rocket physics pdf

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0000001228 00000 n 0000010696 00000 n 0000002920 00000 n 0000007959 00000 n Learning Objectives: The students will: • Build their own simple astrolabes. 0000008158 00000 n This we recognize as Galileo’s concept of inertia, and this is often termed simply the "Law of Inertia."

0000007048 00000 n 0000006278 00000 n h��`B8�O��H�@��AD1��.�ЮKj�G��N\�Q�)�J |�[��U�Qq��_-�_ �Y��궃Jp��N�_Ǐ,�OLzz�'�>��[\h(��FFThY�F��٩�+p��B� �� >��:@�H(�o��@��H��ܢ��gzEzD�~ȓ�Y�z �Ej7�Q��%lճ�ڷ��Z��h�sw�B��K��R��z6��f��Izp��PT��g��x1��l 68 10. However, the real equations that describe the physics of the rockets are so complicated that certain assumptions are usually made to obtain models that are easier to use. A simple rocket can be made using a plastic bottle filled with a volume of water and pressurized air. 83 13. By continuing to use this site you agree to our use of cookies. 0000001305 00000 n 0000007151 00000 n understanding the physics of Water Rockets. ��Ib�T��1@�n(?��|-i續�i�:�)�KN�"%�y"!�%��f�p�~Wp�s؟{�. 459 0 obj <>stream J. Phys. 0000000996 00000 n %PDF-1.6 %�� The rocket velocity is a function of time,,and increases at a rate Because fuel is leaving the rocket, the mass of the rocket is also a function of xref ?OB� �� Jjظ%��R��H@1:J2&�.̰n��J2��c��H# ��ܪ��4P*�/%H�� 3I��!pdh�r1��:� 0000086159 00000 n %H��6��A�$��=>�x�ȭ�b)�4��c+��Ap@�32l��Ȱ�(�pH�ؽ-�H�=�̟��}��e��@�H�d��ok�?��Mk9J��@�P��m�dRI��H��\�� ckT��c-�2�oC��@IŪ��m*1�k��B�e�� 8K�!�إI/a� �U��9O642�+�I��Z��d!�hj�$��c+�� endstream endobj 9 0 obj 730 endobj 4 0 obj << /Type /Page /Parent 5 0 R /Resources << /Font << /F1 6 0 R /F2 7 0 R >> /ProcSet 2 0 R >> /Contents 8 0 R >> endobj 13 0 obj << /Length 14 0 R /Filter /LZWDecode >> stream 11 35 7 3-2-1 POP! This educators’ guide addresses a growing need for higher- To find out more, see our, Browse more than 70 science journal titles, Read the very best research published in IOP journals, Read open access proceedings from science conferences worldwide, Science and Technology Facilities Council (STFC), Experimental evaluation of the drag coefficient of water rockets by a simple free-fall test, Propulsive efficiency of a biomorphic pulsed-jet underwater vehicle, Modelling the motion of meteors in the Earth's atmosphere, A non-traditional fluid problem: transition between theoretical models from Stokes' to turbulent flow. The tests showed maximum differences with predictions of about 6%.

0000098222 00000 n There are many right ways to teach physics. �>~N) ��sy)��@��(*��I��{� e�JaW�b��W�dq(U7B�'�� 'k��z�ʹh��c�_��f�p@e�BQ@�]B�/\��፬��N��Is��!��6��4� T��yr��$~�6{*. 0000009028 00000 n 0000029652 00000 n �AA�WN�s�� o5� C�@-�H��h}0�@�Q,y��@-��E3y��e�Ql$k�)چ��a 0000095467 00000 n Physics and Model Rockets A Teacher’s Guide and Curriculum for Grades 8-11 ... model rocket, light and sound ener gy are very small and may be ignored. 0000002010 00000 n • Calculate theoretical values for the maximum velocity and endstream endobj startxref

X 62. 0000024111 00000 n 0000106965 00000 n This section looks at the relationships between distance, velocity, acceleration, force, work, impulse, energy and power.

If you have a user account, you will need to reset your password the next time you login. The rocket burns fuel that is then ejected backward with velocity relative to the rocket. 6 Rocket Racer.

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31 1131, https://doi.org/10.1088/0143-0807/31/5/015. 0000010267 00000 n Academia.edu is a platform for academics to share research papers. Purchase this article from our trusted document delivery partners. 0000025393 00000 n 0000001679 00000 n ��n�6�֝��u�#�. 441 0 obj <>/Filter/FlateDecode/ID[<26A2258F264130438EA732BAE4250771><7716FEDAAEDC8942A096C34F2821E7EF>]/Index[413 47]/Info 412 0 R/Length 127/Prev 404640/Root 414 0 R/Size 460/Type/XRef/W[1 3 1]>>stream 0000002332 00000 n

Rocket Physics . Water Rocket Physics Principles Forces and Motion Newton’s First Law – An object at rest remains at rest, and an object in motion remains in motion at constant speed and in a straight line unless acted on by an unbalanced force. This causes an increase in the bottle momentum so that it can be propelled to fairly long distances or heights. Rocket Physics . 5 Straw Rockets. 0000003398 00000 n The computer you are using is not registered by an institution with a subscription to this article. The proposed model is finally used to investigate the temporal evolution of some significant variables during the propulsion and flight of the rocket. is perhaps the most effective way to effectively teach physics so that it becomes both relevant and practical. 0000025632 00000 n Rocket Transportation X. 0000001689 00000 n 0000011511 00000 n A small opening at one end of the chamber allows the gas to escape, and in doing so provides a thrust that propels the rocket in the opposite direction.

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rocket,” a multi-staged vehicle for lifting fireworks to higher altitudes. Find out more. 413 0 obj <> endobj A large sky rocket (first stage) carried a smaller sky rocket (second stage). A rocket in its simplest form is a chamber enclosing a gas under pressure. When the rocket is sitting on the launcher, the forces are balanced because the surface of the launcher pushes the 0000106455 00000 n Physics Aeronautics: A Contextual Approach for Learning Physics. Bottle Rocket Lab Physics Concepts: Newton’s 1 st Law - Every object in a state of uniform motion tends to remain in that state of motion unless an external force is applied to it. 0000004542 00000 n 11 0 obj <> endobj

0 Parachute Area Versus Drop Time X. European Journal of Physics, trailer Number 5, 1 Departamento de Energía, Universidad de Oviedo, Campus de Viesques, 33271 Gijón, Asturias, Spain, 2 Departamento de IMEM, Universidad de Extremadura, Escuela de Ingenierías Industriales, 06071 Badajoz, Extremadura, Spain, Received 15 June 2010 74 11. We suppose that the rocket is burning fuel at a rate of b kg s-1 so that, at time t, the mass of the rocket-plus-remaining-fuel is m = m0 − bt. For air-water rockets, Bernoulli’s equation gives uex 2P / ρw = + where P+ is the internal H�b```f``]��$�02 � e�X��p&��B�qA��( b=(f`�w1�e��h�0��3100Y0�0� ��y��3�&��@:*n��˳�{��+�*�\ ��e�3��ma`:�H3�7@� �#� endstream endobj 74 0 obj 158 endobj 27 0 obj << /Type /Page /Parent 22 0 R /Resources 28 0 R /Contents [ 39 0 R 43 0 R 45 0 R 49 0 R 53 0 R 55 0 R 57 0 R 59 0 R ] /MediaBox [ 0 0 612 792 ] /CropBox [ 0 0 612 792 ] /Rotate 0 >> endobj 28 0 obj << /ProcSet [ /PDF /Text ] /Font << /TT2 35 0 R /TT4 30 0 R /TT6 31 0 R /TT8 33 0 R /TT9 40 0 R /TT10 46 0 R /TT12 50 0 R >> /ExtGState << /GS1 67 0 R >> /ColorSpace << /Cs6 37 0 R >> >> endobj 29 0 obj << /Type /FontDescriptor /Ascent 905 /CapHeight 0 /Descent -211 /Flags 32 /FontBBox [ -665 -325 2000 1006 ] /FontName /HPGOPB+Arial /ItalicAngle 0 /StemV 0 /FontFile2 63 0 R >> endobj 30 0 obj << /Type /Font /Subtype /TrueType /FirstChar 32 /LastChar 84 /Widths [ 250 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 500 500 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 722 0 722 0 667 0 0 778 389 0 778 0 944 722 778 611 0 722 0 667 ] /Encoding /WinAnsiEncoding /BaseFont /HPGONB+TimesNewRoman,Bold /FontDescriptor 34 0 R >> endobj 31 0 obj << /Type /Font /Subtype /TrueType /FirstChar 32 /LastChar 32 /Widths [ 278 ] /Encoding /WinAnsiEncoding /BaseFont /HPGOPB+Arial /FontDescriptor 29 0 R >> endobj 32 0 obj << /Type /FontDescriptor /Ascent 891 /CapHeight 656 /Descent -216 /Flags 98 /FontBBox [ -498 -307 1120 1023 ] /FontName /HPGPAH+TimesNewRoman,Italic /ItalicAngle -15 /StemV 83.31799 /XHeight 0 /FontFile2 60 0 R >> endobj 33 0 obj << /Type /Font /Subtype /TrueType /FirstChar 32 /LastChar 121 /Widths [ 250 0 0 0 0 0 0 0 0 0 0 0 250 0 250 278 0 0 0 0 0 0 0 0 0 0 0 333 0 0 0 0 0 611 0 0 0 611 611 0 0 333 0 0 0 0 0 0 611 0 611 0 556 0 611 0 0 0 0 0 0 0 0 0 0 500 500 444 500 444 278 500 500 278 0 444 278 722 500 500 500 500 389 389 278 500 444 667 444 444 ] /Encoding /WinAnsiEncoding /BaseFont /HPGPAH+TimesNewRoman,Italic /FontDescriptor 32 0 R >> endobj 34 0 obj << /Type /FontDescriptor /Ascent 891 /CapHeight 656 /Descent -216 /Flags 34 /FontBBox [ -558 -307 2000 1026 ] /FontName /HPGONB+TimesNewRoman,Bold /ItalicAngle 0 /StemV 160 /FontFile2 62 0 R >> endobj 35 0 obj << /Type /Font /Subtype /TrueType /FirstChar 32 /LastChar 122 /Widths [ 250 0 408 0 0 833 0 180 333 333 0 0 250 333 250 278 500 500 500 500 500 500 500 0 0 500 278 0 0 564 0 444 0 722 667 667 722 611 556 0 722 333 0 0 611 889 722 722 0 0 667 556 611 0 0 944 722 722 0 0 0 0 0 0 0 444 500 444 500 444 333 500 500 278 278 500 278 778 500 500 500 500 333 389 278 500 500 722 500 500 444 ] /Encoding /WinAnsiEncoding /BaseFont /HPGOLL+TimesNewRoman /FontDescriptor 36 0 R >> endobj 36 0 obj << /Type /FontDescriptor /Ascent 891 /CapHeight 656 /Descent -216 /Flags 34 /FontBBox [ -568 -307 2000 1007 ] /FontName /HPGOLL+TimesNewRoman /ItalicAngle 0 /StemV 94 /XHeight 0 /FontFile2 61 0 R >> endobj 37 0 obj [ /ICCBased 66 0 R ] endobj 38 0 obj 511 endobj 39 0 obj << /Filter /FlateDecode /Length 38 0 R >> stream

0000006895 00000 n Export citation and abstract 0000026100 00000 n 0000001755 00000 n 0000002756 00000 n Part of the mechanical ener gy is transformed to the kinetic ener gy of the rocketÕ s motion. Version 1.02 June 2007 Warning: Water Rocketeering is a potentially dangerous activity and individuals following the instructions herein do so at their own risk. trailer << /Size 75 /Info 23 0 R /Root 26 0 R /Prev 185289 /ID[<8e74921983a25f542c95881ba667a83f><69fd44172f8a65cc05989537105b02ea>] >> startxref 0 %%EOF 26 0 obj << /Type /Catalog /Pages 22 0 R /Metadata 24 0 R /PageLabels 21 0 R >> endobj 73 0 obj << /S 67 /L 189 /Filter /FlateDecode /Length 74 0 R >> stream 0000005920 00000 n 0000065407 00000 n 0000010815 00000 n Volume 31, The validity of the model is checked by a series of field tests. 0000008403 00000 n X X. X 58. Example. When the large rocket burned out, the smaller one continued to a higher altitude before showering the sky with glowing cinders. The Nose Cone Experts X. 10-year back file (where available). 0000012483 00000 n %PDF-1.6 %�� content_copy. Rocket motion has been traditionally used in the classroom as an application of some basic principles of physics to a real world situation [1–3]. 0000009664 00000 n 0000007338 00000 n

0 Teaching by inquiry in context . rocket,” a multi-staged vehicle for lifting fireworks to higher altitudes. 25 0 obj << /Linearized 1 /O 27 /H [ 1440 270 ] /L 185917 /E 107966 /N 6 /T 185299 >> endobj xref 25 50 0000000016 00000 n h�bbd``b`�Y@��H�Y�� BH��X@, k��b�] �d��U��A��@�r}L'��G��f �&be �Z �Q�� r#]�� | endstream endobj startxref 0 %%EOF 749 0 obj <>stream Rocket Propulsion A rocket at time t = 0 is moving with speed v r,0 in the positive x-direction in empty space. ��00ʱT3�0�d�g�g��j�2�E��,��2W�{o�1?�۝��^�$�΢+�YY��eZ�NA*�� H3}�HK2�� "�w�ش� � �< 0000009049 00000 n

90 15. LESSON PLAN . 0000003756 00000 n 0000098144 00000 n <]>> management contact at your company. 0000002517 00000 n Water rockets are widely used as an educational activity, and several mathematical models have been proposed to investigate and predict their physics. 0000008042 00000 n The rate of increase of mass with time is dm dt =−b and is supposed constant with time. 0000004766 00000 n 0000003082 00000 n 0000003531 00000 n 0000001710 00000 n Paper Rockets X. X 43. Form and we will follow up with your librarian or Institution on your behalf. H�TQ�n�0��-��1��(r��(�P �Y��`,c 0000085954 00000 n