I've a question: its just that most of the UAVs which are catapult launched are pusher configurations. Is there any particular reason for it?
Besides, I've been wondering that going for catapult launch means great forces on the underbelly. What structural changes are necessary to secure the plane against that? I mean does reinforcing the underbelly have great changes on the GTOW?
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For example:
Assume that you know your minimum airspeed is 30 mph (13.4 m/s), you reach that speed in 1 second, and your mass is 2 lbs (0.9072 Kg). The acceleration will be 13.4 m/s^2 (a=deltaV/time). Then you will need to apply 13.4*0.9072 = 12.156 Newtons (2.7 lbs) of force. This seems low until you consider that the track for this example would be 6.7 m (21 ft) long.
It is also easy enough to start with a certain track length, mass, and air-speed and calculate the forces. This all assumes that the acceleration is smooth and constant over the length of the track.
Another reason for catapults is that with some there is a severe danger of having your hand travel through the prop. When it is spinning at 20,000+ rpm that it a problem ;)
As for structural changes to the airframe? I can't help, we haven't gotten that far yet.