Launch (TL12)
Designed by Greg Svenson, Svenson Small Craft, LIC
| Summary: | 20.00 displacement ton cylinder streamlined; 252 tones; MCr 8.47 |
| Chassis: | 280 kL cylinder streamlined (16 m long x 4.7 m wide x 4.7 m high); Structure: 15.5 tones of superdense, body 1.0 cm thick, sealed (1 atm), 11 armor rating |
| Performance: | 38.0 MW TL12 Fusion Plus power plant with vacuum radiators; Fuel: 1.14 kL of enriched water (1.14 tones), 96 hours supply |
| Propulsion System: | 27.0 MW thruster; Maximum Speed: 405 km/h; Range: 38817 km; Agility: -1DM |
| Crew & Passengers: | pilot; 1 crew station; 9 roomy passenger seats |
| Communications: | Far Orbit Radio (100 kW, TL12, DirAnt, DirFnd), Orbital Laser (1.00 MW, TL12, SmVcl, MilSpec) |
| Sensors: | Active Regional Radar (1.00 kW, DispArray) Resolution: 0.050 mm per km of range |
| Other: | 204 kL of cargo space (15.1 tones) |
Designed with CSC (software (c) Robert Prior, 1997)
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