Glossary
Space flight involves a lot of technical terms and acronyms. This glossary gives an expansion or brief description of many of those most likely to occur.
- AEA
- Abort electronics assembly
- AGS
- Abort guidance system
- ALSCC
- Apollo lunar surface closeup camera
- ALSD
- Apollo lunar surface drill
- ALSEP
- Apollo lunar surface experiments package
- AOS
- Acquisition of signal
- AOT
- Alinement optical telescope
- APS
- Auxiliary propulsion system (S-IVB)/Ascent propulsion system (LM)
- ARIA
- Apollo Range Instrumentation Aircraft
- ARS
- Atmosphere revitalization system
- BECO
- Booster Engine Cut-Off
- BEF
- Blunt end forward
- BMAG
- Body Mounted Attitude Gyroscope
- CAL
- Calibration angle
- CCGE
- Cold cathode gage experiment
- CCIG
- Cold cathode ion gage
- CDH
- Constant delta altitude (height)
- CDU
- Control data unit
- CM
- Command module
- CMC
- Command module computer
- COAS
- Crew optical alinement sight
- COI
- Contingency Orbit Injection
- CP
- Control point
- CPCB
- Crew Procedures Control Board
- CPLEE
- Charged particle lunar environment experiment
- CSC
- Contingency sample collection
- CSI
- Coelliptic sequence initiation
- CSM
- Command and service module
- CWEA
- Caution and warning electronics assembly
- DAC
- Data acquisition camera
- DAP
- Digital autopilot
- DEDA
- Data entry and display assembly
- DET
- Digital event timer
- DOI
- Descent orbit insertion
- DPS
- Descent propulsion system
- DSE
- Data storage equipment
- DSEA
- Data storage equipment assembly
- DSKY
- Display and keyboard
- DTO
- Detailed test objective
- Drogue
- Drogue parachute
- A parachute fired before the main parachute, to gain control of the spacecraft after re-entry, providing stability and slowing descent.
- ECS
- Environmental control system
- EDS
- Emergency detection system
- The emergency detection system monitored the flight vehicle during the early stages of the launch. It could trigger an automatic abort in situations where the flight crew could not be expected to react quickly enough to ensure a successful escape from the booster.
- EECOM
- Electrical, Environmental and Consumables Manager
- EI
- Entry interface
- EMI
- Extravehicular mobility unit
- EMS
- Entry monitor system
- EPS
- Electrical power system
- ETB
- Equipment transfer bag
- EVA
- Extravehicular activity
- EVT
- Extravehicular transfer
- FAO
- Flight Activities Officer
- FDAI
- Flight director attitude indicator
- FIDO
- Flight Dynamics Officer
- FM
- Frequency Modulation
- G&N
- Guidance and Navigation
- GDC
- Gyro display coupler
- GET
- Ground elapsed time
- GETI
- Ground elapsed time of ignition
- GNC
- Guidance, Navigation, and Controls System Engineer
- GUIDO
- Guidance Officer
- HA
- Apogee altitude
- HFE
- Heat flow experiment
- HGA
- High gain antenna
- HP
- Perigee altitude
- HTC
- Handtool carrier
- ICDU
- Inertial Coupling Data Unit
- IMU
- Inertial measurement unit
- INCO
- Integrated Communications Officer
- IP
- Initial point
- ISA
- Interim stowage assembly
- IU
- Instrument unit
- IVT
- Intravehicular transfer
- JOD
- Junior Officer of the Day
- LAD
- Lunar atmosphere detector
- LCG
- Liquid cooled garment
- LEB
- Lower equipment bay
- LEC
- Lunar equipment conveyor
- LGC
- Lunar module guidance computer
- LM
- Lunar module
- LOI
- Lunar orbit insertion
- LOPC
- Lunar orbit plane change
- LOS
- Loss of signal (or line or sight)
- LPD
- Landing point designator
- LTC
- Lunar topographic camera
- M&O
- Maintenance and Operations
- MAX Q
- Maximum dynamic pressure
- The point at which aerodynamic stress on a spacecraft in atmospheric flight is maximized.
- MC&W
- Master Caution & Warning
- MCC
- Mission Control Center/midcourse correction
- MESA
- Modular equipment stowage assembly
- MILA
- Meritt Island Launch Area tracking station
- MSFN
- Manned Space Flight Network
- MTVC
- Manual thrust vector control
- NOUN 01
- Specify machine address (fractional)
- NOUN 07
- Set/reset values
- NOUN 09
- Last three program alarms
- NOUN 14
- Desired Delta-V
- NOUN 17
- Astronaut total attitude
- NOUN 18
- Auto maneuvre ball angles
- NOUN 20
- ICDUs
- NOUN 21
- PIPA (accelerometer) values
- NOUN 22
- New ICDU angles
- NOUN 23
- Number of passes, time to burn, burn delta-V.
- NOUN 25
- Perform checklist action
- NOUN 29
- Launch azimuth
- NOUN 33
- Time of ignition
- NOUN 34
- Time of next program event
- NOUN 42
- Apogee, perigee and DELTA-V
- NOUN 44
- Height (nautical miles)
- NOUN 46
- Autopilot configuration
- NOUN 47
- Vehicle weights
- NOUN 48
- Gimbal pitch and roll trim
- NOUN 51
- Time to event (IG or ECO)
- NOUN 60
- Forward velocity (LM)
- NOUN 61
- Impact latitude/longitude
- NOUN 62
- Velocity information during launch and landing
- NOUN 63
- Absolute velocity (LM)
- NOUN 65
- Sampled AGC time
- NOUN 67
- Range to target (CSM)
- NOUN 70
- AOT detent and star code
- NOUN 72
- Rendezvous radar shaft and trunnion (LM)
- NOUN 81
- Delta V: Change in velocity (fps)
- NOUN 87
- Mark data shaft and trunnion
- NOUN 88
- Half-unit sun or planet vector
- NOUN 89
- Landmark lattitude and longitude
- NOUN 91
- OCDU shaft and trunnion (CSM)
- NOUN 93
- Delta gyro angles
- NOUN 99
- W-matrix position
- OPS
- Oxygen purge system
- ORDEAL
- Orbital rate display earth and lunar
- P00
- Idle
- P01
- Pre-launch or service: initialization
- P02
- Pre-launch or service: gyro compassing
- P11
- Launch control
- P21
- Ground track determination
- P22
- Optics update
- P23
- Cislunar navigation
- P27
- CMC update
- P30
- External Delta-V
- P33
- Corrective combination maneuvre (NCC)
- P37
- Rendezvous final phase
- P40
- SPS thrusting
- P41
- RCS thrusting
- P47
- Thrust monitor
- P51
- Read guidance platform orientation
- P52
- Guidance platform realignment
- P53
- Back-up IMU orientation determination
- P61
- Entry preparation
- P62
- Entry CM/SM separation and pre-entry maneuvre
- P63
- Entry intitialization
- P65
- Entry up control
- PAD
- Voice update
- PC
- Pericynthian
- PCM
- Pulse Code Modulation
- PDI
- Powered descent initiation
- PGA
- Pressure garment assembly
- PGNCS
- Primary guidance, navigation, and control system (CM)
- PGNS
- Primary guidance and navigation system (LM)
- PIPA
- Pulsed integrating pendulous accelerometer
- PLSS
- Portable life support system
- PRD
- Personal radiation dosimeter
- PSE
- Passive seismic experiment
- PTC
- Passive thermal control
- PU
- Propellant Utilization
- RCS
- Reaction control system
- RCU
- Remote control unit
- REFSMMAT
- Reference to stable member matrix
- REV
- Revolution
- RLS
- Radius of landing site
- RTC
- Real-Time Command
- RTG
- Radioisotope thermoelectric generator
- S-IVB
- Saturn V Third Stage
- SCE
- Signal conditioning equipment
- SCS
- Stabilization control system
- SECO
- Sustainer Engine Cut-Off
- SECS
- Sequential events control system
- SEF
- Sharp end forward
- SEP
- Separation
- SIDE
- Suprathermal ion detector experiment
- SLA
- SM/LM adapter
- SM
- Service module
- SNAP
- Systems for nuclear auxiliary power
- SPS
- Service propulsion system
- SRC
- Sample return container
- SWC
- Solar wind composition
- SWE
- Solar wind experiment
- TCA
- Time of Closest Approach
- TEC
- Transearth coast
- TEI
- Transearth injection
- TELMU
- Telemetry, Electrical, EVA Mobility Unit Officer (LM's EECOM)
- TLC
- Translunar coast
- TLI
- Translunar injection
- TLM
- Telemetry
- TPF
- Terminal phase final
- TPI
- Terminal phase initiation
- TSB
- Temporary stowage bag
- TTCA
- Thrust/Translation Controller Assembly
- TVC
- Thrust vector control
- Tig
- Time of ignition
- UHT
- Universal handtool
- VERB 01
- Display contents of erasable memory location
- VERB 03
- Display register 1
- VERB 04
- Display register 1 and 2
- VERB 05
- Display register 1, 2 and 3
- VERB 06
- Display data in decimal
- VERB 07
- Display double-precision data
- VERB 11
- Monitor register 1
- VERB 12
- Monitor register 2
- VERB 13
- Monitor register 3
- VERB 14
- Monitor register 1 and 2
- VERB 15
- Monitor register 1, 2 and 3
- VERB 16
- Monitor data in decimal
- VERB 17
- Monitor double-precision data
- VERB 21
- Load register 1
- VERB 22
- Load register 2
- VERB 23
- Load register 3
- VERB 24
- Load register 1 and 2
- VERB 25
- Load register 1, 2 and 3
- VERB 31
- Bank display
- VERB 33
- Proceed without data
- VERB 34
- Terminate
- VERB 36
- Fresh start
- VERB 37
- Change major mode to
- VERB 40
- Zero CDU registers
- VERB 41
- Coarse align IMU
- VERB 42
- Fine align IMU
- VERB 43
- Lock IMU
- VERB 44
- Terminate Rendezvous Radar Continuous Designate
- VERB 45
- Set IMU ENTRY
- VERB 46
- Establish G&C Control
- VERB 47
- Move LM state vector into CM state vector
- VERB 48
- Request DAP data load
- VERB 49
- Request Crew Defined Maneuver routine
- VERB 51
- Please mark
- VERB 52
- Mark reject
- VERB 53
- Free
- VERB 54
- Pulse torque gyros
- VERB 55
- Increment LGC time (decimal)
- VERB 56
- Perform bank sum
- VERB 62
- Display total attitude errors with respect to new ICDU angles
- VERB 64
- Request S-Band Antenna Routine
- VERB 65
- Disable U and V jet firings during DPS burns
- VERB 66
- Move state vector to other vehicle
- VERB 67
- Calculate maximum declination and time of arrival
- VERB 69
- Cause restart
- VERB 73
- Return to Earth aim point update
- VERB 74
- Initialize erasable dump via downlink
- VERB 75
- Manual lift-off
- VERB 76
- Minimum Impulse Command mode
- VERB 77
- Rate Command and Attitude Hold mode
- VERB 79
- Request Lunar Landmark Selection Routine (CSM)
- VERB 82
- Request orbital parameter display
- VERB 83
- Request rendezvous parameter display
- VERB 89
- Request rendezvous final attitude
- VERB 96
- Terminate integration and go to P00
- ΔV
- Delta V (change in velocity)