franchise-star-trek-tng-technical-manual1
franchise-star-trek-tng-technical-manual1 franchise-star-trek-tng-technical-manual1
2.4 STRUCTURAL INTEGRITY FIELD SYSTE.an 8.7 cm multiaxis tritanium truss framework, which providesadditional thermal insulation and a pass-through for fixedutility conduits.Radiation attenuation is provided by a 4.2 cm layer ofmonocrystal beryllium silicate infused with semiferrous polycarbonatewhiskers. This layer is networked with a series of2.3 cm x 0.85 cm molybdenum-jacketed conduits. Theseconduits, which occur at 130 cm intervals, serve as triphasewaveguides for the secondary structural integrity field. Conductivetritanium rods penetrate the waveguides at 10 cmintervals and transfer SIF energy into the ceramic-polymerconductive layer.The outermost hull layer is composed of a 1.6 cm sheetof AGP ablative ceramic fabric chemically bonded onto asubstrate of 0.15 cm tritanium foil. This material is formed intosegments of approximately 3.7 m 2 and is attached to theradiation attenuation layer by a series of duranium fasteners,which allows individual segments to be replaced as necessary.(Micrometeoroid erosion is kept to a minimum by thedeflector shield system, but is sufficient to warrant replacementof 30% of leading-edge segments on the average ofevery 7.2 Standard years.) Individual outer hull segments aremachined toatolerance of+0.5 mm to allow for minimum dragthrough the interstellar medium. Joints between segmentsare manufactured to a tolerance of ±0.25 mm.Also incorporated into the outermost hull layer is a seriesof superconducting molybdenum-jacketed waveguide conduitswhich serves to distribute and disperse the energy of thetactical deflector system. Selected segments of this networkalso serve as radiators for starship thermal management.2.4 STRUCTURAL INTEGRITY FIELD SYSTEMThe mechanical integrity of the physical spaceframe isaugmented by the structural integrity field (SIF) system. Thissystem provides a network of forcefield segments that compensatefor propulsive and other structural load factors thatotherwise exceed the design limits of the spaceframe. TheSIF applies forcefield energy directly to field conductiveelements within the spaceframe and increases the loadbearingcapacity of the structure.Field generation for the SIF is provided by three fieldgenerators located on Deck 11 in the Primary Hull and by twogenerators located on Deck 32 in the Secondary Hull. Eachgenerator consists of a cluster of twenty 12 MW gravitonpolarity sources feeding a pair of 250 millicochrane subspacefield distortion amplifiers. Heat dissipation on each unit isprovided by a pair of 300,000 megajoules per hour (MJ/hr)continuous-duty liquid helium coolant loops. Two backupgenerators are located in each hull, providing up to twelvehours of service at 55% of maximum rated power. Normalduty cycle on generators is thirty-six hours online, with nominaltwenty-four hours degauss and scheduled maintenancetime. Graviton polarity sources are rated for 1,500 operatinghours between routine servicing of superconductive elements.The output of each SIF generator is directed by means ofanetwork of molybdenum-jacketed triphase waveguides whichdistributes the field energy throughout the spaceframe. SIFconductivity elements are incorporated into all major structuralmembers. When energized by the SIF, the load-bearingcapacity of these conductive structural elements is increasedby up to 125,000%. Secondary feeds also provide for reinforcementof the vehicle's external shell.Cruise Mode operating rules require at least one fieldgenerator to be active at all times in each hull, although theFlight Control Officer may call for activation of a second generatorwhen extreme maneuvers are anticipated. During Alertmodes, all operational units are brought to hot standby forimmediate activation. Reduced Power Mode rules permit asingle field generator to feed the entire spaceframe using thefield conduit umbilical connect between the primary andengineering sections.Fairly early on, Rick did a drawing for our writers showing the Enterprise superimposed over a map of the Paramount Studioslot. This was fun because it gave us for the first time a concrete idea of how big the ship "really" is. Abitlater, though, westartedto think of some of the implications of this enormous size. We began to realize that it would be pretty difficult for a structurethat size to maintain its rigidity and form, especially under the tremendous accelerations that impulse and warp drive wouldlikely entail. (We envisioned the main impulse engines firing, squashing the ship like a partially deflated blimp. This mightactually be a valid way for a space vehicle to operate, but it would probably look pretty silly on film.) Because of this, we cameup with the "structural integrity field," which we envision as a powerful forcefield that helps to hold the ship together.
2.5 INERTIAL DAMPING SYSTEM2.5.1 Inertial potential cancellation using IDFPrimary/backup IDF generatorsCounter-acceleration imposedby IDF generatorsNatural acceleration vector2.5 INERTIAL DAMPING SYSTEMOperating in parallel with the structural integrity field (SIF)system is the inertial damping field system (IDF). This systemgenerates a controlled series of variable-symmetry forcef ieldsthat serve to absorb the inertial forces of spaceflight whichwould otherwise cause fatal injury to the crew. The IDF isgenerated separately from the SIF, but is fed by a parallelseries of waveguides that are then conducted through syntheticgravity plates.The IDF operates by maintaining a low-level forcefieldthroughout the habitable volume of the spacecraft. This fieldaverages 75 millicochranes with field differential limited to5.26 nanocochranes/meter, per SFRA-standard 352.12 forcrew exposure to subspace fields.As acceleration effects are anticipated, this field is distortedalong a vector diametrically opposed to the velocitychange. The IDF thereby absorbs the inertial potential, whichwould otherwise have acted upon the crew.generator consists of a cluster of twelve 500 kW gravitonpolarity sources feeding a pair of 150 millicochrane subspacefield distortion amplifiers. Heat dissipation on each unit isprovided by a pair of 100,000 MJ/hr continuous-duty liquidhelium coolant loops. Three backup generators are locatedin each hull, providing up to twelve hours of service at 65% ofmaximum rated power. Normal duty cycle on generators isforty-eight hours online, with nominal twelve hours degaussand scheduled maintenance time. Graviton polarity sourcesare rated for 2,500 operating hours between routine servicingof superconductive elements.Cruise Mode operating rules require at least two fieldgenerators to be active at all times in each hull, although theFlight Control Officer may call for activation of additional unitswhen extreme maneuvers are anticipated. During Alertmodes, all operational units are brought to hot standby forimmediate activation. Reduced Power Mode rules permit asingle field generator to feed the entire spaceframe, using thefield conduit umbilical connect between the primary and engineeringsections.There is a characteristic lag time for the shifting of IDFdirection and intensity. This lag varies with the net accelerationinvolved, but averages 295 milliseconds for normal impulsemaneuvers. Because IDF control is generally derivedfrom Flight Controller data, normal course corrections can beanticipated so there is rarely any noticeable acceleration tothe crew. Exceptions to this sometimes occur when power forIDF operations is restricted or when sudden maneuvers orother externally caused accelerations occur more rapidly thanthe system can respond.Flux generation for the IDF is provided by four fieldgenerators located on Deck 11 in the Primary Hull and by twogenerators located on Deck 33 in the Engineering Hull. EachThe tremendous accelerations involved in the kind of spaceflight seen on Star Trek would instantly turn the crew to chunkysalsa unless there was some kind of heavy-duty protection. Hence, the inertial damping field. The reason for the "characteristiclag" referred to above is to "explain" why our crew is occasionally knocked out of their chairs during battle or other drasticmaneuvers despite the IDF. The science of all this is admittedly a bit hazy, but it seems a good compromise between dramaticnecessity and maintaining some kind of technical consistency.
- 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 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 46 and 47: 3.11 ENGINEERING3.11.1 Engineering
- 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
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- Page 70 and 71: 5.4 ANTIMATTER STORAGE AND TRANSFER
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2.5 INERTIAL DAMPING SYSTEM2.5.1 Inertial potential cancellation using IDFPrimary/backup IDF generatorsCounter-acceleration imposedby IDF generatorsNatural acceleration vector2.5 INERTIAL DAMPING SYSTEMOperating in parallel with the structural integrity field (SIF)system is the inertial damping field system (IDF). This systemgenerates a controlled series of variable-symmetry forcef ieldsthat serve to absorb the inertial forces of spaceflight whichwould otherwise cause fatal injury to the crew. The IDF isgenerated separately from the SIF, but is fed by a parallelseries of waveguides that are then conducted through syntheticgravity plates.The IDF operates by maintaining a low-level forcefieldthroughout the habitable volume of the spacecraft. This fieldaverages 75 millicochranes with field differential limited to5.26 nanocochranes/meter, per SFRA-standard 352.12 forcrew exposure to subspace fields.As acceleration effects are anticipated, this field is distortedalong a vector diametrically opposed to the velocitychange. The IDF thereby absorbs the inertial potential, whichwould otherwise have acted upon the crew.generator consists of a cluster of twelve 500 kW gravitonpolarity sources feeding a pair of 150 millicochrane subspacefield distortion amplifiers. Heat dissipation on each unit isprovided by a pair of 100,000 MJ/hr continuous-duty liquidhelium coolant loops. Three backup generators are locatedin each hull, providing up to twelve hours of service at 65% ofmaximum rated power. Normal duty cycle on generators isforty-eight hours online, with nominal twelve hours degaussand scheduled maintenance time. Graviton polarity sourcesare rated for 2,500 operating hours between routine servicingof superconductive elements.Cruise Mode operating rules require at least two fieldgenerators to be active at all times in each hull, although theFlight Control Officer may call for activation of additional unitswhen extreme maneuvers are anticipated. During Alertmodes, all operational units are brought to hot standby forimmediate activation. Reduced Power Mode rules permit asingle field generator to feed the entire spaceframe, using thefield conduit umbilical connect between the primary and engineeringsections.There is a characteristic lag time for the shifting of IDFdirection and intensity. This lag varies with the net accelerationinvolved, but averages 295 milliseconds for normal impulsemaneuvers. Because IDF control is generally derivedfrom Flight Controller data, normal course corrections can beanticipated so there is rarely any noticeable acceleration tothe crew. Exceptions to this sometimes occur when power forIDF operations is restricted or when sudden maneuvers orother externally caused accelerations occur more rapidly thanthe system can respond.Flux generation for the IDF is provided by four fieldgenerators located on Deck 11 in the Primary Hull and by twogenerators located on Deck 33 in the Engineering Hull. EachThe tremendous accelerations involved in the kind of spaceflight seen on Star Trek would instantly turn the crew to chunkysalsa unless there was some kind of heavy-duty protection. Hence, the inertial damping field. The reason for the "characteristiclag" referred to above is to "explain" why our crew is occasionally knocked out of their chairs during battle or other drasticmaneuvers despite the IDF. The science of all this is admittedly a bit hazy, but it seems a good compromise between dramaticnecessity and maintaining some kind of <strong>technical</strong> consistency.