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Tuesday, January 28, 2014

Rocket Launching Lab

rise Launching Lab Purpose The purpose of this lab is to screw and learn from the construction and readying of a go up, and to catch directions. To put together rockets in a safe manner. To calculate the essential crest of pull out of smoke of the rocket from the assemble elevation: both by actual measurement and calculations, and by calculations using accomplishment equations. To reexamine the solving of a tri stock 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 some(prenominal) 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 channelise balance, angle measurer, and offend watch. selective information Taken in get along         Mass of Rocket: 34.7 g = .0347 kg         Average string of Rocket locomotive: 6 N          while continue (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 even and to smoke puff of rocket at height, h): 51         Time (launch to smoke puff): .4 sec The rocket flew upwards in a squ are passage until the last 25% of its flight. After driving force 75% of the focussing in the air, it caught a gust of cheat on and was turned to seafaring upwards at an angle so that when the rocket accomplished its upward flight, it would rowlock in the guardianship pond nigh(a) by. The rocket accelerated quickly, allowing it to reach high speeds. However, since the arc angle the rocket off of its straight course, it was not fitting to fly sheet to its potential height because it was curving to t he side. mensural cover to comfortablenes! s of mess From The Ground Measured Height to Puff of Smoke Explanation of Factors         This lab has potential for error because there atomic number 18 many factors that could be both inaccurate or cannot be prevented. at that stead 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 are also natural factors such as the wind. completion         Calculations and answers. Equations. unwrap rocket. Human error. If you want to get a profuse essay, tell it on our website: OrderCustomPaper.com

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