft propulsion, in which an electrical discharge (arc) is created in a flow of propellant (typically hydrazine or ammonia). This imparts additional energy to the propellant, so that one can extract more work out of each kilogram of propellant, at the expense of increased power consumption and (usually) higher cost. Also, the thrust levels available from typically used arcjet engines are very low compared with chemical engines.
• Areal velocity — In classical mechanics, areal velocity (also called sector velocity or sectorial velocity) is the rate at which area is swept out by a particle as it moves along a curve.
• Argument of periapsis — (also called argument of perifocus or argument of pericenter), symbolized as ω, is one of the orbital elements of an orbiting body. Parametrically, ω is the angle from the body's ascending node to its periapsis, measured in the direction of motion.
• ARP4761 —
• Aspect ratio (aeronautics) — In aeronautics, the aspect ratio of a wing is the ratio of its span to its mean chord. It is equal to the square of the wingspan divided by the wing area. Thus, a long, narrow wing has a high aspect ratio, whereas a short, wide wing has a low aspect ratio. Aspect ratio and other features of the planform are often used to predict the aerodynamic efficiency of a wing because the lift-to-drag ratio increases with aspect ratio, improving fuel economy in aircraft.
• Asteroid — Asteroids are minor planets, especially of the inner Solar System. Larger asteroids have also been called planetoids. These terms have historically been applied to any astronomical object orbiting the Sun that did not resemble a planet-like disc and was not observed to have characteristics of an active comet such as a tail. As minor planets in the outer Solar System were discovered they were typically found to have volatile-rich surfaces similar to comets. As a result, they were often distinguished from objects found in the main asteroid belt.
• Astrodynamics — Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft.
• Atmospheric entry — is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet or natural satellite. There are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or following a predetermined course. Technologies and procedures allowing the controlled atmospheric entry, descent and landing of spacecraft are collectively termed as EDL.
• Attitude control — is controlling the orientation of an object with respect to an inertial frame of reference or another entity like the celestial sphere, certain fields, and nearby objects, etc. Controlling vehicle attitude requires sensors to measure vehicle orientation, actuators to apply the torques needed to re-orient the vehicle to a desired attitude, and algorithms to command the actuators based on (1) sensor measurements of the current attitude and (2) specification of a desired attitude. The integrated field that studies the combination of sensors, actuators and algorithms is called "Guidance, Navigation and Control" (GNC).
• Automatic direction finder — (ADF) is a marine or aircraft radio-navigation instrument that automatically and continuously displays the relative bearing from the ship or aircraft to a suitable radio station.
• Avionics — are the electronic systems used on aircraft, artificial satellites, and spacecraft. Avionic systems include communications, navigation, the display and management of multiple systems, and the hundreds of systems that are fitted to aircraft to perform individual functions.
• Axial stress — a normal stress parallel to the axis of cylindrical symmetry.

B

• Balloon — In aeronautics, a balloon is an unpowered aerostat, which remains aloft or floats due to its buoyancy. A balloon may be free, moving with the wind, or tethered to a fixed point. It is distinct from an airship, which is a powered aerostat that can propel itself through the air in a controlled manner.
• Ballute — (a portmanteau of balloon and parachute) is a parachute-like braking device optimized for use at high altitudes and supersonic velocities. Invented by Goodyear in 1958, the original ballute was a cone-shaped balloon with a toroidal burble fence fitted around its widest point. A burble fence is an inflated structure intended to ensure flow separation. This stabilizes the ballute as it decelerates through different flow regimes (from supersonic to subsonic).
• Beam-powered propulsion — also known as directed energy propulsion, is a class of aircraft or spacecraft propulsion that uses energy beamed to the spacecraft from a remote power plant to provide energy. The beam is typically either a microwave or a laser beam and it is either pulsed or continuous. A continuous beam lends itself to thermal rockets, photonic thrusters and light sails, whereas a pulsed beam lends itself to ablative thrusters and pulse detonation engines.
• Bearing — In navigation, bearing is the horizontal angle between the direction of an object and another object, or between it and that of true north. Absolute bearing refers to the angle between the magnetic North (magnetic bearing) or true North (true bearing) and an object. For example, an object to the East would have an absolute bearing of 90 degrees. 'Relative bearing refers to the angle between the craft's forward direction, and the location of another object. For example, an object relative bearing of 0 degrees would be dead ahead; an object relative bearing 180 degrees would be behind. Bearings can be measured in mils or degrees.
• Bernoulli's principle — In fluid dynamics, Bernoulli's principle states that an increase in the speed of a fluid occurs simultaneously with a decrease in pressure or a decrease in the fluid's potential energy.
• Bi-elliptic transfer — is an orbital maneuver that moves a spacecraft from one orbit to another and may, in certain situations, require less delta-v than a Hohmann transfer maneuver. The bi-elliptic transfer consists of two half-elliptic orbits. From the initial orbit, a first burn expends delta-v to boost the spacecraft into the first transfer orbit with an apoapsis at some point $r_{b}$ away from the central body. At this point a second burn sends the spacecraft into the second elliptical orbit with periapsis at the radius of the final desired orbit, where a third burn is performed, injecting the spacecraft into the desired orbit.
• Big dumb booster — (BDB), is a general class of launch vehicle based on the premise that it is cheaper to operate large rockets of simple design than it is to operate smaller, more complex ones regardless of the lower payload efficiency.
• Bleed air — produced by gas turbine engines is compressed air that is taken from the compressor stage of those engines, which is upstream of the fuel-burning sections.
• Booster — A booster rocket (or engine) is either the first stage of a multistage launch vehicle, or else a shorter-burning rocket used in parallel with longer-burning sustainer rockets to augment the space vehicle's takeoff thrust and payload capability.
• Boundary layer — In physics and fluid mechanics, a boundary layer is an important concept and refers to the layer of fluid in the immediate vicinity of a bounding surface where the effects of viscosity are significant. In the Earth's atmosphere, the atmospheric boundary layer is the air layer near the ground affected by diurnal heat, moisture or momentum transfer to or from the surface. On an aircraft wing the boundary layer is the part of the flow close to the wing, where viscous forces distort the surrounding non-viscous flow.
• Buoyancy — In physics, buoyancy or upthrust, is an upward force exerted by a fluid that opposes the weight of an immersed object. In a column of fluid, pressure increases with depth as a result of the weight of the overlying fluid. Thus the pressure at the bottom of a column of fluid is greater than at the top of the column. Similarly, the pressure at the bottom of an object submerged in a fluid is greater than at the top of the object. This pressure difference results in a net upwards force on the object. The magnitude of that force exerted is proportional to that pressure difference, and (as explained by Archimedes' principle) is equivalent to the weight of the fluid that would otherwise occupy the volume of the object, i.e. the displaced fluid.

C

• Cabin pressurization — is a process in which conditioned air is pumped into the cabin of an aircraft or spacecraft, in order to create a safe and comfortable environment for passengers and crew flying at high altitudes. For aircraft, this air is usually bled off from the gas turbine engines at the compressor stage, and for spacecraft, it is carried in high-pressure, often cryogenic tanks. The air is cooled, humidified, and mixed with recirculated air if necessary, before it is distributed to the cabin by one or more environmental control systems. The cabin pressure is regulated by the outflow valve.
• Cable lacing — is a method for tying wiring harnesses and cable looms, traditionally used in telecommunication, naval, and aerospace applications. This old cable management technique, taught to generations of linemen, is still used in some modern applications since it does not create obstructions along the length of the cable, avoiding the handling problems of cables groomed by plastic or hook-and-loop cable ties.
• Canard — is an aeronautical arrangement wherein a small forewing or foreplane is placed forward of the main wing of a fixed-wing aircraft. The term "canard" may be used to describe the aircraft itself, the wing configuration or the foreplane.
• Centennial challenges —
• Center of gravity — A body's center of gravity is the point around which the resultant torque due to gravity forces vanishes. Where a gravity field can be considered to be uniform, the mass-center and the center-of-gravity will be the same. However, for satellites in orbit around a planet, in the absence of other torques being applied to a satellite, the slight variation (gradient) in gravitational field between closer-to (stronger) and further-from (weaker) the planet can lead to a torque that will tend to align the satellite such that its long axis is vertical. In such a case, it is important to make the distinction between the center-of-gravity and the mass-center. Any horizontal offset between the two will result in an applied torque.
• Center of mass —
• Center of pressure —
• Chord —
• Clean configuration —
• Cockpit —
• Collimated light —
• Comet —
• Compression —
• Compressibility —
• Computational fluid dynamics —
• Computing —
• Constant speed drive —
• Control engineering —
• Conservation of momentum —
• Controllability —
• Crew Exploration Vehicle —
• Critical mach — In aerodynamics, the critical Mach number (Mcr or M* ) of an aircraft is the lowest Mach number at which the airflow over some point of the aircraft reaches the speed of sound, but does not exceed it. At the lower critical Mach number, airflow around the entire aircraft is subsonic. At the upper critical Mach number, airflow around the entire aircraft is supersonic.
• Centrifugal compressor —
• Constant speed drive —
• Corrected flow —
• Corrected speed —
• Cylinder stress — In mechanics, a cylinder stress is a stress distribution with rotational symmetry; that is, which remains unchanged if the stressed object is rotated about some fixed axis.

D

• Damage tolerance — is a property of a structure relating to its ability to sustain defects safely until repair can be effected. The approach to engineering design to account for damage tolerance is based on the assumption that flaws can exist in any structure and such flaws propagate with usage.
• Decalage —
• De Laval nozzle —
• Dead reckoning —
• Deflection —
• Deformation (engineering) —
• Deformation (mechanics) —
• Delta-v —
• Delta-v budget —
• Delta wing—
• Density —
• Departure resistance –
• Derivative —
• Digital Datcom —
• Dihedral —
• Disk loading —
• Displacement (vector) —
• Distance measuring equipment —
• DME — distance measuring equipment.
• DO-178B —
• DO-254 —
• Drag (physics) —
• Drag coefficient — In fluid dynamics, the drag coefficient (commonly denoted as: $\scriptstyle C_{\mathrm {d} }\,$, $\scriptstyle C_{\mathrm {x} }\,$ or $\scriptstyle C_{\mathrm {w} }\,$) is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. It is used in the drag equation in which a lower drag coefficient indicates the object will have less aerodynamic or hydrodynamic drag. The drag coefficient is always associated with a particular surface area.
• Drag equation —
• Drop test —
• Dual mode propulsion rocket —
• Ductility —

E

• Earth's atmosphere —
• Eccentric anomaly —
• Eccentricity vector —
• Eigenvector slew —
• Electrostatic ion thruster —
• Elevator —
• Elliptic partial differential equation —
• Empennage —
• Energy —
• Engineering —
• Engineering economics —
• Enstrophy —
• Equation of motion —
• ESA — European Space Agency
• Euler angles —
• European Space Agency —
• Expander cycle (rocket) —

F

• Fatigue —
• Field emission electric propulsion —
• Fixed-wing aircraft —
• Flange —
• Flap —
• Flight control surfaces —
• Flight control system (aircraft) —
• Flight control system (helicopter) —
• Flight dynamics —
• Flight management system —
• Floatstick —
• Fluid —
• Fluid dynamics —
• Fluid mechanics —
• Fluid statics —
• FMS — Flight management system.
• Force —
• Freefall —
• Fuselage —
• Future Air Navigation System —
• Flying wing —

G

• Galaxy —
• Gas-generator cycle (rocket) —
• Geostationary orbit —
• Geosynchronous orbit—
• Glide ratio —
• Glider —
• Global Positioning System —
• Goddard problem —
• GPS — Global Positioning System.
• Gravitational constant —
• Gravitational slingshot —
• Gravity —

H

• Hall effect thruster —
• Heat shield —
• Helicopter —
• High-hypersonic —
• Hohmann transfer orbit —
• Hybrid rocket —
• Hydrodynamics —
• Hydrostatics —
• Hyperbolic partial differential equation —
• Hypersonic —
• Hypoxia —
• HyShot —

I

• Impulse —
• Indicated airspeed —
• Instrument landing system —
• Integral —
• Internal combustion —
• Interplanetary Transport Network —
• Interplanetary travel —
• Interstellar travel —
• Ion thruster —
• ISRO —

J

• Jet engine —

K

• Keel effect —
• Kepler's laws of planetary motion —
• Kessler syndrome —
• Kestrel rocket engine —
• Kinetic energy —
• Kite —
• Kutta condition —
• Kutta–Joukowski theorem —

L

• Landing —
• Landing gear —
• Lagrangian —
• Lagrangian point —
• Laser broom —
• Laser Camera System —
• Latus rectum —
• Launch window —
• Law of universal gravitation —
• Leading edge —
• Lift —
• Lift coefficient — is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. A lifting body is a foil or a complete foil-bearing body such as a fixed-wing aircraft. C_L is a function of the angle of the body to the flow, its Reynolds number and its Mach number. The lift coefficient c_l refers to the dynamic lift characteristics of a two-dimensional foil section, with the reference area replaced by the foil chord.
• Lightcraft —
• Lighter than air —
• Liquid air cycle engine —
• Liquid fuels —
• Liquid-propellant rocket —
• Liquid rocket propellants —
• Lithobraking —
• Loiter —
• Low Earth orbit —
• Lunar space elevator —

M

• Mach number — In fluid dynamics, the Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
• Magnetic sail —
• Magnetoplasmadynamic thruster —
• Mass —
• Mass driver —
• Mechanics of fluids —
• Membrane mirror —
• Metre per second —
• Microwave landing system —
• Mini-magnetospheric plasma propulsion —
• Moment of inertia —
• Momentum —
• Momentum wheel —
• Monopropellant rocket —
• Motion —
• Multistage rocket —

N

• Nanotechnology —
• NASA —
• Navier–Stokes equations —
• Newton (unit) —
• Newton's laws of motion —
• Nose cone design —
• Nozzle —

O

• Orbit —
• Orbit phasing —
• Orbital eccentricity —
• Orbital elements —
• Orbital inclination —
• Orbital inclination change —
• Orbital maneuver —
• Orbital mechanics —
• Orbital node —
• Orbital period —
• Orbital stationkeeping —
• Orbiter Boom Sensor System —
• Osculating orbit —

P

• Parallel axes rule —
• Parasitic drag —
• Parawing —
• Perpendicular axes rule —
• Physical science —
• Physics —
• Planetary orbit —
• Plasma (physics) —
• Plug nozzle —
• Pogo oscillation —
• Prandtl–Glauert singularity —
• Precession —
• Pressure —
• Pressure altitude —
• Pressure-fed engine —
• Propeller —
• Proper orbital elements —
• Pulsed inductive thruster —
• Pulsed plasma thruster —
• Propulsion —

R

• Radar —
• Radio direction finder —
• Railgun —
• Ram accelerator —
• Ramjet —
• Rate of climb –
• Reaction control system —
• Redshift rocket —
• Reentry —
• Reflection —
• Relativistic rocket —
• Remote Manipulator System —
• Resistojet rocket —
• Reusable launch system —
• Reynolds number —
• RL-10 (rocket engine) —
• Rocket —
• Rocket engine –
• Rocket engine nozzle —
• Rocket fuel —
• Rocket launch —
• Rudder —

S

• SABRE —
• Satellite —
• Saturn (rocket family) —
• Scalar (physics) —
• Schlieren —
• Schlieren photography —
• Scramjet —
• Second moment of area —
• Shock wave —
• SI —
• Single point of failure —
• Single-stage to orbit —
• Skyhook (structure) —
• Slew —
• Stream function —
• Streamline —
• Solar panel —
• Solar sail —
• Solar thermal rocket —
• Solid of revolution —
• Solid rocket —
• Sound barrier —
• Space activity suit —
• Space elevator —
• Space fountain —
• Space plane —
• Space Shuttle —
• Space Shuttle external tank —
• Space Shuttle Main Engine —
• Space station —
• Space suit —
• Space technology —
• Space transport —
• Spacecraft —
• Spacecraft design —
• Spacecraft propulsion —
• Special relativity —
• Specific impulse —
• Speed of sound —
• Staged combustion cycle (rocket) —
• Subsonic —
• Supersonic —
• Surface of revolution —
• Sweep theory —

T

• Tait–Bryan rotations —
• Temperature —
• Terminal velocity —
• Test target —
• Tether propulsion —
• Thermal protection system —
• Thermodynamics —
• Thrust —
• Thruster —
• Torricelli's equation —
• Total air temperature —
• Trajectory —
• Trailing edge —
• Trans Lunar Injection —
• Transonic —
• Transverse wave —
• Tripropellant rocket —
• Tsiolkovsky rocket equation —
• Turbomachinery —
• Two stage to orbit —

U

• UFO —

V

• V-2 rocket —
• Variable specific impulse magnetoplasma rocket —
• Velocity —
• Viscometer —
• Viscosity —
• Vortex generator —

W

• Wave drag —
• Weight —
• Weight function —
• Wind tunnel —
• Wing —
• Woodward effect —
• Wright Flyer —
• Wright Glider of 1902 —

See also

• Aerospace engineering
• List of aviation, aerospace and aeronautical abbreviations
• Engineering
• Glossary of engineering
• National Council of Examiners for Engineering and Surveying (NCEES)
• Fundamentals of Engineering Examination
• Principles and Practice of Engineering Examination (PE exam)
• Graduate Aptitude Test in Engineering (GATE)
• Glossary of areas of mathematics
• Glossary of artificial intelligence
• Glossary of astronomy
• Glossary of biology
• Glossary of chemistry
• Glossary of civil engineering
• Glossary of economics
• Glossary of mechanical engineering
• Glossary of physics
• Glossary of probability and statistics
• Glossary of structural engineering