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Dictionary
Martin Sundhaug edited this page Jan 2, 2019
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| Word | Description |
|---|---|
| A | One of four Omni Directional Control Antennas |
| ACA | Attitude Control Assembly |
| ACQ | Acquisition |
| AELD | Ascent Engine Latching Device |
| AGC | Apollo Guidance Computer |
| AGC | Abort Guidance System |
| ALIGN | Alignment |
| ALM | Alarm |
| ALT | Altimeter |
| AM | Ammeter or Amplitude Modulation |
| AMP | Ampere or Amplifier |
| AMP-HR | Ampere Hour |
| ANNUN-NUM | Annunciator/Numerics |
| ANT | Antenna |
| AOS | Acquisition Of Signal or Acquisition Of Site |
| AOT | Alignment Optical Telescope |
| AP | Alpha Particle (spectrometer) |
| APS | Auxiliary Propulsion System (S-IVB) or Ascent Propulsion System (LM) |
| ARIA | Apollo Range Instrumentation Aircraft |
| ARM | Armed |
| ARS | Atmosphere Revitalization System |
| ASA | Abort Sensor Assembly |
| ASAP | As Soon As Possible |
| ASC | Ascent |
| ASR | Area Surveillance Radar |
| ASSY | Assembly |
| ATCA | Attitude & Translation Control Assembly |
| ATT | Attitude |
| AUTO | Automatic |
| AUX | Auxiliary |
| AVAIL | Available |
| AZ | Azimuth |
| B | One of Four Omni Directional Control Antennas, known as Omni Bravo |
| BAT | Battery |
| BATT | Battery |
| BCN | Beacon |
| BEF | Blunt End Forward |
| BIP | Bipropellant |
| BMAG | Body Mounted Attitude Gyros |
| BP | Barber Pole |
| BPS | Bits Per Second or Bits Per Sample |
| BTH | Both |
| BUSS | Biomedical Urine Sampling System |
| C | One of Four Omni Directional Control Antennas, known as Omni Charlie |
| C-BND | C-Band |
| CAL | Calibrate or Calibration |
| CALC | Calculate or Calculated |
| CAPCOM | Spacecraft Communicator |
| CB | Circuit Breaker |
| CDU | Coupling Data Units |
| CES | Control Electronics Section |
| CG | Center of Gravity |
| CL | Close |
| CLSD | Closed |
| CM | Command Module |
| CM RCS | Command Module Reaction Control System |
| CMD | Command |
| CMDED | Commanded |
| CMP | Command Module Pilot |
| CNTL | Control |
| CO2 | Carbon Dioxide |
| COAS | Crewman Optical Alignment Sight |
| COAS | Crewman Optical Alignment Sight |
| COMM | Communications |
| COND | Condition, Conditioning or Conditioner |
| CONFIG | Configuration |
| CONT | Continue |
| COOL | Coolant |
| CP | Command Pilot or Control Point |
| CPS | Cycles Per Second |
| CRSFD | Crossfeed |
| CRYO | Cryogenic |
| CSI | Coelliptic Sequence Initiation |
| CSM | Command/Service Module |
| CSS | Computer Subsystem |
| CWS | Caution and Warning System |
| D | Downward Thrusting RCS Engine or One of Four Omni Directional Control Antennas, known as Omni Delta |
| DAP | Digital Autopilot |
| DB | Decibel |
| DC | Direct Current |
| DECA | Descent Engine Control Assembly |
| DECR | Decrease |
| DEDA | Data Entry and Display Assembly |
| DEG | Degree |
| DELTA H | Height Difference |
| DELTA P | Pressure Difference |
| DELTA T | Time Difference |
| DELTA V | Change in Velocity |
| DESC | Descent |
| DET | Detent or Detector or Digital Event Timer |
| DF | Direction Finding |
| DFI | Development Flight Instrumentation |
| DIFF | Difference or Differential |
| DIG | Digital |
| DIR | Direct |
| DISCH | Discharge |
| DISP | Display |
| DIV | Diverter |
| DLAY | Delay |
| DOI | Descent Orbit Insertion |
| DPLY | Deploy or Deployed |
| DPS | Descent Propulsion System |
| DR | Dead Reckoning or Descent Rate |
| DSE | Data Storage Equipment |
| DSEA | Data Storage Electronics Assembly |
| DSKY | DiSplayKeYboard |
| E-DUMP | Erasable-Memory Download |
| E-MOD | Erasable-Memory Download |
| ECA | Electronics Control Assembly |
| ECOM | Electronics Communications |
| ED | Explosive Device |
| EDS | Emergency Detection System |
| ELS | Earth Landing System |
| EMI | Electromagnetic Interference |
| EMS | Entry Monitoring System |
| Ephemeris | gives the positions of naturally occurring astronomical objects as well as artificial satellites in the sky at a given time or times |
| EVA | Extravehicular Activity |
| F | Fahrenheit or Forward Thrusting RCS Engine |
| FAIL | Failure |
| FDAI | Flight Director Attitude Indicator |
| FITH | Fire In The Hole |
| FL | Flag |
| FM | Frequency Modulation |
| FP | Flight Progress |
| FRAG | Fragment |
| FREQ | Frequency |
| FWD | Forward |
| G&C | Guidance and Control |
| G&N | Guidance and Navigation |
| GASTA | Gimbal Angle Sequencing Transformation Assembly |
| GCA | Ground Controlled Approach |
| GDA | Gimbal Drive Actuator |
| GDC | Gyro Display Coupler |
| GET | Ground-Elapsed Time |
| GETI | Ground-Elapsed Time of Ignition |
| GLY | Glycol |
| GMBL | Gimbal |
| GNCS | Guidance, Navigation and Control System |
| GND | Ground |
| GOX | Gaseous Oxygen |
| GPI | Gimbal Position Indicator |
| GUID | Guidance |
| H-dot | Time derivative of height (H); Descent Rate or Ascent Rate. In mathematical notation, the time (t) derivative of height (H) can be written as dH/dt or as Ḣ |
| H/H | Altitude or Altitude Rate |
| H/X | Heat Exchanger |
| H2O | Water |
| HBR | High Bit Rate |
| HE | Helium |
| HGA | High Gain Antenna |
| HI | High |
| HL | High Level |
| HLD | Hold |
| HSD | High-Speed Data |
| HV | High Voltage |
| HVR | Hover |
| ICS | Intercommunications System |
| ID | Identification |
| IFR | Instrument Flight Rules |
| IG | Inner Gimbal |
| IGA | Inner Gimbal Angle |
| IGN | Ignition |
| ILS | Instrument Landing System |
| IMU | Inertial Measurement Unit |
| IMU | Inertial Measurement Unit |
| IN | Inlet |
| INCO | Instrumentation and Communications Officer |
| INCR | Increase |
| INJ | Injector |
| INST | Instrumentation |
| INTEG | Integrity |
| INVTR | Inverter |
| IP | Initial Point |
| IPI | Integrated Position Indicator |
| IRIG | Inertial Rate Integrating Gyro |
| ISOL | Isolation |
| ISS | Inertial Subsystem |
| JETT | Jettison |
| KEY REL | Key Release |
| LAT | Latitude or Lateral |
| LBR | Low Bit Rate |
| LCRU | Lunar Communications Relay Unit |
| LDG | Landing |
| LGC | Lunar Module Guidance Computer |
| LIM | Limit or Limits |
| LiOH | Lithium Hydroxide |
| LM | Lunar Module |
| LMP | LM Mission Programmer or Lunar Module Pilot |
| LO | Low |
| LOI | Lunar Orbit Insertion |
| LONG | Longitude |
| LOPC | Lunar Orbit Plane Change |
| LOS | Loss Of Signal or Loss Of Site |
| LPD | Landing Point Designator |
| LR | Landing Radar |
| LSB | Least Significant Bit |
| LV | Low Voltage |
| LVL | Level |
| MA | Master Alarm |
| MAG | Magazine |
| MAL | Malfunction |
| MAN | Manual or Manifold |
| MAP | Message Acceptance Pulse |
| MAX | Maximum |
| MCC | Mission Control Center or MidCourse Correction |
| MCCH | Mission Control Center Houston |
| MDC | Main Display Console |
| MET | Mission Elapsed Time, Mission Event Timer |
| MFC | Main Feeder Contactor |
| MG | Middle Gimbal |
| MGA | Middle Gimbal Angle |
| MIN | Minimum |
| MOCR | Mission Operations Control Room |
| MPX | Multiplex |
| MSB | Most Significant Bit |
| MSC | Manned Spacecraft Center |
| MSFN | Manned Space Flight Network |
| MSOB | Manned Spacecraft Operations Building |
| MTR | Meter |
| MTVC | Manual Thrust Vector Control |
| N/A | Not Applicable |
| N204 | Nitrogen Tetroxide |
| NAV | Navigation |
| NB | Narrow Band |
| NORM | Normal |
| O2 | Oxygen |
| OB | OnBoard |
| OBC | On-Board Computer |
| OG | Outer Gimbal |
| OGA | Outer Gimbal Angle |
| OPN | Open |
| OPR | Operate |
| OPS | Oxygen Purge System |
| ORDEAL | Orbital Rate Display Earth And Lunar |
| OSS | Optics Subsystem |
| OUT | Outlet or Output |
| OVR | Over |
| OVRD | Override |
| OX | Oxidizer or Oxygen |
| P00 | Program Zero-Zero |
| P22 | LM computer program that uses the rendezvous radar to track the Command Module |
| PA | Power Amplifier |
| PAD | Preliminary Advisory Data |
| PART | Partial |
| PCA | Program Coupler Assembly |
| PCM | Pulse Code Modulation |
| PCT | Per Cent |
| PDI | Powered Descent Initiation |
| PFS | Per Cent Full Scale |
| PGNCS | Primary Guidance Navigation and Control System |
| PGNS | Primary Guidance and Navigation System |
| PIA | Pre-Installation Acceptance |
| PIPA | Pulse Integrated Pendulous Accelerometers |
| PLSD | Pulsed |
| PLSS | Portable Life Support System |
| PM | Phase Modulation |
| PM1/NB | Phase Modulator 1/Narrowband |
| PM1/WB | Phase Modulator 1/Wideband |
| PMQD | Propellant Quantity Measuring Device |
| PNLS | Panels |
| PO | Power Output |
| POS | Position |
| PRA | Program Reader Assembly |
| PRD | Personal Radiation Dosimeter |
| PRELIM | Preliminary |
| PRESS | Pressure |
| PRIM | Primary |
| PRO | Proceed |
| PROG | Program |
| PROP | Propellant or Propulsion |
| PSIA | Pounds Per Square Inch Absolute |
| PSID | Pounds Per Square Inch Differential |
| PTA | Pulsed Torque Assembly |
| PTC | Passive Thermal Control |
| PTT | Push-To-Talk |
| PUGS | Propellant Utilization and Gauging Subsystem |
| PVR | Percent Voltage Reference |
| PWM | Pulse Width Modulation |
| PWR | Power |
| PYRO | Pyrotechnic |
| QD | Quick Disconnect |
| QTY | Quantity |
| QUAD | Quadrant |
| R-Dot | Rate of approach; time (t) derivative of range, which can be written mathematically as dR/dt or Ṙ |
| RAD | Radiation |
| RC/OC | Reverse Current/OverCurrent |
| RCS | Reaction Control System |
| RCU | Remote Control Unit |
| RCVR | Receiver |
| REACQ | Re-acquire |
| REC | Recorder |
| RECD | Received |
| REF | Reference |
| REFSMMAT | Reference Stable Member Matrix |
| REG | Regulator |
| REL | Release |
| RET | Retract or Return |
| REV | Reverse |
| RF | Radio Frequency |
| RFLT | Reflect or Reflected |
| RGA | Rate Gyro Assembly |
| RJ/EC | Reaction Jet and Engine On-Off Control |
| RLS | Radius of Landing Site or Reference Landing Site |
| RLY | Relay |
| RNG | Range or Ranging |
| ROD | Rate of Descent |
| RR | Rendezvous Radar |
| RS | Remote Site |
| RSVR | Resolver |
| RTG | Radioisotopic Thermoelectric Generator |
| RTV | Room Temperature Vulcanizing |
| RUPT | Rupture |
| S | Sideward Thrusting RCS Engine |
| S-BND | S-Band |
| S/C | Spacecraft |
| S/O | Shut Off |
| S/S | Samples per Second |
| SBT | S-Band Transponder |
| SCE | Signal-Conditioning Equipment |
| SCS | Stabilization and Control System |
| SEC | Secondary, Second |
| SECS | Sequential Events Control Subsystem |
| SEF | Sharp End Forward |
| SEL | Select |
| SENS | Sensitivity |
| SEP | Separation, Separator |
| SEQ | Sequence |
| SET | Set or Setting |
| SHE | SuperCritical Helium |
| SIG | Signal |
| SIM | Scientific Instrument Module |
| SLA | Spacecraft Launch Adapter or SM/LM Adapter |
| SM | Service Module |
| SM RCS | Service Module Reaction Control System |
| SNAP-27 | System for Nuclear Auxiliary Power, Model 27 |
| SOL | Solenoid |
| SOV | Shut Off Valve |
| SP | Spare |
| SPEC | Specification |
| SPS | Service Propulsion System |
| ST | Static |
| STBY | Standby |
| STGE | Stage |
| STR | Strength |
| STRB | Strobe |
| SUP | Supply |
| SUSP | Suspension |
| SVO | Servo |
| SW | Switch |
| SYNCH | Synchronization |
| SYS | System |
| T/R | Transmit/Receive |
| TB | TalkBack |
| TCA | Thrust Chamber Assembly |
| TCP | Thrust Chamber Pressure |
| TCU | Television Control Unit |
| TEC | Transearth Coast |
| TEI | Transearth Injection |
| TELEMU | Telemetry |
| TEMP | Temperature |
| Tephem | Time of Ephemeris |
| THC | Translation Hand Controller |
| THROT | Throttle |
| TIG | Time of Ignition |
| TJM | Tower Jettison Motor |
| TK | Tank |
| TLC | Translunar Coast |
| TLI | Translunar Injection |
| TLM | Telemetry |
| TM | Telemetry |
| TOL | Tolerance |
| TPI | Terminal Phase Initiation |
| TRANS | Translation |
| TRUN | Trunnion |
| Trunnion | a cylindrical protrusion used as a mounting or pivoting point |
| TTCA | Thrust/Translation Controller Assembly |
| TTHR | Tether |
| TTY | Teletype or Teletypewriter |
| TVC | Thrust Vector Control |
| U | Upward Thrusting RCS Engine |
| UCTA | Urine Collection and Transfer Assembly |
| UDMX | Unsymmetrical-Dimethylhydrazine, part of the fuel for the DPS and APS |
| UHF | Ultra-High Frequency |
| V | Volt |
| V sub I | Inertial Velocity |
| VAC | Volts Alternating Current |
| VAR | Variable |
| VDC | Volts Direct Current |
| VEL | Velocity |
| VHF | Very High Frequency |
| VLV(S) | Valve(s) |
| VOX | Voice Activated Transmission |
| VPI | Valve Position Indicator |
| VR | Vector Ranging |
| VRMS | Volt Root Mean Square |
| W | Watt |
| W/B | Water Boiler |
| WB | WideBand |
| WILCO | Will Comply |
| X | Cross |
| X Axis | Vertical Axis |
| X-Pointer | Crosspointer |
| XMTR | Transmitter |
| XPNDR | Transponder |
| Y Axis | Left to Right Axis |
| Z Axis | Fore/Aft Axis |
| ΔV | Delta V |