Difference between revisions of "DY-100 class"

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{{ImageBox|imgname=dy100-tos24|caption=DY-100 class ([[Star Trek|TOS]] [[Space Seed (Episode)|24]])}}
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{{ImageInfoBox|name=DY-100 class|imgname=dy100-tos24|caption=DY-100 class ([[Star Trek|TOS]] [[Space Seed (Episode)|24]])}}
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{{TableRow|title=Advertising|data={{AmazonLink}}}}
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|}</div>
 
==FASA Timeline==
 
==FASA Timeline==
 
The DY-100, introduced in [[FASA Timeline: 1990s#1995|1995]], was the first mass-produced spacecraft capable of routine circumlunar ([[Earth]]-[[Moon (Sol IIIa)|moon]]) travel. Interchangeable modules permitted wide diversity of mission profiles, including an upgrade for interplanetary travel that allowed it to take humans to [[Mars#FASA Timeline|Mars]]. The class remained in service until [[FASA Chronology: 2020s#2020|2020]].<ref name="SFC"/>
 
The DY-100, introduced in [[FASA Timeline: 1990s#1995|1995]], was the first mass-produced spacecraft capable of routine circumlunar ([[Earth]]-[[Moon (Sol IIIa)|moon]]) travel. Interchangeable modules permitted wide diversity of mission profiles, including an upgrade for interplanetary travel that allowed it to take humans to [[Mars#FASA Timeline|Mars]]. The class remained in service until [[FASA Chronology: 2020s#2020|2020]].<ref name="SFC"/>
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<div style="width:25%;float:left;margin-right:0.25em;">
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===Specifications===
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{{InfoBox|float=left;|name=Specifications<ref name="SFC"/>}}
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{|
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{{TableRow|title=Length|data=100 [[meter|m]]}}
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|-
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{{TableRow|title=Beam|data=23.37 [[meter|m]]}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Length
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{{TableRow|title=Draught|data=34.9 [[meter|m]]}}
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|style="vertical-align:top;"|100[[meter|m]]
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{{TableRow|title=Mass|data=2.72 million [[kilogram|kg]]}}
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|-
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{{TableRow|title=Living/Fuel/Cargo Units|data=Interchangeable modules each 27x5.5x6.57[[meter|m]] (795[[cubic meter|m&sup3;]] usable volume)}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Beam
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{{TableRow|title=Engine Section|data=Combination Chemical/Fission<br/>{{bullet}} Diameter: 6.13 [[meter|m]]<br/>{{bullet}} Length: 19[[meter|m]]}}
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|style="vertical-align:top;"|23.37[[meter|m]]
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{{TableRow|title=Command Con|data=12.3x7.4x4.9 [[meter|m]]}}
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|-
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{{TableRow|title=Complement|data={{bullet}} Officers: 2<br/>{{bullet}} Crew/Passengers: 0-20}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Draught
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{{TableRow|title=Navigation|data=Optical Tracker-Controlled Inertial Guidance}}
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|style="vertical-align:top;"|34.9[[meter|m]]
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{{TableRow|title=Communications|data=Laser Radiotelemetry}}
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|-
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{{TableRow|title=Computer|data=Standard Program-Dependent Digital Memory}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Mass
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{{TableRow|title=Life Support|data={{bullet}} Gravity: No internal control<br/>{{bullet}} Atmosphere: 34.7% [[oxygen|O<sub>2</sub>]]; 11% humidity}}
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|style="vertical-align:top;"|2.72 million [[kilogram|kg]]
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|}</div>
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|-
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{{InfoBox|float=left|name=Performance<ref name="SFC"/>}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Living Units/ Fuel Units/ Cargo Units
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{{TableRow|title=Range|data={{bullet}} Standard: 900,000 [[kilometer|km]]<br/>{{bullet}} Maximum: 387 million [[kilometer|km]] (refit for duration travel)}}
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|style="vertical-align:top;"|Interchangeable modules each 27x5.5x6.57[[meter|m]] (795[[cubic meter|m&sup3;]] usable volume)
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{{TableRow|title=Velocity|data={{bullet}} Cruising: 55,000 [[kilometer|km]]/hour<br/>{{bullet}} Maximum: 80,000 [[kilometer|km]]/hour<br/>{{bullet}} Escape Velocity ([[Earth]]): 38,000 [[kilometer|km]]/hour}}
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|-
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{{TableRow|title=Voyage Duration|data={{bullet}} Typical ([[Earth]]-[[Luna|Moon]]): 9.2 hours<br/>{{bullet}} Maximum ([[Earth]]-[[Mars]]-[[Asteropolis]]-[[Mars]]-[[Earth]]): 934 days (with supply stops)}}
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Engine Section
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{{TableRow|title=Thrust|data={{bullet}} Chemical: Six chemical boost engines for [[Earth]] escape producing 4.2 million [[kilogram|kg]]<br/>{{bullet}} Fission: One Amjet hydrogen fission thruster for interplanetary transfer producing 68,000 [[kilogram|kg]] (average)}}
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|style="vertical-align:top;"|Combination Chemical/Fission
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|}</div>
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* Diameter: 6.13[[meter|m]]
 
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* Length: 19[[meter|m]]
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Command Con
 
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|style="vertical-align:top;"|12.3x7.4x4.9[[meter|m]]
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Complement
 
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|style="vertical-align:top;"|
 
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* Officers: 2
 
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* Crew/Passengers: 0-20
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Navigation
 
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|style="vertical-align:top;"|Optical Tracker-Controlled Inertial Guidance
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Communications
 
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|style="vertical-align:top;"|Laser Radiotelemetry
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Computer
 
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|style="vertical-align:top;"|Standard Program-Dependent Digital Memory
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Life Support
 
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|style="vertical-align:top;"|
 
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* Gravity: No internal control
 
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* Atmosphere: 34.7% [[oxygen|O<sub>2</sub>]]; 11% humidity
 
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|}
 
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</div>
 
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<div style="width:25%;float:left;margin-right:0.25em;">
 
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===Performance===
 
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{|
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Range (Standard)
 
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|style="vertical-align:top;"|900,000[[kilometer|km]]
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Range (Maximum)
 
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|style="vertical-align:top;"|387 million [[kilometer|km]] (refitted for duration travel)
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Velocity (Cruising)
 
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|style="vertical-align:top;"|55,000[[kilometer|km]]/hour
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Velocity (Maximum)
 
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|style="vertical-align:top;"|80,000[[kilometer|km]]/hour
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Escape Velocity ([[Earth]])
 
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|style="vertical-align:top;"|38,000[[kilometer|km]]/hour
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Typical Voyage Duration
 
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|style="vertical-align:top;"|9.2 hours ([[Earth]]-[[Moon (Sol IIIa)|Moon]])
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Maximum Voyage (With Supply Stops)
 
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|style="vertical-align:top;"|934 days ([[Earth]]-[[Mars]]-[[Asteropolis]]-[[Mars]]-[[Earth]])
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Thrust (Chemical)
 
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|style="vertical-align:top;"|4.2 million [[kilogram|kg]]
 
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* Six chemical boost engines for [[Earth]]-escape
 
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|-
 
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|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Thrust (Fission)
 
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|style="vertical-align:top;"|68,000 [[kilogram|kg]] (average)
 
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* One Amjet hydrogen fission thruster for interplanetary transfer
 
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|}
 
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{{Clear}}
 
{{Clear}}
 
{{ClassDY100}}
 
{{ClassDY100}}
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[[Category:LUG]]
 
[[Category:LUG]]
 
[[Category:Modiphius]]
 
[[Category:Modiphius]]
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[[Category:Alternate Universes]]
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[[Category:Prime Timeline]]
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[[Category:EU Timeline]]
 
[[Category:Kelvin Timeline]]
 
[[Category:Kelvin Timeline]]
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[[Category:FASA Timeline]]
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[[Category:Mirror Universe]]
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[[Category:Myriad Universes]]

Revision as of 23:20, 12 April 2020

DY-100 class
DY-100 class (TOS 24)

DY-100 class (TOS 24)
Advertising

FASA Timeline

The DY-100, introduced in 1995, was the first mass-produced spacecraft capable of routine circumlunar (Earth-moon) travel. Interchangeable modules permitted wide diversity of mission profiles, including an upgrade for interplanetary travel that allowed it to take humans to Mars. The class remained in service until 2020.[1]

Specifications[1]
Length 100 m
Beam 23.37 m
Draught 34.9 m
Mass 2.72 million kg
Living/Fuel/Cargo Units Interchangeable modules each 27x5.5x6.57m (795m³ usable volume)
Engine Section Combination Chemical/Fission
 •  Diameter: 6.13 m
 •  Length: 19m
Command Con 12.3x7.4x4.9 m
Complement  •  Officers: 2
 •  Crew/Passengers: 0-20
Navigation Optical Tracker-Controlled Inertial Guidance
Communications Laser Radiotelemetry
Computer Standard Program-Dependent Digital Memory
Life Support  •  Gravity: No internal control
 •  Atmosphere: 34.7% O2; 11% humidity
Performance[1]
Range  •  Standard: 900,000 km
 •  Maximum: 387 million km (refit for duration travel)
Velocity  •  Cruising: 55,000 km/hour
 •  Maximum: 80,000 km/hour
 •  Escape Velocity (Earth): 38,000 km/hour
Voyage Duration  •  Typical (Earth-Moon): 9.2 hours
 •  Maximum (Earth-Mars-Asteropolis-Mars-Earth): 934 days (with supply stops)
Thrust  •  Chemical: Six chemical boost engines for Earth escape producing 4.2 million kg
 •  Fission: One Amjet hydrogen fission thruster for interplanetary transfer producing 68,000 kg (average)


Notes and References

  1. ↑ 1.0 1.1 1.2 Goldstein, Stan et al (Authors). Spaceflight Chronology. Star Trek. Book. Wallaby Books. 1980.
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