DY-100 class (FASA)

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Myriad Universes: DY-100 class
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DY-100 class
DY-100 class (TOS 24)

DY-100 class (TOS 24)
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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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