Aircraft Launch with Launch Loop Transformer Track Technology


The following presumes good computer models and active control of thrust and cable tensioning. Computation is cheaper than extra structural strength added to an aircraft.

Military Fighter Launch

One of the first applications of loop technology may be the rapid burst launch of squadrons of military aircraft. Presume control distributed among the aircraft to separate them safely after launch, and to control them in the turbulent wake of their predecessors, so they can average one second spacing. In peacetime, this allows low cost training and quiet operation, less likely to upset civilian neighbors. It reduces pollution and fuel consumption. Green war? :-(

I was in the economy parking lot at Portland Airport (PDX) when a pair of F15 fighters (?) took off from runway 10L, then rotated and hit the afterburners overhead, seemingly flying straight up (though I don't think they have that much thrust). The noise was ear-splitting and bone rattling; when the noise and shaking died down, I could hear half-a-dozen car alarms blaring in the parking lot. I suppose pilots need training, but every noisy exercise like this shifts voters into the "cut the military budget, shut down the PDX Air Guard" voting block. A quiet way to launch training exercises, and a quick way to get an entire squadron airborne to altitude in a crisis, will promote a squadron's political and military survivability.

Assume a launch of 30 F-35A aircraft, one per second. WAG follows:


The aircraft may be connected to the sled with cables so they can be "flown like kites" after reaching takeoff speed. They can be hauled back down to the ground during an abort, with subsequent aircraft flying over the aborted aircraft.


Wikipedia: The EMALS 300-foot (91 m) LIM will accelerate a 100,000-pound (45,000 kg) aircraft to 130 kn (240 km/h; 150 mph), cites EDN 240 km/h is 66.7 m/s, in 91m is average 24.4 m/s², perhaps a peak of 30 m/s², kinetic energy of 200 MJ.


Launch loop version 1 assumes a 14km radius D magnet and 14 km/s, thus a radial acceleration of 14000 m/s². A 500 m radius power loop with 8,000 m/s² acceleration would move at 2000 m/s and store 2 MJ/kg. 3000 meters of 4 kg/m rotor stores 24 GJ. With a transformer track, this is more than enough energy to launch the 30 aircraft. With a 1 MW grid feed, loop energy could be restored in 90 minutes.


Commercial airport runway launch

If the loop takeoff assist system is available for war, it should be maintained for peaceful purposes 95% of the time. Commercial airliners are less noisy than fighters on afterburners, but perform many more takeoffs at most airports, angering civilian neighbors. Let's protect the neighbor's sleep from commercial takeoffs as well.

Here's some air transport takeoff masses and speeds:

Boeing 737

45 tonnes

250 km/h

69 m/s

108 MJ

Boeing 757

109 tonnes

260 km/h

72 m/s

284 MJ

Boeing 747

363 tonnes

290 km/h

81 m/s

1180 MJ

Antonov 124

405 tonnes

300 km/h WAG!!!

83 m/s

1400 MJ

Concorde

181 tonnes

360 km/h

100 m/s

905 MJ

Per runway flight ops at big airports seem like one per minute, but might be 30 seconds apart? So, we might need power capacity for an occasional Antonov, but we will typically be launching about 1200 MJ per minute, or 20 MW of launch power, on average. A 24 GJ loop could easily launch a 1.4 GJ Antonov, getting that huge bird off the ground with as much thrust as the cable-anchoring hardpoints would allow. Presume that we attach to the aircraft at many points, and adjust the distribution of forces on the cables to minimize structural load; we could get it off the ground with much less than 10,000 feet of runway.

The Concorde is a special case. 100 m/s (on its small, overloaded undercarriage) created far more damage to its tires than normal aircraft. It may require both thrust and vertical support to reduce the tire stress. Landing after an aborted takeoff would put the full weight of the aircraft on the wheels, plus vertical acceleration. The Concorde's fatal accident (which doomed the SST concept) was a tire failure during takeoff. Sled-assisted launch probably won't help. The Concorde was a commercial and economic failure. While another high performance commercial passenger aircraft may succeed someday, it is probably beyond the planning needs of loop assisted launch.

AircraftLaunch (last edited 2017-10-11 01:35:00 by KeithLofstrom)