# How to determine the minimum thrust to weight ratio for a fixed-wing aircraft?

I am considering building a fixed-wing aircraft with foam board, and I'm unsure what the necessary thrust to weight ratio is. With quads, it's easy to determine the necessary thrust. Just find a motor/prop combination that can provide more thrust than the weight of the quadcopter. With a fixed-wing, it isn't as simple because the aircraft can fly with less thrust than the total weight of the aircraft.

Is there any way to determine the minimum amount of thrust that can keep a fixed-wing airborne? The reason I'm trying to figure this out is because the goal of this aircraft is to be as efficient as possible.

I'm afraid it's not that simple. As you mention, planes can fly with a fairly low thrust to weight ratio. Obviously gliders can fly with no power at all, so there's no critical lower-limit.

The other issue is that pitch-speed is important - the prop needs to be producing thrust when the plane is moving, not stationary. Measuring static thrust only tells you half the story.

Instead of thrust, it's better to look at power. Assuming that your motor and prop are reasonably efficient (and most are) measure the power going into the motor with a watt meter (or run it for a minute and see how much energy your charger puts back into the battery). Then weigh the complete model, including the battery.

• 50 w/lb is about the minimum for gentle cruising and slow climbs.
• 100 W/lb is 'sporty', say for a warbird. You don't have to worry about conserving energy and can easily climb out of trouble. It might not have unlimited vertical climb though.
• 200 W/lb is unlimited vertical climb, hovering and climbing vertically out of the hover.

For ducted fans, you should double these numbers. i.e. at 100 w/lb you'll need to be careful to conserve energy.

However foam board planes aren't super-efficient or super-fast, so you can usually do a simple thrust test to check it'll be OK. Dangle it by a wing tip and gradually apply power.

• If the model has enough power to support its own weight, it's probably around 100 w/lb
• If it can only reach about 45 degrees, its about 50 w/lb and will fly if you're careful.