Student Technical Reference

Aerospace Reference Center

A professional quick-reference library for flight, aerospace engineering, avionics, navigation, weather, propulsion, aircraft systems, unmanned systems, and spaceflight terminology.

Reference Architecture

Use this like an engineering handbook

Start with a term, jump to a technical topic, or use the quick-reference panels while working through aerospace lessons and simulator training.

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Flight Science

Aerodynamics

Four forces, angle of attack, lift and drag, stability, load factor, and performance relationships.

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Avionics

Flight Deck

PFD, MFD, GTC, flight director, autopilot, navigation displays, engine information, and scan priorities.

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Position & Route

Navigation

Heading, course, track, GPS/GNSS, VOR, RNAV, ILS, airport references, and common navigation abbreviations.

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Atmosphere

Weather

METAR, TAF, wind, visibility, pressure, temperature, clouds, turbulence, and weather information sources.

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Energy Conversion

Propulsion

Piston-engine and propeller fundamentals, RPM, manifold pressure, temperatures, thrust, and efficiency.

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Integrated Design

Aircraft Systems

Flight controls, electrical, fuel, landing gear, braking, environmental, safety, and structural systems.

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Autonomy

UAS

UAS terminology, FAA TRUST, command and control, situational awareness, and system-level thinking.

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Beyond the Atmosphere

Space Systems

Orbit families, spacecraft attitude control, communications, guidance, propulsion, and mission architecture.

Searchable Dictionary

Aerospace & flight acronyms

Search by acronym, full term, topic, or description. Use the category filters to narrow the list.

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Flight Science

Aerodynamics quick reference

Core relationships students should recognize when analyzing aircraft behavior and performance.

The four forces

ForceDirectionPrimary Idea
LiftPerpendicular to relative windAerodynamic force generated primarily by the wings.
WeightToward EarthGravitational force acting through the center of gravity.
ThrustGenerally forwardPropulsive force produced by the engine/propeller or other propulsion system.
DragOpposes relative motionAerodynamic resistance to movement through the air.

Lift relationship

The standard engineering form of the lift equation helps explain why airspeed, air density, wing area, and lift coefficient matter.

Lift L = ½ ρ V² S CL
ρ Air density
V True airspeed relative to the air mass
S Wing reference area
CL Lift coefficient

Angle of attack

Angle of attack (AOA) is the angle between the airfoil chord line and the relative wind. It is not the same as pitch attitude.

A stall occurs when the wing exceeds its critical angle of attack. The exact airspeed at which that happens can change with weight, load factor, configuration, and other conditions.

Stability vocabulary

  • Longitudinal: pitch stability about the lateral axis.
  • Lateral: roll stability about the longitudinal axis.
  • Directional: yaw stability about the vertical axis.
  • Static stability: initial tendency after a disturbance.
  • Dynamic stability: how motion changes over time after the disturbance.
Glass Cockpit

Flight deck & avionics reference

Use this section with the Cirrus G7 simulator and other integrated flight-deck lessons.

PFD — Primary Flight DisplayPrimary attitude, airspeed, altitude, vertical speed, heading, and flight-guidance information.
MFD — Multi-Function DisplayMaps, engine/system information, traffic, weather, flight-plan information, and other situational data.
GTC — Touchscreen ControllerTouchscreen interface used to enter and control flight-plan, communications, transponder, and system functions.
Flight DirectorCommand cues that show the pitch and bank required to satisfy selected guidance modes.
AutopilotAutomatic flight-control system. Students should always identify which modes are armed or active before predicting what the system will do.
Engine IndicationsPower, RPM, fuel, temperature, pressure, and other engine/system parameters used to assess operating condition.

Primary scan questions

  1. What is the aircraft attitude?
  2. What is the airspeed doing?
  3. What is the altitude/vertical trend?
  4. What heading or track is being flown?
  5. Which flight-director/autopilot modes are active?
  6. Are engine/system indications normal?

Automation discipline

Automation should reduce workload without reducing awareness. Before selecting a mode, identify the desired aircraft behavior, select the control, then verify the mode annunciation and aircraft response.

Select → Verify → Monitor. If the aircraft does something unexpected, return attention to basic aircraft control first.
Atmosphere & Decision Making

Aviation weather reference

Weather products

METARObserved weather at an aerodrome.
TAFForecast weather for a terminal area.
ATISRecorded terminal information including weather and runway details.
AWOS / ASOSAutomated surface weather observations.
NOTAMTime-sensitive operational information that may affect a flight.

Wind language

Wind is described by the direction from which it is blowing. A runway aligned more closely with the wind reduces the crosswind component.

Headwind Component parallel to the runway/track.
Crosswind Component perpendicular to the runway/track.

Pressure & temperature

Air density changes with pressure, temperature, and altitude. Lower density generally reduces aerodynamic and engine/propeller performance.

High elevation, high temperature, and lower pressure can combine to produce high density altitude.

Hazards to recognize

  • Low visibility and ceilings
  • Thunderstorms and convective weather
  • Turbulence and wind shear
  • Icing conditions
  • Strong or gusty crosswinds
  • Rapid weather changes
Power & Thrust

Propulsion reference

Piston-engine terms

  • RPM: rotational speed.
  • MAP: manifold absolute pressure; a power indication on many piston aircraft.
  • EGT: exhaust gas temperature.
  • CHT: cylinder head temperature.
  • Mixture: fuel-to-air mixture delivered to the engine.

Propeller fundamentals

A propeller is a rotating airfoil. Blade angle, rotational speed, forward speed, air density, and engine power all affect thrust and efficiency.

Think of each propeller blade as a wing moving through a helical path.

Jet propulsion concept

Gas-turbine engines compress incoming air, add energy through combustion, and accelerate the flow through the turbine/nozzle system. Thrust follows from the change in momentum of the airflow.

Rocket propulsion concept

Rocket engines carry both fuel and oxidizer, allowing operation without atmospheric oxygen. Thrust is produced by accelerating exhaust mass through the nozzle.

Integrated Aircraft

Aircraft systems reference

Control

Primary Flight Controls

Ailerons control roll, elevator/stabilator controls pitch, and rudder controls yaw.

Configuration

Secondary Controls

Flaps, trim, spoilers, and other devices modify lift, drag, control force, or configuration.

Energy

Electrical System

Battery, alternator/generator, buses, circuit protection, loads, and emergency/essential power architecture.

Fuel

Fuel System

Storage, venting, selection, delivery, quantity indication, pumps, and engine-feed architecture.

Structure

Airframe

Fuselage, wing, empennage, control surfaces, landing gear, load paths, and structural design tradeoffs.

Ground

Landing Gear & Brakes

Ground support, steering, braking, shock absorption, and energy dissipation during landing and taxi.

Awareness

Pitot-Static System

Pressure sources used to support airspeed, altitude, and vertical-speed indications.

Safety

Emergency Systems

ELT and aircraft-specific emergency equipment, checklists, redundancy, and system isolation concepts.

Spaceflight

Space systems quick reference

Orbit families

LEOLow Earth Orbit; used by many crewed spacecraft, imaging satellites, and large constellations.
MEOMedium Earth Orbit; includes important navigation-satellite regimes.
GEOGeostationary Earth Orbit; equatorial orbit matching Earth's rotation period.
PolarHigh-inclination orbit that passes near the poles and can provide broad Earth coverage over time.

Spacecraft subsystems

  • Structure and mechanisms
  • Electrical power
  • Thermal control
  • Command and data handling
  • Communications
  • Guidance, navigation, and control
  • Propulsion / reaction control
  • Payload

Attitude vs. orbit

Attitude describes spacecraft orientation. Orbit describes its trajectory around a body. Reaction wheels, control moment gyros, magnetic torquers, and thrusters are examples of attitude-control technologies.

Mission architecture

Professional aerospace design treats a mission as an integrated system: requirements, launch, spacecraft, ground segment, communications, operations, payload, risk, cost, and verification all interact.

Classroom Quick Reference

Aerospace & Flight Acronym Guide

Use the searchable glossary above online, or print this page when you need a paper reference during class. The glossary is intentionally written in short technical language so it works as both a study tool and a desk reference.

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