The second interval begins at t = 10 and ends at t = 15, so its width is At2 1595 %3D

Algebra & Trigonometry with Analytic Geometry
13th Edition
ISBN:9781133382119
Author:Swokowski
Publisher:Swokowski
Chapter7: Analytic Trigonometry
Section7.2: Trigonometric Equations
Problem 97E
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how to find width

Tutorial Exercise
When we estimate distances from velocity data, it is sometimes necessary to use times to, t1, t2, t3, ... that
are not equally spaced. We can still estimate distances using the time periods At; = t; – t; - 1. For example, a
space shuttle was launched on a mission, the purpose of which was to install a new motor in a satellite. The
table provided gives the velocity data for the shuttle between liftoff and the jettisoning of the solid rocket
boosters. Use these data to estimate the height, h, above Earth's surface of the space shuttle, 62 seconds
after liftoff.
Event
Time (s) Velocity (ft/s)
Launch
Begin roll maneuver
10
185
End roll maneuver
15
319
Throttle to 89%
20
447
Throttle to 67%
32
742
Throttle to 104%
59
1325
Maximum dynamic pressure
62
1445
Solid rocket booster separation
125
4151
Step 1
We can obtain an upper estimate for the height by using the final velocity for each time interval.
The first interval begins att = 0 and ends at t =
10, so its width is
Ati
= 10
10
Step 2
The second interval begins at t = 10 and ends at t = 15, so its width is
Atz =
1595
Transcribed Image Text:Tutorial Exercise When we estimate distances from velocity data, it is sometimes necessary to use times to, t1, t2, t3, ... that are not equally spaced. We can still estimate distances using the time periods At; = t; – t; - 1. For example, a space shuttle was launched on a mission, the purpose of which was to install a new motor in a satellite. The table provided gives the velocity data for the shuttle between liftoff and the jettisoning of the solid rocket boosters. Use these data to estimate the height, h, above Earth's surface of the space shuttle, 62 seconds after liftoff. Event Time (s) Velocity (ft/s) Launch Begin roll maneuver 10 185 End roll maneuver 15 319 Throttle to 89% 20 447 Throttle to 67% 32 742 Throttle to 104% 59 1325 Maximum dynamic pressure 62 1445 Solid rocket booster separation 125 4151 Step 1 We can obtain an upper estimate for the height by using the final velocity for each time interval. The first interval begins att = 0 and ends at t = 10, so its width is Ati = 10 10 Step 2 The second interval begins at t = 10 and ends at t = 15, so its width is Atz = 1595
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