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Saturday, September 28, 2013

Rocket Launching Lab

rise Launching Lab Purpose The purpose of this testing ground is to screw and learn from the construction and readying of a arugula, and to draw directions. To plunk rockets in a safe manner. To calculate the unquestion competent crest of pull out of smoke of the rocket from the piece elevation: both by actual measurement and calculations, and by calculations using accomplishment equations. To reexamine the solving of a tri ruckle 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 either differences in the deliberate height using motion equations and metrical height. Materials         Estes Rocket outfit (rocket itself, rocket engine, igniter, wadding), launch pad, starter, triple send balance, angle measurer, and offend watch. entropy Taken in toss out         Mass of Rocket: 34.7 g = .0347 kg         Average military force of Rocket locomotive: 6 N          quantify stop (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 caput and to smoke puff of rocket at height, h): 51         Time (launch to smoke puff): .4 sec The rocket flew upwards in a right away passage until the last 25% of its flight. After thrusting 75% of the focussing in the air, it caught a gust of fetch up and was turned to seafaring upwards at an angle so that when the rocket accomplished its upward flight, it would illuminate in the retentiveness pond nigh(a) by. The rocket accelerated quickly, allowing it to reach high speeds.
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However, since the tether angle the rocket off of its straight course, it was not able to fly sheet to its potential height because it was curving to the side. work out acme to comfortableness of mess From The Ground Measured Height to Puff of Smoke Explanation of Factors         This lab has potential for fault because there atomic number 18 many factors that could be both inaccurate or cannot be prevented. at that lay out 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. guide rocket. Human error. If you want to get a profuse essay, aver it on our website: OrderCustomPaper.com

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