Difference between revisions of "DY-100 class"

From Trekipedia
Jump to: navigation, search
(Created page with "350px|thumb|right|DY-100 class ([[Star Trek|TOS 24)]] * RSD -1/9500: The DY-100 is the first m...")
 
Line 1: Line 1:
 +
==FASA Timeline==
 
[[File:dy100-tos24.jpg|350px|thumb|right|DY-100 class ([[Star Trek|TOS]] [[Space Seed (Episode)|24]])]]
 
[[File:dy100-tos24.jpg|350px|thumb|right|DY-100 class ([[Star Trek|TOS]] [[Space Seed (Episode)|24]])]]
−
* RSD -1/9500: The [[DY-100 class#FASA_Timeline|DY-100]] is the first mass-produced spacecraft capable of short interplanetary travel ([[Earth]]-[[Moon (Sol IIIa)|moon]]). In an [[DY-500#FASA_Timeline|uprated mode]], it will be able to take humans to [[Mars#FASA Timeline|Mars]]. The class will remain 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"/>
  
 
===DY-100 class Vessels===
 
===DY-100 class Vessels===
Line 6: Line 7:
 
* [[S.S. Botany Bay (DY-100)|S.S. ''Botany Bay'']]
 
* [[S.S. Botany Bay (DY-100)|S.S. ''Botany Bay'']]
  
 +
<div style="width:25%;float:left;margin-right:0.25em;">
 +
===Specifications===
 +
{|
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Length
 +
|style="vertical-align:top;"|100[[meter|m]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Beam
 +
|style="vertical-align:top;"|23.37[[meter|m]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Draught
 +
|style="vertical-align:top;"|34.9[[meter|m]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Mass
 +
|style="vertical-align:top;"|2.72 million [[kilogram|kg]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Living Units/ Fuel Units/ Cargo Units
 +
|style="vertical-align:top;"|Interchangeable modules each 27x5.5x6.57[[meter|m]] (795[[cubic meter|m&sup3;]] usable volume)
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Engine Section
 +
|style="vertical-align:top;"|Combination Chemical/Fission
 +
* Diameter: 6.13[[meter|m]]
 +
* Length: 19[[meter|m]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Command Con
 +
|style="vertical-align:top;"|12.3x7.4x4.9[[meter|m]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Complement
 +
|style="vertical-align:top;"|
 +
* Officers: 2
 +
* Crew/Passengers: 0-20
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Navigation
 +
|style="vertical-align:top;"|Optical Tracker-Controlled Inertial Guidance
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Communications
 +
|style="vertical-align:top;"|Laser Radiotelemetry
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Computer
 +
|style="vertical-align:top;"|Standard Program-Dependent Digital Memory
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Life Support
 +
|style="vertical-align:top;"|
 +
* Gravity: No internal control
 +
* Atmosphere: 34.7% [[oxygen|O&sub2;]]; 11% humidity
 +
|}
 +
</div>
 +
<div style="width:25%;float:left;margin-right:0.25em;">
 +
===Performance===
 +
{|
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Range (Standard)
 +
|style="vertical-align:top;"|900,000[[kilometer|km]]
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Range (Maximum)
 +
|style="vertical-align:top;"|387 million [[kilometer|km]] (refitted for duration travel)
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Velocity (Cruising)
 +
|style="vertical-align:top;"|55,000[[kilometer|km]]/hour
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Velocity (Maximum)
 +
|style="vertical-align:top;"|80,000[[kilometer|km]]/hour
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Escape Velocity ([[Earth]])
 +
|style="vertical-align:top;"|38,000[[kilometer|km]]/hour
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Typical Voyage Duration
 +
|style="vertical-align:top;"|9.2 hours ([[Earth]]-[[Moon (Sol IIIa)|Moon]])
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Maximum Voyage (With Supply Stops)
 +
|style="vertical-align:top;"|934 days ([[Earth]]-[[Mars]]-[[Asteropolis]]-[[Mars]]-[[Earth]])
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Thrust (Chemical)
 +
|style="vertical-align:top;"|4.2 million [[kilogram|kg]]
 +
* Six chemical boost engines for [[Earth]]-escape
 +
|-
 +
|class="HeaderRow ButtonLeft" style="width:25%;text-align:left;vertical-align:top;"|Thrust (Fission)
 +
|style="vertical-align:top;"|68,000 [[kilogram|kg]] (average)
 +
* One Amjet hydrogen fission thruster for interplanetary transfer
 +
|}
 +
</div>
 +
 +
<div style="clear:both;"></div>
 
==References==
 
==References==
 
<references>
 
<references>

Revision as of 11:49, 26 April 2019

FASA Timeline

DY-100 class (TOS 24)

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]

DY-100 class Vessels

Specifications

Length 100m
Beam 23.37m
Draught 34.9m
Mass 2.72 million kg
Living Units/ Fuel Units/ Cargo Units Interchangeable modules each 27x5.5x6.57m (795m³ usable volume)
Engine Section Combination Chemical/Fission
  • Diameter: 6.13m
  • Length: 19m
Command Con 12.3x7.4x4.9m
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% O&sub2;; 11% humidity

Performance

Range (Standard) 900,000km
Range (Maximum) 387 million km (refitted for duration travel)
Velocity (Cruising) 55,000km/hour
Velocity (Maximum) 80,000km/hour
Escape Velocity (Earth) 38,000km/hour
Typical Voyage Duration 9.2 hours (Earth-Moon)
Maximum Voyage (With Supply Stops) 934 days (Earth-Mars-Asteropolis-Mars-Earth)
Thrust (Chemical) 4.2 million kg
  • Six chemical boost engines for Earth-escape
Thrust (Fission) 68,000 kg (average)
  • One Amjet hydrogen fission thruster for interplanetary transfer

References

  1. ↑ Goldstein, Stan and Goldstein, Fred with Sternbach, Rick. Star Trek: Spaceflight Chronology. Pocket Books, 1980.
Retrieved from "http://trekipedia.com/mw/index.php?title=DY-100_class&oldid=12964"