Glossary of aerospace engineering

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

A[]

• Above ground level — In aviation, atmospheric sciences and broadcasting, a height above ground level (AGL^[1]) 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^[2] or grams per kilogram.^[3]
• 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.^[4] 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.^[5][6] 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.^[7] The point at which a spacecraft comes closest to a ground observer is the time of closest approach.^[7]
• 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.^[8] 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.^[9] 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.^[9]
• 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 with respect to its interaction with a solid object, such as an airplane wing. Aerodynamics is a sub-field of gas dynamics, which in turn is a sub-field of fluid dynamics. Many aspects and principles of aerodynamics theory are common to these three 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^[10] and understanding snoring.^[11] 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.^[12] 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,^[13] 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.^[14]
• 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.^[15] 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 ${\displaystyle \alpha }$) 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.^[16] 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".^[17]
• 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.^[18] For elliptic orbits about a larger body, there are two apsides, named with the prefixes peri- (from περί (peri) 'near') and ap-/apo- (from ἀπ(ό) (ap(ó)) '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^[19][20] (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.^[21] 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.^[22]
• 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.^[23][24]
• 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.^[25] 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.^[26]
• 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.^[27] 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.^{[28]: Ch.3 [29]: 156–164, § 3.5}
• 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 ${\displaystyle r_{b}}$ 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.^[30]
• 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.^[31]
• 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.^[32][33]
• 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.^[34] 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,^[35] 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.
• Camber — the asymmetric curves on the top and bottom, or front and back, of an aerofoil
• 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.^[36][37][38]
• 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 — In physics, the center of mass of a distribution of mass in space is the unique point where the weighted relative position of the distributed mass sums to zero, or the point where if a force is applied it moves in the direction of the force without rotating. The distribution of mass is balanced around the center of mass and the average of the weighted position coordinates of the distributed mass defines its coordinates.
• Center of pressure — is the point where the total sum of a pressure field acts on a body, causing a force to act through that point.
• Centrifugal compressor — Centrifugal compressors, sometimes called radial compressors, are a sub-class of dynamic axisymmetric work-absorbing turbomachinery.^[39] They achieve a pressure rise by adding kinetic energy/velocity to a continuous flow of fluid through the rotor or impeller. This kinetic energy is then converted to an increase in potential energy/static pressure by slowing the flow through a diffuser. The pressure rise in the impeller is in most cases almost equal to the rise in the diffuser.
• Chord — is the imaginary straight line joining the leading and trailing edges of an aerofoil. The chord length is the distance between the trailing edge and the point on the leading edge where the chord intersects the leading edge.^[40][41]
• Clean configuration — is the flight configuration of a fixed-wing aircraft when its external equipment is retracted to minimize drag and thus maximize airspeed for a given power setting.
• Cockpit — or flight deck, is the area, usually near the front of an aircraft or spacecraft, from which a pilot controls the aircraft.
• Collimated beam — A collimated beam of light or other electromagnetic radiation has parallel rays, and therefore will spread minimally as it propagates. A perfectly collimated light beam, with no divergence, would not disperse with distance. Such a beam cannot be created, due to diffraction.^[42]
• Comet — is an icy, small Solar System body that, when passing close to the Sun, warms and begins to release gases, a process called outgassing. This produces a visible atmosphere or coma, and sometimes also a tail.
• Compressibility — In thermodynamics and fluid mechanics, compressibility (also known as the coefficient of compressibility^[43] or isothermal compressibility^[44]) is a measure of the relative volume change of a fluid or solid as a response to a pressure (or mean stress) change. In its simple form, the compressibility ${\displaystyle \beta }$ may be expressed as

${\displaystyle \beta =-{\frac {1}{V}}{\frac {\partial V}{\partial p}}}$, where V is volume and p is pressure. The choice to define compressibility as the opposite of the fraction makes compressibility positive in the (usual) case that an increase in pressure induces a reduction in volume. t is also known as reciprocal of bulk modulus(k) of elasticity of a fluid.

• Compression — In mechanics, compression is the application of balanced inward ("pushing") forces to different points on a material or structure, that is, forces with no net sum or torque directed so as to reduce its size in one or more directions.^[45] It is contrasted with tension or traction, the application of balanced outward ("pulling") forces; and with shearing forces, directed so as to displace layers of the material parallel to each other. The compressive strength of materials and structures is an important engineering consideration.
• Compressor map – is a diagram showing significant performance parameters for a rotating compressor, and how they vary with changing ambient conditions of pressure and temperature.
• Computational fluid dynamics — (CFD), is a branch of fluid mechanics that uses numerical analysis and data structures to analyze and solve problems that involve fluid flows. Computers are used to perform the calculations required to simulate the free-stream flow of the fluid, and the interaction of the fluid (liquids and gases) with surfaces defined by boundary conditions. With high-speed supercomputers, better solutions can be achieved, and are often required to solve the largest and most complex problems.
• Conservation of momentum — The total momentum of objects involved in a collision remains constant regardless of friction and permanent deformation that may occur during the collision. The law of conservation of momentum can be used to analyse the interactions between objects, even in the presence of friction and other non-conservative forces. Conservation of momentum is a consequence of Newton's laws of motion.
• Constant speed drive — (CSD), is a type of transmission that takes an input shaft rotating at a wide range of speeds, delivering this power to an output shaft that rotates at a constant speed, despite the varying input. They are used to drive mechanisms, typically electrical generators, that require a constant input speed. The term is most commonly applied to hydraulic transmissions found on the accessory drives of gas turbine engines, such as aircraft jet engines. On modern aircraft, the CSD is often combined with a generator into a single unit known as an integrated drive generator (IDG).
• Control engineering — or control systems engineering, is an engineering discipline that applies automatic control theory to design systems with desired behaviors in control environments.^[46] The discipline of controls overlaps and is usually taught along with electrical engineering at many institutions around the world.^[46]
• 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.^[47] 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.^[48]
• 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 — Decalage on a fixed-wing aircraft is the angle difference between the upper and lower wings of a biplane, i.e. the acute angle contained between the chords of the wings in question. Decalage is said to be positive when the upper wing has a higher angle of incidence than the lower wing, and negative when the lower wing's incidence is greater than that of the upper wing. Positive decalage results in greater lift from the upper wing than the lower wing, the difference increasing with the amount of decalage.^[49]
• De Laval nozzle — (or convergent-divergent nozzle, CD nozzle or con-di nozzle), is a tube that is pinched in the middle, making a carefully balanced, asymmetric hourglass shape. It is used to accelerate a hot, pressurized gas passing through it to a higher supersonic speed in the axial (thrust) direction, by converting the heat energy of the flow into kinetic energy. Because of this, the nozzle is widely used in some types of steam turbines and rocket engine nozzles. It also sees use in supersonic jet engines.
• Dead reckoning — In navigation, dead reckoning is the process of calculating one's current position by using a previously determined position, or fix, and advancing that position based upon known or estimated speeds over elapsed time and course.
• Deflection — is the degree to which a structural element is displaced under a load. It may refer to an angle or a distance.
• Deformation (engineering) — In materials science, deformation refers to any changes in the shape or size of an object due to an applied force (the deformation energy, in this case, is transferred through work) or a change in temperature (the deformation energy, in this case, is transferred through heat).
• Deformation (mechanics) — in continuum mechanics is the transformation of a body from a reference configuration to a current configuration.^[50] A configuration is a set containing the positions of all particles of the body. A deformation may be caused by external loads,^[51] body forces (such as gravity or electromagnetic forces), or changes in temperature, moisture content, or chemical reactions, etc.
• Delta-v — (literally "change in velocity"), symbolised as ∆v and pronounced delta-vee, as used in spacecraft flight dynamics, is a measure of the impulse that is needed to perform a maneuver such as launch from, or landing on a planet or moon, or in-space orbital maneuver. It is a scalar that has the units of speed. As used in this context, it is not the same as the physical change in velocity of the vehicle.
• Delta-v budget — is an estimate of the total delta-v required for a space mission. It is calculated as the sum of the delta-v required for the propulsive maneuvers during the mission, and as input to the Tsiolkovsky rocket equation, determines how much propellant is required for a vehicle of given mass and propulsion system.
• Delta wing— is a wing shaped in the form of a triangle. It is named for its similarity in shape to the Greek uppercase letter delta (Δ). Although long studied, it did not find significant applications until the jet age, when it proved suitable for high-speed subsonic and supersonic flight.
• Density —
• Departure resistance – is a quality of an aircraft which enables it to remain in controlled flight and resist entering potentially dangerous less-controlled maneuvers such as spin.
• Derivative — The derivative of a function of a real variable measures the sensitivity to change of the function value (output value) with respect to a change in its argument (input value). Derivatives are a fundamental tool of calculus. For example, the derivative of the position of a moving object with respect to time is the object's velocity: this measures how quickly the position of the object changes when time advances.
• Digital Datcom — The United States Air Force Stability and Control Digital DATCOM is a computer program that implements the methods contained in the USAF Stability and Control DATCOM to calculate the static stability, control and dynamic derivative characteristics of fixed-wing aircraft. Digital DATCOM requires an input file containing a geometric description of an aircraft, and outputs its corresponding dimensionless stability derivatives according to the specified flight conditions. The values obtained can be used to calculate meaningful aspects of flight dynamics.
• Dihedral — Dihedral angle is the upward angle from horizontal of the wings or tailplane of a fixed-wing aircraft. "Anhedral angle" is the name given to negative dihedral angle, that is, when there is a downward angle from horizontal of the wings or tailplane of a fixed-wing aircraft.
• Disk loading — In fluid dynamics, disk loading or disc loading is the average pressure change across an actuator disk, such as an airscrew. Airscrews with a relatively low disk loading are typically called rotors, including helicopter main rotors and tail rotors; propellers typically have a higher disk loading.^[52]
• Displacement (vector) —
• Distance measuring equipment — (DME), is a radio navigation technology that measures the slant range (distance) between an aircraft and a ground station by timing the propagation delay of radio signals in the frequency band between 960 and 1215 megahertz (MHz). Line-of-visibility between the aircraft and ground station is required. An interrogator (airborne) initiates an exchange by transmitting a pulse pair, on an assigned ‘channel’, to the transponder ground station. The channel assignment specifies the carrier frequency and the spacing between the pulses. After a known delay, the transponder replies by transmitting a pulse pair on a frequency that is offset from the interrogation frequency by 63 MHz and having specified separation.^[53]
• DME — distance measuring equipment.
• DO-178B —
• DO-254 —
• Drag (physics) — In fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.^[54] This can exist between two fluid layers (or surfaces) or a fluid and a solid surface. Unlike other resistive forces, such as dry friction, which are nearly independent of velocity, drag forces depend on velocity.^[55][56] Drag force is proportional to the velocity for a laminar flow and the squared velocity for a turbulent flow. Even though the ultimate cause of a drag is viscous friction, the turbulent drag is independent of viscosity.^[57] Drag forces always decrease fluid velocity relative to the solid object in the fluid's path.
• Drag coefficient — In fluid dynamics, the drag coefficient (commonly denoted as: ${\displaystyle \scriptstyle C_{\mathrm {d} }\,}$, ${\displaystyle \scriptstyle C_{\mathrm {x} }\,}$ or ${\displaystyle \scriptstyle C_{\mathrm {w} }\,}$) 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.^[58]
• Drag equation — In fluid dynamics, the drag equation is a formula used to calculate the force of drag experienced by an object due to movement through a fully enclosing fluid. The equation is:

${\displaystyle F_{D}\,=\,{\tfrac {1}{2}}\,\rho \,u^{2}\,C_{D}\,A}$

${\displaystyle F_{D}}$ is the drag force, which is by definition the force component in the direction of the flow velocity,

${\displaystyle \rho }$ is the mass density of the fluid,^[59]

${\displaystyle u}$ is the flow velocity relative to the object,

${\displaystyle A}$ is the reference area, and

${\displaystyle C_{D}}$ is the drag coefficient – a dimensionless coefficient related to the object's geometry and taking into account both skin friction and form drag. In general, ${\displaystyle C_{D}}$ depends on the Reynolds number.

• Drop test — is a method of testing the in-flight characteristics of prototype or experimental aircraft and spacecraft by raising the test vehicle to a specific altitude and then releasing it. Test flights involving powered aircraft, particularly rocket-powered aircraft, may be referred to as drop launches due to the launch of the aircraft's rockets after release from its carrier aircraft.
• Dual mode propulsion rocket — Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets. It is based upon the use of two rocket fuels, liquid hydrogen and more dense hydrocarbon fuels, like RP, which are all burned with liquid oxygen.^[60]
• Ductility — is a measure of a material's ability to undergo significant plastic deformation before rupture, which may be expressed as percent elongation or percent area reduction from a tensile test.

E[]

• Earth's atmosphere — The atmosphere of Earth is the layer of gases, commonly known as air, that surrounds the planet Earth and is retained by Earth's gravity. The atmosphere of Earth protects life on Earth by creating pressure allowing for liquid water to exist on the Earth's surface, absorbing ultraviolet solar radiation, warming the surface through heat retention (greenhouse effect), and reducing temperature extremes between day and night (the diurnal temperature variation).
• Eccentric anomaly — In orbital mechanics, the eccentric anomaly is an angular parameter that defines the position of a body that is moving along an elliptic Kepler orbit. The eccentric anomaly is one of three angular parameters ("anomalies") that define a position along an orbit, the other two being the true anomaly and the mean anomaly.
• Eccentricity vector — In celestial mechanics, the eccentricity vector of a Kepler orbit is the dimensionless vector with direction pointing from apoapsis to periapsis and with magnitude equal to the orbit's scalar eccentricity. For Kepler orbits the eccentricity vector is a constant of motion. Its main use is in the analysis of almost circular orbits, as perturbing (non-Keplerian) forces on an actual orbit will cause the osculating eccentricity vector to change continuously. For the eccentricity and argument of periapsis parameters, eccentricity zero (circular orbit) corresponds to a singularity. The magnitude of the eccentricity vector represents the eccentricity of the orbit. Note that the velocity and position vectors need to be relative to the inertial frame of the central body.
• Eigenvector slew — In aerospace engineering, especially those areas dealing with spacecraft, the eigenvector slew is a method to calculate a steering correction (called a slew) by rotating the spacecraft around one fixed axis, or a gimbal. This corresponds in general to the fastest and most efficient way to reach the desired target orientation as there is only one acceleration phase and one braking phase for the angular rate. If this fixed axis is not a principal axis a time varying torque must be applied to force the spacecraft to rotate as desired, though. Also the gyroscopic effect of momentum wheels must be compensated for.
• Electrostatic ion thruster — is a form of electric propulsion used for spacecraft propulsion. It creates thrust by accelerating ions using electricity.
• Elevator — is a flight control surface, usually at the rear of an aircraft, which control the aircraft's pitch, and therefore the angle of attack and the lift of the wing. The elevators are usually hinged to the tailplane or horizontal stabilizer.
• Elliptic partial differential equation —
• Empennage — The empennage (/ˌɑːmpɪˈnɑːʒ/ or /ˈɛmpɪnɪdʒ/), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.^[61][62][63] The term derives from the French language verb empenner which means "to feather an arrow".^[64] Most aircraft feature an empennage incorporating vertical and horizontal stabilising surfaces which stabilise the flight dynamics of yaw and pitch,^[61][62] as well as housing control surfaces.

• Enstrophy — In fluid dynamics, the enstrophy E can be interpreted as another type of potential density; or, more concretely, the quantity directly related to the kinetic energy in the flow model that corresponds to dissipation effects in the fluid. It is particularly useful in the study of turbulent flows, and is often identified in the study of thrusters as well as the field of combustion theory.

Given a domain ${\displaystyle \Omega \subseteq \mathbb {R} ^{n}}$ and a once-weakly differentiable vector field ${\displaystyle u\in H^{1}(\mathbb {R} ^{n})^{n}}$ which represents a fluid flow, such as a solution to the Navier-Stokes equations, its enstrophy is given by:^[65]

${\displaystyle {\mathcal {E}}(u):=\int _{\Omega }|\nabla \mathbf {u} |^{2}\,dx}$

Where ${\displaystyle |\nabla \mathbf {u} |^{2}=\sum _{i,j=1}^{n}\left|\partial _{i}u^{j}\right|^{2}}$. This is quantity is the same as the squared seminorm ${\displaystyle |\mathbf {u} |_{H^{1}(\Omega )^{n}}^{2}}$of the solution in the Sobolev space ::::${\displaystyle H^{1}(\Omega )^{n}}$.

In the case that the flow is incompressible, or equivalently that ${\displaystyle \nabla \cdot \mathbf {u} =0}$, the enstrophy can be described as the integral of the square of the vorticity ${\displaystyle \mathbf {\omega } }$,^[66]

${\displaystyle {\mathcal {E}}({\boldsymbol {\omega }})\equiv \int _{\Omega }|{\boldsymbol {\omega }}|^{2}\,dx}$

or, in terms of the flow velocity,

${\displaystyle {\mathcal {E}}(\mathbf {u} )\equiv \int _{S}|\nabla \times \mathbf {u} |^{2}\,dS\,.}$

In the context of the incompressible Navier-Stokes equations, enstrophy appears in the following useful result^[18]

${\displaystyle {\frac {d}{dt}}\left({\frac {1}{2}}\int _{\Omega }|\mathbf {u} |^{2}\right)=-\nu {\mathcal {E}}(\mathbf {u} )}$

The quantity in parentheses on the left is the energy in the flow, so the result says that energy declines proportional to the kinematic viscosity ${\displaystyle \nu }$ times the enstrophy.

• Equations of motion — In physics, equations of motion are equations that describe the behavior of a physical system in terms of its motion as a function of time.^[67] More specifically, the equations of motion describe the behavior of a physical system as a set of mathematical functions in terms of dynamic variables. These variables are usually spatial coordinates and time, but may include momentum components. The most general choice are generalized coordinates which can be any convenient variables characteristic of the physical system.^[68] The functions are defined in a Euclidean space in classical mechanics, but are replaced by curved spaces in relativity. If the dynamics of a system is known, the equations are the solutions for the differential equations describing the motion of the dynamics.
• ESA — European Space Agency
• ET — (Space Shuttle) external tank
• Euler angles — are three angles introduced by Leonhard Euler to describe the orientation of a rigid body with respect to a fixed coordinate system.^[69] They can also represent the orientation of a mobile frame of reference in physics or the orientation of a general basis in 3-dimensional linear algebra. Alternative forms were later introduced by Peter Guthrie Tait and George H. Bryan intended for use in aeronautics and engineering.

• European Space Agency —
• Expander cycle (rocket) — is a power cycle of a bipropellant rocket engine. In this cycle, the fuel is used to cool the engine's combustion chamber, picking up heat and changing phase. The now heated and gaseous fuel then powers the turbine that drives the engine's fuel and oxidizer pumps before being injected into the combustion chamber and burned for thrust.

F[]

• Fatigue — In materials science, fatigue is the weakening of a material caused by repeatedly applied loads. It is the progressive and localized structural damage that occurs when a material is subjected to cyclic loading. The nominal maximum stress values that cause such damage may be much less than the strength of the material typically quoted as the ultimate tensile stress limit, or the yield stress limit.
• Field emission electric propulsion — (FEEP), is an advanced electrostatic space propulsion concept, a form of ion thruster, that uses a liquid metal as a propellant – usually either caesium, indium, or mercury.
• Fixed-wing aircraft — is a heavier-than-air flying machine, such as an airplane, which is capable of flight using wings that generate lift caused by the aircraft's forward airspeed and the shape of the wings. Fixed-wing aircraft are distinct from rotary-wing aircraft (in which the wings form a rotor mounted on a spinning shaft or "mast"), and ornithopters (in which the wings flap in a manner similar to that of a bird). The wings of a fixed-wing aircraft are not necessarily rigid; kites, hang gliders, variable-sweep wing aircraft and airplanes that use wing morphing are all examples of fixed-wing aircraft.
• Flange —
• Flap — is a high-lift device used to reduce the stalling speed of an aircraft wing at a given weight. Flaps are usually mounted on the wing trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance and the landing distance. Flaps also cause an increase in drag so they are retracted when not needed.
• Flight control surfaces — are aerodynamic devices allowing a pilot to adjust and control the aircraft's flight attitude.
• Flight control system (aircraft) — 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.
• Flight control system (helicopter) — A helicopter pilot manipulates the helicopter flight controls to achieve and maintain controlled aerodynamic flight.^[70] Changes to the aircraft flight control system transmit mechanically to the rotor, producing aerodynamic effects on the rotor blades that make the helicopter move in a deliberate way. To tilt forward and back (pitch) or sideways (roll) requires that the controls alter the angle of attack of the main rotor blades cyclically during rotation, creating differing amounts of lift (force) at different points in the cycle. To increase or decrease overall lift requires that the controls alter the angle of attack for all blades collectively by equal amounts at the same time, resulting in ascent, descent, acceleration and deceleration.
• Flight dynamics — is the study of the performance, stability, and control of vehicles flying through the air or in outer space.^[71] It is concerned with how forces acting on the vehicle determine its velocity and attitude with respect to time. For a fixed-wing aircraft, its changing orientation with respect to the local air flow is represented by two critical angles, the angle of attack of the wing ("alpha") and the angle of attack of the vertical tail, known as the sideslip angle ("beta"). A sideslip angle will arise if an aircraft yaws about its centre of gravity and if the aircraft sideslips bodily, i.e. the centre of gravity moves sideways.^[72] These angles are important because they are the principal source of changes in the aerodynamic forces and moments applied to the aircraft. Spacecraft flight dynamics involve three main forces: propulsive (rocket engine), gravitational, and atmospheric resistance.^[73] Propulsive force and atmospheric resistance have significantly less influence over a given spacecraft compared to gravitational forces.
• Flight management system — A flight management system (FMS) is a fundamental component of a modern airliner's avionics. An FMS is a specialized computer system that automates a wide variety of in-flight tasks, reducing the workload on the flight crew to the point that modern civilian aircraft no longer carry flight engineers or navigators. A primary function is in-flight management of the flight plan. Using various sensors (such as GPS and INS often backed up by radio navigation) to determine the aircraft's position, the FMS can guide the aircraft along the flight plan. From the cockpit, the FMS is normally controlled through a Control Display Unit (CDU) which incorporates a small screen and keyboard or touchscreen. The FMS sends the flight plan for display to the Electronic Flight Instrument System (EFIS), Navigation Display (ND), or Multifunction Display (MFD). The FMS can be summarised as being a dual system consisting of the Flight Management Computer (FMC), CDU and a cross talk bus.
• Floatstick — is a device to measure fuel levels in modern large aircraft. It consists of a closed tube rising from the bottom of the fuel tank. Surrounding the tube is a ring-shaped float, and inside it is a graduated rod indicating fuel capacity. The float and the top of the rod contain magnets. The rod is withdrawn from the bottom of the wing until the magnets stick, the distance it is withdrawn indicating the level of the fuel. When not in use, the stick is secured within the tube.
• 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 — Specific impulse (usually abbreviated I_sp) is a measure of how efficiently a rocket uses propellant or a jet engine uses fuel. For engines whose reaction mass is only the fuel they carry, specific impulse is exactly proportional to exhaust gas velocity.
• Indicated airspeed —
• Instrument landing system —
• Integral —
• Internal combustion —
• Interplanetary Transport Network —
• Interplanetary travel —
• Interstellar travel —
• Ion thruster —
• ISRO —

J[]

• Jet engine — is a type of reaction engine discharging a fast-moving jet that generates thrust by jet propulsion.

K[]

• Keel effect — In aeronautics, the keel effect (also known as the pendulum effect or pendulum stability^[74]) is the result of the sideforce-generating surfaces being above (or below) the center of mass (which coincides with the center of gravity) in an aircraft. Along with dihedral, sweepback, and weight distribution, keel effect is one of the four main design considerations in aircraft lateral stability.^[75]
• Kepler's laws of planetary motion —
• Kessler syndrome —
• Kestrel rocket engine —
• Kinetic energy —
• Kite —
• Kutta condition —
• Kutta–Joukowski theorem —

L[]

• Lander — spacecraft designed to soft-land intact or almost undamaged on the surface of a celestial body and eventually take-off from it
• 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.^[76][77]
• Lightcraft —
• Lighter than air —
• Liquid air cycle engine —
• Liquid fuels —
• Liquid-propellant rocket —
• Liquid rocket propellants —
• Lithobraking —
• LM — (Apollo) Lunar Module
• 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.^[78][79]
• 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[]

• NACA — United States National Advisory Committee for Aeronautics, replaced by NASA in 1958.
• Nanotechnology —
• NASA — United States National Aeronautics and Space Administration.
• Navier–Stokes equations —
• Newton (unit) —
• Newton's laws of motion —
• Nose cone design —
• Nozzle —

O[]

• Orbit — In physics, an orbit is the gravitationally curved trajectory of an object,^[80] such as the trajectory of a planet around a star or a natural satellite around a planet. Normally, orbit refers to a regularly repeating trajectory, although it may also refer to a non-repeating trajectory. To a close approximation, planets and satellites follow elliptic orbits, with the center of mass being orbited at a focal point of the ellipse,^[81] as described by Kepler's laws of planetary motion. For most situations, orbital motion is adequately approximated by Newtonian mechanics, which explains gravity as a force obeying an inverse-square law.^[82] However, Albert Einstein's general theory of relativity, which accounts for gravity as due to curvature of spacetime, with orbits following geodesics, provides a more accurate calculation and understanding of the exact mechanics of orbital motion.
• 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 —

Q[]

R[]

• Radar — system using the reflection from transmitted electromagnetic waves to detect the distance and rough shape of an object, working even in outer space, unlike sonar
• Radio direction finder —
• Railgun —
• Ram accelerator —
• Ramjet —
• Rate of climb –
• RCS — reaction control system
• Reaction control system — set of rocket thrusters used for spacecraft maneuvers over the craft's three rotation axes in outer space
• 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 — spacecraft able to fly from a celestial body (usually the Earth or the Moon)'s surface to its orbit without using external boosters
• 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 Shuttle — manned NASA spacecraft used between 1981 and 2011, consisting of a reusable spaceplane (the Space Shuttle orbiter, capable of airplane-like landing) attached to an expendable external tank (which disintegrated during re-entry) and two recoverable solid rocket boosters (which re-entered the Earth's atmosphere and splash-landed)
• Space Shuttle external tank — external tank attached to the orbiter and the solid rocket boosters in the NASA Space Shuttle program
• Space Shuttle main engine —
• Space Shuttle orbiter — reusable NASA spaceplane used during the Space Shuttle program (1981-2011)
• Space station — habitable artificial satellite
• Space suit —
• Space technology —
• Space transport —
• Spacecraft —
• Spacecraft design —
• Spacecraft propulsion —
• Spaceplane — vehicle capable of both atmospheric flight according to the laws of aerodynamics (like an aircraft) and spaceflight in outer space (like a spacecraft)
• Special relativity —
• Specific impulse —
• Speed of sound —
• SRB — solid rocket booster
• SSTO — single-stage-to-orbit
• Staged combustion cycle (rocket) —
• Subsonic — inferior to the speed of sound
• Supersonic — superior to the speed of sound
• 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 —
• Wright Flyer —
• Wright Glider of 1902 —

X[]

Y[]

Z[]

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

References[]