Deltaglider EX "Dakota"
Purpose :
Acomplish flights within stellar systems. Atmospheric re-entry capabilities.
Release date : 2150/2250.
l : 50 m ;
ws : 45 m ;
h : 13 m (landed, in fligth : 12 m) ;
weight : 100 tons empty, 200 tons full (from earth). *
Crew : 4.
Payload :
- 1 shuttle sized bay ; *
- 1 Multipurpose bay.
Hull, structure and parts :
- Nanolathing , biomechanics systems.
Electrical power :
- APU (5Mw) ; *
- Fusion reactor (45Mw) ; *
- 1 Nanolathed collisioner ;
- 1 Cryo-molecular compressed nanits cartridge. Used for cooling reactor ;
- Additional cooling by deployables nanocaloducs.
Engines :
- 4 Hybrid Atmospherics Propulsors (HAP) : Turbojet, works on Earth, Mars and Titan, up to 95 000 lbs trust (Titan) ;
Ramjet, work on Earth, Mars and Titan, up to 123 000 lbs trust (Titan) ; Combustion chamber ; *
- 1 Plasma grid ;
- 64 RCS engines ; *
- 32 Hover engines. *
Propelants :
- APU : fuel/oxidizer ;
- Hybrid engines : fuel/oxidizer ;
- Plasma grid : 1 cryo-molecular compressed He3 cartridge.
* : temporary specifications.
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