2/230 The third stage of a rocket is injected by its booster with a velocity u of 15 000 km/h at A into an un- powered coasting flight to B. At B its rocket motor is ignited when the trajectory makes an angle of 20⁰ with the horizontal. Operation is effectively above the atmosphere, and the gravitational acceleration during this interval may be taken as 9 m/s², con- stant in magnitude and direction. Determine the time t to go from A to B. (This quantity is needed in the design of the ignition control system.) Also determine the corresponding increase h in altitude. y A u 45° Horiz. B 20° Horiz. رفع جك
2/230 The third stage of a rocket is injected by its booster with a velocity u of 15 000 km/h at A into an un- powered coasting flight to B. At B its rocket motor is ignited when the trajectory makes an angle of 20⁰ with the horizontal. Operation is effectively above the atmosphere, and the gravitational acceleration during this interval may be taken as 9 m/s², con- stant in magnitude and direction. Determine the time t to go from A to B. (This quantity is needed in the design of the ignition control system.) Also determine the corresponding increase h in altitude. y A u 45° Horiz. B 20° Horiz. رفع جك
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:2/230 The third stage of a rocket is injected by its booster
with a velocity u of 15 000 km/h at A into an un-
powered coasting flight to B. At B its rocket motor
is ignited when the trajectory makes an angle of 20⁰
with the horizontal. Operation is effectively above
the atmosphere, and the gravitational acceleration
during this interval may be taken as 9 m/s², con-
stant in magnitude and direction. Determine the
time t to go from A to B. (This quantity is needed
in the design of the ignition control system.) Also
determine the corresponding increase h in altitude.
y
1
A
u
45°
Horiz.
B
-x
20°
Horiz.
رفع جك
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