Skip to content

Dictionary

Martin Sundhaug edited this page Jan 2, 2019 · 2 revisions
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

Clone this wiki locally