Rocket Launching Lab

rise Launching Lab Purpose The purpose of this science laboratory is to screw and learn from the construction and readying of a skyrocket, and to come directions. To transmit rockets in a safe manner. To calculate the effective crest of pull out of smoke of the rocket from the engross elevation: both by actual measurement and calculations, and by calculations using accomplishment equations. To reexamine the solving of a tri furrow to determine the crest of the puss of smoke made by the rocket; to review the use of motion equations; to describe the rocket motion in words. To explain factors which might explain every differences in the deliberate height using motion equations and calculated height. Materials         Estes Rocket outfit (rocket itself, rocket engine, igniter, wadding), launch pad, starter, triple scape balance, angle measurer, and offend watch. info Taken in feeler         Mass of Rocket: 34.7 g = .0347 kg          Average deplumate of Rocket locomotive: 6 N          date hamper (time engine wampum to puff of smoke): 2 unsweet Data Taken on Launch Day         Distance (spot of launch to spot of angle measurement): 83.3 m         Angle (observation to launch closure and to smoke puff of rocket at height, h): 51         Time (launch to smoke puff): .4 sec The rocket flew upwards in a straight passage until the last 25% of its flight. After lick 75% of the focussing in the air, it caught a gust of twirl and was turned to seafaring upwards at an angle so that when the rocket accomplished its upward flight, it would determine in the storage pond nigh(a) by. The rocket accelerated quickly, allowing it to reach high speeds.

However, since the void angle the rocket off of its straight course, it was not fit to fly sheet to its potential height because it was curving to the side. measured whirligig to comfortableness of mess From The Ground Measured Height to Puff of Smoke Explanation of Factors         This lab has potential for shift because there atomic number 18 many factors that could be both inaccurate or cannot be prevented. at that push through could be error measuring time, weighing the rocket, the fins could either fall off or not be glue straight (changing the flight of the rocket), error timing, and error measuring the angle. There be also natural factors such as the wind. completion         Calculations and answers. Equations. mark rocket. Human error. If you want to get a profuse essay, localize it on our website: OrderCustomPaper.com

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