Power to mass ratios, ion engines, FTL, et cetera.
Posted: Thu Dec 06, 2007 9:09 am
Just throwing some figures out there. Most of these are on my website, but they get ignored a lot there.
Power required for a current generation ion engine per unit of thrust: ~25 kW/N.
Efficiency of a modern ion engine: High enough that differences in efficiency are insignificant for these calculations.
Primary determining factor, thrust/power ratio: Exhaust velocity.
Relationship: Linear.
Is it plausible that SW ion engines have similar exhaust velocities, and therefore thrust/power ratios? Yes. Could it be otherwise? Of course.
Top thrust of a SW fighter: Somewhere around 200 g (median estimate.)
Expected power consumption, SW fighter engine, under the above assumptions: 50 MW/kg. If a heavy SW fighter has a mass of 20 tons, this would be 1 TW.
Estimated acceleraton of capital ships in SW: Generously, ~50g.
Expected power consumption, SW capital ship engine, under the above assumptions: 12 MW/kg. If a SW capital ship has a mass of 50 million tons (5e10 kg) this would be 600 PW.
Gravitational potential, R=850,000 km, 1 solar mass: -160 GJ/kg
Gravitational potential, R=100,000,000 km, 1 solar mass: -1.3 GJ/kg.
Minimum wattage required to go from R=850,000 km to R=100,000,000 km in 100 seconds (stationary): 1.6 GW/kg. ("Relics") If a Galaxy class is 10 million tons, this would be 16 EW.
Time required to travel this distance using a terawatt engine pushing a million ton starship, i.e., a KW/kg engine: Years.
Gravitational potential, R=6400 km, 1 terran mass: -62 MJ/kg.
Gravitational potential, R=19200 km, 1 terran mass: -21 MJ/kg.
Gravitational potential, R=83200 km, 1 terran mass: -5 MJ/kg.
Change in energy, surface to 1-6.5 planetary diameters: 49+/-8 MJ/kg.
Average power, ship using 100% efficient non-inertial anti-gravity drive going from surface to hyper limit in ~1 minute: ~800 KW/kg.
With an inertial drive and a final velocity of 2 Earth diameters per minute: 380 MW/kg.
Rate of change of gravitational potential, ship displacing "magically" with no actual kinetic energy away from a large mass at an "effective velocity" of v[i.e., as in an freely interruptable FTL, such as warp drive, Enchenach drive, et cetera]: (v dot g)m, where g is the local gravitational field and v is the velocity.
Local value of g close to the Sun: 274 m/s.
Power for a "lightspeed" drive directly fleeing the Sun at an "effective velocity" of c: 82 GW/kg. If a GCS is 10 million tons, this is 800 EW.
Power for a "lightspeed" drive directly fleeing the Earth at an "effective velocity" of c: 3 GW/kg. If an ICS is 700,000 tons, this is 2 EW.
Power for a 1000 times lightspeed drive in an orbital 1 m/s g field: 300 GW/kg. If a GCS is 10 million tons, this is 3,000 EW.
Gravitational potential, R=19200 km, 1 terran mass, R=150,000,000 km, 1 solar mass: -910 MJ/kg.
Gravitational potential, R=4,500,000,000 km, 1 solar mass: -30 MJ/kg.
Change in energy, fairly low Earth orbit to Neptune, "lightspeed" drive: 880 MJ/kg.
Average rate of power, 3 minute trip one-way: 5 MW/kg. If the NX-01 is ~200,000 tons, this would be 100 TW.
Time required to travel this distance using a terawatt engine pushing a million ton starship, i.e., a KW/kg engine: Days.
Power required for a current generation ion engine per unit of thrust: ~25 kW/N.
Efficiency of a modern ion engine: High enough that differences in efficiency are insignificant for these calculations.
Primary determining factor, thrust/power ratio: Exhaust velocity.
Relationship: Linear.
Is it plausible that SW ion engines have similar exhaust velocities, and therefore thrust/power ratios? Yes. Could it be otherwise? Of course.
Top thrust of a SW fighter: Somewhere around 200 g (median estimate.)
Expected power consumption, SW fighter engine, under the above assumptions: 50 MW/kg. If a heavy SW fighter has a mass of 20 tons, this would be 1 TW.
Estimated acceleraton of capital ships in SW: Generously, ~50g.
Expected power consumption, SW capital ship engine, under the above assumptions: 12 MW/kg. If a SW capital ship has a mass of 50 million tons (5e10 kg) this would be 600 PW.
Gravitational potential, R=850,000 km, 1 solar mass: -160 GJ/kg
Gravitational potential, R=100,000,000 km, 1 solar mass: -1.3 GJ/kg.
Minimum wattage required to go from R=850,000 km to R=100,000,000 km in 100 seconds (stationary): 1.6 GW/kg. ("Relics") If a Galaxy class is 10 million tons, this would be 16 EW.
Time required to travel this distance using a terawatt engine pushing a million ton starship, i.e., a KW/kg engine: Years.
Gravitational potential, R=6400 km, 1 terran mass: -62 MJ/kg.
Gravitational potential, R=19200 km, 1 terran mass: -21 MJ/kg.
Gravitational potential, R=83200 km, 1 terran mass: -5 MJ/kg.
Change in energy, surface to 1-6.5 planetary diameters: 49+/-8 MJ/kg.
Average power, ship using 100% efficient non-inertial anti-gravity drive going from surface to hyper limit in ~1 minute: ~800 KW/kg.
With an inertial drive and a final velocity of 2 Earth diameters per minute: 380 MW/kg.
Rate of change of gravitational potential, ship displacing "magically" with no actual kinetic energy away from a large mass at an "effective velocity" of v[i.e., as in an freely interruptable FTL, such as warp drive, Enchenach drive, et cetera]: (v dot g)m, where g is the local gravitational field and v is the velocity.
Local value of g close to the Sun: 274 m/s.
Power for a "lightspeed" drive directly fleeing the Sun at an "effective velocity" of c: 82 GW/kg. If a GCS is 10 million tons, this is 800 EW.
Power for a "lightspeed" drive directly fleeing the Earth at an "effective velocity" of c: 3 GW/kg. If an ICS is 700,000 tons, this is 2 EW.
Power for a 1000 times lightspeed drive in an orbital 1 m/s g field: 300 GW/kg. If a GCS is 10 million tons, this is 3,000 EW.
Gravitational potential, R=19200 km, 1 terran mass, R=150,000,000 km, 1 solar mass: -910 MJ/kg.
Gravitational potential, R=4,500,000,000 km, 1 solar mass: -30 MJ/kg.
Change in energy, fairly low Earth orbit to Neptune, "lightspeed" drive: 880 MJ/kg.
Average rate of power, 3 minute trip one-way: 5 MW/kg. If the NX-01 is ~200,000 tons, this would be 100 TW.
Time required to travel this distance using a terawatt engine pushing a million ton starship, i.e., a KW/kg engine: Days.