Editing Rocket (section)

====Drag====
{{main|Drag (physics)|Gravity drag|Aerodynamic drag}}
Drag is a force opposite to the direction of the rocket's motion relative to any air it is moving through. This slows the speed of the vehicle and produces structural loads. The deceleration forces for fast-moving rockets are calculated using the [[drag equation]].

Drag can be minimised by an aerodynamic [[nose cone]] and by using a shape with a high [[ballistic coefficient]] (the "classic" rocket shape—long and thin), and by keeping the rocket's [[angle of attack]] as low as possible.

During a launch, as the vehicle speed increases, and the atmosphere thins, there is a point of maximum aerodynamic drag called [[max Q]]. This determines the minimum aerodynamic strength of the vehicle, as the rocket must avoid [[buckling]] under these forces.<ref name=maxq>{{cite web |url=http://www.aerospaceweb.org/question/aerodynamics/q0025.shtml |title=Space Shuttle Max-Q |publisher=Aerospaceweb |date=2001-05-06 |access-date=2012-12-10}}</ref>