(Sorry, I don't understand what I've done wrong with the table layout. I'll be glad to edit it if someone gives me a hint...)
I went over the T5 rules for LTA vehicles and basically concluded that the Hindenburg, a real-life airship, could never have been built.
Then again, aerodynamic engineers swear bumblebees can't fly and yet they do...
So, here's my take on a TL6 LTA Airship manuevered by electric engines powered by a standard Fusion+ powerplant unit.
All Ton Measurements in LH volume Tons unless otherwise noted.
TL 6 Construction-capable unless otherwise noted.
Item | Size | Notes |
Gas Bag | 14,218 | Helium-filled, Hindenburg 14,124 |
Cupola | 1,579 | Aluminum or Titanium construction |
Passenger Cabin, 1st Class | 240 | 60 passengers @ 4T |
Passenger Cabin, 2nd Class | 312 | 156 passengers @ 2T |
Captain's Cabin | 6 | . |
Head Steward's Cabin | 4 | . |
Flight Crew Cabins | 38 | 19 crew @ 2T |
Steward Crew Cabins | 58 | 29 @ 2T, includes 2 Medics |
Ship's Stores | 33 | .2 T per 1st Passenger, Captain, Head Steward, .1 T per 2nd Passenger, Flight and Steward Crew |
Mail | 1 | . |
Cargo | 100 | . |
Cargo Lift Plate Compartment | 20 | Grav lift plates are not installed, but the ability to add them is present. This would enable heavier cargo to be carried or possibly to be used to replace the need for ballast. Currently used for Cargo. |
Ballast | 100 | Can be easily converted to cargo space if lift plates installed. |
Powerplant, Engines | 30 | Standard Fusion+ powerplant, electric engines. |
Galley | 20 | . |
Common Areas | 708 | Passengers & Crew @ 3T |
Option | . | Protected |
Option | . | Wilderness Landing |
Option | . | AutoPilot, Powered Controls |
Speed | 76Kph | . |
Duration | 7 days | . |
Range | 13440K | . |
The Hindenburg had a huge allotment for fuel and oil - over 30% of its weight allotment went to those two categories. A standard Fusion+ module saves a huge amount of weight and space.
57% of the Hindenburg's weight went to the rigid airframe, engines, etc. Electric engines are smaller and lighter than diesel/gasoline engines, plus more reliable. The actual fuel tanks wouldn't be needed either. Key structural elements made out of titanium instead of steel or aluminum should also reduce the weight. Plus, of course, several thousand years worth of metallurgical and structural engineering knowledge can be applied to further reduce the weight.
I haven't worked out cost yet.