2/29 A model rocket is launched from rest with a con- stant upward acceleration of 3 m/s2 under the ac- tion of a small thruster. The thruster shuts off after 8 seconds, and the rocket continues upward until it reaches its apex. At apex, a small chute opens which ensures that the rocket falls at a constant speed of 0.85 m/s until it impacts the ground. Determine the maximum height h attained by the rocket and the total flight time. Neglect aerodynamic drag during ascent, and assume that the mass of the rocket and the acceleration of gravity are both constant. 0.85 m/s 3 m/s2 Or ww hill

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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windowscommunicationsapps_8wekyb3d8bbwe/LocalState/Files/SO/145/Attachmen
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HEATRALOlvasnal
2/29 A model rocket is launched from rest with a con-
stant upward acceleration of 3 m/s2 under the ac-
tion of a small thruster. The thruster shuts off after
8 seconds, and the rocket continues upward until it
reaches its apex. At apex, a small chute opens which
learly
Pales ensures that the rocket falls at a constant speed of
0.85 m/s until it impacts the ground. Determine the
maximum height h attained by the rocket and the
total flight time. Neglect aerodynamic drag during
ascent, and assume that the mass of the rocket and
the acceleration of gravity are both constant.
To lear
0.85 m/s
D
C
H
3 m/s² Or
3
Transcribed Image Text:cal/Packages/microsoft + windowscommunicationsapps_8wekyb3d8bbwe/LocalState/Files/SO/145/Attachmen CD Page view A Read aloud | Add textDraw HEATRALOlvasnal 2/29 A model rocket is launched from rest with a con- stant upward acceleration of 3 m/s2 under the ac- tion of a small thruster. The thruster shuts off after 8 seconds, and the rocket continues upward until it reaches its apex. At apex, a small chute opens which learly Pales ensures that the rocket falls at a constant speed of 0.85 m/s until it impacts the ground. Determine the maximum height h attained by the rocket and the total flight time. Neglect aerodynamic drag during ascent, and assume that the mass of the rocket and the acceleration of gravity are both constant. To lear 0.85 m/s D C H 3 m/s² Or 3
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