franchise-star-trek-tng-technical-manual1
franchise-star-trek-tng-technical-manual1 franchise-star-trek-tng-technical-manual1
3.11 ENGINEERING3.11.1 Engineering aft station panelThe Engineering systems monitor duplicates in simplifiedform the Chief Engineer's primary status displays from MainEngineering. These displays include the warp propulsionsystem, impulse propulsion system, and related subsystems.The purpose of this station is to permit the Chief Engineer tomaintain supervision over engineering systems while on thebridge. This is particularly critical during Alert situations thatmay require the Chief Engineer's presence on the bridgewhile simultaneously requiring that officer to maintain a closewatch over the status of key systems. During most routineCruise Mode operations, bridge monitoring of these systemsis the responsibility of the Flight Control Officer and the OperationsManager.Although this station is normally configured for passivesystems status display, priority access by the Chief Engineeror senior staff can provide full control of virtually all engineeringsystems.The console is linked to the engineering systems throughthe bridge's dedicated optical data network (ODN) trunks, butan additional measure of redundancy is provided by dedicatedoptical hardlines, which permit direct control of keysystems in the event of major control systems failure. In sucha case, the main computer cores would be assumed to beunavailable or unreliable, so manual control of systems wouldbe enabled with support from the bridge Engineering subprocessor.In Full Enable Mode, this station is capable of individuallyaddressing each control and servo device (as well as Engineeringcommand software) in all propulsion systems (subjecttosafety restrictions), giving the Chief Engineer enormousflexibility to reconfigure system operations in response tounforeseen situations.This station is normally unattended, except by the ChiefEngineer or key Engineering personnel, although most of itsdisplays are readily accessible to both Ops and Conn throughtheir respective control programs.3.12 GUIDANCE AND NAVIGATIONCritical to the flight of any vehicle through interstellarspace are the concepts of guidance and navigation. Theseinvolve the ability to control spacecraft motions, to determinethe locations of specific points in three and four dimensions,and to allow the spacecraft to follow safe paths between thosepoints.The theater of operation for the USS Enterprise takes itthrough both known and unknown regions of the Milky Waygalaxy. While the problems of interstellar navigation havebeen well-defined for over two hundred years, navigatingabout this celestial whirlpool, especially at warp velocities, stillrequires the precise orchestration of computers, sensors,active high-energy deflecting devices, and crew decisionmakingabilities.SPACECRAFT GUIDANCEThe attitude and translational control of the USS Enterpriserelative to the surrounding space involves numeroussystems aboard both the Saucer Module and Battle Section.As the starship maneuvers within the volume of the galaxy,the main computers attempt to calculate the location of thespacecraft to a precision of 10 kilometers at sublight, and 100kilometers during warp flight. The subject of velocity isimportant in these discussions, as different sensing and
3.12.1 Galactic navigational reference systemFar infraredscannersSubspacefield sensorsLong-rangearrayPulsar/quasarcountersStellar pairimagersFed TimebaseBeaconsInertial dampersensors _\OpticalWarp drivesystemsIImpulse drivesystemsLateralsensor arraysOthersensorsGravitonNavigationsensorsreceiversOnboardtimebaseAccelerometersIInertial Baseline^*Input System _^1ReactionControl SysTPropulsionsys inputsFlightControllercomputation methods are employed for each flight regime.During extremely slow in-system maneuvering at sublightvelocity, the main computers, coupled with the reaction controlthrusters, are capable of resolving spacecraft motions to0.05 seconds of arc in axial rotation, and 0.5 meters of singleimpulsetranslation. During terminal docking maneuvers,accuracies of up to 2.75 cm can be maintained. Changes inspacecraft direction of flight, relative to its own center of mass,is measured in bearings, as shown in 3.4.2.Internal sensing devices such as accelerometers, opticalgyros, and velocity vector processors, are grouped within theinertial baseline input system, or IBIS. The IBIS is in realtimecontact with the structural integrity field and inertial dampingsystems, which provide compensating factors to adjustapparent internal sensor values, allowing them to be comparedwith externally derived readings. The IBIS also providesa continuous feedback loop used by the reaction controlsystem to verify propulsion inputs.EXTERNAL SENSORSThe major external sensors employed at sublight includestellar graviton detectors, stellar pair coordinate imagers,pulsar/quasar counters, far infrared scanners, and FederationTimebase Beacon (FTB) receivers. These devices alsocommunicate with the structural integrity field and inertialdamping field processors, inertial sensors, and main computersto obtain an adjusted awareness of the ship's location.The wide range of external sensors make it possible to obtainthe greatest number of readings under many different conditions.The standard external sensor pallet has been designedto insure that coarse position calculations can be made underadverse operating conditions: e.g., magnetic fields, denseinterstellar dust, and stellar flares.While the network of FTBs operate on subspace frequenciesto facilitate position calculations at warp, vehicles atsublight speed can, in fact, obtain more precise positioningdata than ships at warp. In the absence of clear FTB signals,onboard timebase processors continue computing distanceand velocity for later synchronization when FTB pulses areonce again detected.Guidance of the USS Enterprise athigher sublight velocitiescouples the impulse engines with those systems alreadymentioned. External sensor readings, distorted by higherrelativistic speeds, necessitate adjustment by the guidanceand navigation (G&N) subprocessors in order to accuratelycompute ship location and provide proper control inputs to theimpulse engines. Extended travel at high sublight speed is nota preferred mode of travel for Federation vessels, due to theundesired time-dilation effects, but may be required occasionallyif warp systems are unavailable.In the Galaxy class starship, ongoing G&N system researchtasks are handled by a mixed consultation crew oftwelve Tursiops truncatus and T. truncatus gilli, Atlantic and
- Page 2 and 3: CONTENTSINTRODUCTION BYGENE RODDENB
- Page 4 and 5: 1.1 MISSION OBJECTIVES FOR GALAXY C
- Page 6 and 7: 1.2 DESIGN LINEAGEENVIRONMENT/CREW
- Page 8 and 9: 1.3 GENERAL OVERVIEW1.3 GENERAL OVE
- Page 10 and 11: sionally to monitor their operation
- Page 12 and 13: Transporter emitter (typ.)Saucer Mo
- Page 14 and 15: Observation lounge •Main Shuttleb
- Page 16 and 17: 1.3.10 USS Enterprise forward dorsa
- Page 18 and 19: 1.4.2 Structural frame assembly at
- Page 20 and 21: 1.4 CONSTRUCTION CHRONOLOGYprogramm
- Page 22 and 23: 2.1 MAIN SKELETAL STRUCTURE2.1.2 St
- Page 24 and 25: The first group of two digits refer
- Page 26 and 27: 2.4 STRUCTURAL INTEGRITY FIELD SYST
- Page 28 and 29: 2.6 EMERGENCY PROCEDURES IN SIF/IDF
- Page 30 and 31: 2.7 SAUCER MUOULE SEPARATIUN SYSTEM
- Page 32 and 33: 2.7 SAUCER MODULE SEPARATION SYSTEM
- Page 34 and 35: 3.1 MAIN BRIDGEmain viewer display
- Page 36 and 37: 3.2 BRIDGE OPERATIONS 3.3 BASIC CON
- Page 38 and 39: 3.4 FLIGHT CONTROL (CONN)3.4 FLIGHT
- Page 40 and 41: 3.4.3 Headings can be measured rela
- Page 42 and 43: 3.6 TACTICALThe Main Bridge station
- Page 44 and 45: necessary overriding ongoing scienc
- Page 48 and 49: Pacific bottlenose dolphins, respec
- Page 50 and 51: 3.14 BATTLE BRIDGE 3.15 MAIN ENGINE
- Page 52 and 53: 4.0 COMPUTER SYSTEMS4.1 COMPUTER SY
- Page 54 and 55: 4.1 COMPUTER SYSTEM4.1.3 Optical da
- Page 56 and 57: PADD memory limitations and the rel
- Page 58 and 59: A subspace field of one thousand mi
- Page 60 and 61: 5.2 MATTER/ANTIMATTER REACTION ASSE
- Page 62 and 63: .Z HUM 11 tli/flhl I IMA 11 tii KtA
- Page 64 and 65: 5.2 MATTER/ANTIMATTER ¥highly comp
- Page 66 and 67: 5.3 WARP FIELD NACELLES5.3 WARP FIE
- Page 68 and 69: and is constructed from a core of d
- Page 70 and 71: 5.4 ANTIMATTER STORAGE AND TRANSFER
- Page 72 and 73: 5.5 WARP PROPULSION SYSTEM FUEL SUP
- Page 74 and 75: compact set of six coils designed t
- Page 76 and 77: iT.ll.Mlii iiiirm 1'iirninil nunNUU
- Page 78 and 79: 6.0 IMPULSE PROPULSION SYSTEMSG.1 I
- Page 80 and 81: UliU'lithese modules may be channel
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- Page 84 and 85: 7.0 UTILITIES ARID AUXILIARY SYSTEM
- Page 86 and 87: 7.1 UTILITIESto emergency environme
- Page 88 and 89: 7.3 REACTION CONTROL SYSTEMbe deplo
- Page 90 and 91: 7.4 NAVIGATIONAL DEFLECTOR7.4 NAVIG
- Page 92 and 93: 7.5 TRACTOR BEAMS7.5 TRACTOR REAMS7
- Page 94 and 95: 7.6 REPLICATOR SYSTEMSgeometry tran
3.11 ENGINEERING3.11.1 Engineering aft station panelThe Engineering systems monitor duplicates in simplifiedform the Chief Engineer's primary status displays from MainEngineering. These displays include the warp propulsionsystem, impulse propulsion system, and related subsystems.The purpose of this station is to permit the Chief Engineer tomaintain supervision over engineering systems while on thebridge. This is particularly critical during Alert situations thatmay require the Chief Engineer's presence on the bridgewhile simultaneously requiring that officer to maintain a closewatch over the status of key systems. During most routineCruise Mode operations, bridge monitoring of these systemsis the responsibility of the Flight Control Officer and the OperationsManager.Although this station is normally configured for passivesystems status display, priority access by the Chief Engineeror senior staff can provide full control of virtually all engineeringsystems.The console is linked to the engineering systems throughthe bridge's dedicated optical data network (ODN) trunks, butan additional measure of redundancy is provided by dedicatedoptical hardlines, which permit direct control of keysystems in the event of major control systems failure. In sucha case, the main computer cores would be assumed to beunavailable or unreliable, so manual control of systems wouldbe enabled with support from the bridge Engineering subprocessor.In Full Enable Mode, this station is capable of individuallyaddressing each control and servo device (as well as Engineeringcommand software) in all propulsion systems (subjecttosafety restrictions), giving the Chief Engineer enormousflexibility to reconfigure system operations in response tounforeseen situations.This station is normally unattended, except by the ChiefEngineer or key Engineering personnel, although most of itsdisplays are readily accessible to both Ops and Conn throughtheir respective control programs.3.12 GUIDANCE AND NAVIGATIONCritical to the flight of any vehicle through interstellarspace are the concepts of guidance and navigation. Theseinvolve the ability to control spacecraft motions, to determinethe locations of specific points in three and four dimensions,and to allow the spacecraft to follow safe paths between thosepoints.The theater of operation for the USS Enterprise takes itthrough both known and unknown regions of the Milky Waygalaxy. While the problems of interstellar navigation havebeen well-defined for over two hundred years, navigatingabout this celestial whirlpool, especially at warp velocities, stillrequires the precise orchestration of computers, sensors,active high-energy deflecting devices, and crew decisionmakingabilities.SPACECRAFT GUIDANCEThe attitude and translational control of the USS Enterpriserelative to the surrounding space involves numeroussystems aboard both the Saucer Module and Battle Section.As the <strong>star</strong>ship maneuvers within the volume of the galaxy,the main computers attempt to calculate the location of thespacecraft to a precision of 10 kilometers at sublight, and 100kilometers during warp flight. The subject of velocity isimportant in these discussions, as different sensing and