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Q: What are the amount of lift and drag of an rocket?
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How many forces acting are on a rocket?

There are four forces acting upon a rocket these are: Thrust, Gravity, Drag and Lift.


What four forces is a model rocket subject to during a flight?

Lift, drag, thrust, and gravity.


Why are aeroplanes shaped the way they are?

To produce lift with the least amount of induced drag.


What force must a rocket overcome to be launched into space?

Alright, it is mainly the force of gravity. This is because if there was no gravity, you do not heat energy to fire the rocket up.


How does a rocket achieve lift?

A rocket achieves lift by pushing back the air column


Why drag increases as lift increase - for helis?

The production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.


What is lift from a rocket?

Rockets do not have lift, they have thrust.


How are the lift and drag components of the wing affected when you lower the flaps?

lift decrease and increase drag


What is the zero lift drag coefficient of Airbus A330-200?

coefficient of drag in 0 lift


What is the importance of lift to drag ratio?

In aircraft aerodynamics, the lift-to-drag ratio, or L/D ratio, is the amount of lift generated by an aerofoil, divided by the drag it creates by moving through the air. A higher or more favourable L/D ratio is typically one of the major goals in aircraft design; since a particular aircraft's required lift is set by its weight, delivering that lift with lower drag leads directly to better fuel economy, climb performance, and glide ratio.


Why is th tip of the rocket made pointer?

The tip of a rocket is pointy to increase aerodynamics and reduces drag. For example, if a rocket had a flat end, it would create more drag and slow the rocket down. It's also the same for planes too.


How does the lift thrust drag and gravity affect a helicopter?

Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.