Quote:
Originally Posted by Phaelen Bleux
Two 15,151-lb. thrust Turbofans with Afterburners
Fuel: 5,025 gallons jet fuel (Fire 13) in standard self-sealing fuel tanks (Fire +0).
Occupancy: 2 NCS.
1,500-lb. bomb bay.
Body is 1,080 cf;
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Some questions. I did an F-111 long ago and had a significantly larger body.
Engines = 129.208 cf + 129.208 cf Access Space
5,025 gallons = 753.75 cf
2 NCS = 60 cf
1,500 lb bomb bay = 45 cf
Those components alone add up to 1,117.166 cf.
Did you put some fuel tanks into the wings ?
Is there a rule somewhere lifting the access space requirement for powered propulsion systems outside of pods (VE2/15) ?
I used a Heavy Cheap Frame and DR 8. Is aMR 9.5 realistic ?