Difference between revisions of "DY-100 class"
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==FASA Timeline== | ==FASA Timeline== | ||
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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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===Specifications=== | ===Specifications=== | ||
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Revision as of 11:12, 29 August 2019
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
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 |
Command Con | 12.3x7.4x4.9m |
Complement |
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Navigation | Optical Tracker-Controlled Inertial Guidance |
Communications | Laser Radiotelemetry |
Computer | Standard Program-Dependent Digital Memory |
Life Support |
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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
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Thrust (Fission) | 68,000 kg (average)
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DY-100 class vessels
Prime Timeline
Columbia Timeline
LUG Timeline
S.S. Botany Bay DY-109 • S.S. Iberville DY-120 • S.S. Lyons Creek DY-166 • S.S. Monticello DY-158 • S.S. Salisbury DY-131 • S.S. San Juan DY-177 • S.S. Santa Maria DY-164 • S.S. Shenandoah DY-178 • S.S. Wacosta DY-104
FASA Timeline
S.S. Botany Bay • S.S. Copernicus
Kelvin Timeline
Myriad Universes
Notes and References
- ↑ Goldstein, Stan et al (Authors). Spaceflight Chronology. Star Trek. Book. Wallaby Books. 1980.