. When we estimate distances from velocity data, it is some- times necessary to use times fo, f1, fz, fz, ... that are not equally spaced. We can still estimate distances using the time periods At; = ti – ti-1. For example, on May 7, 1992, the space shuttle Endeavour was launched on mission STS-49, the purpose of which was to install a new perigee kick motor in an Intelsat communications satellite. The table, provided by NASA, gives the velocity data for the shuttle between liftoff and the jettisoning of the solid rocket boosters. Use these data to estimate the height above the earth's surface of the space shuttle Endeavour, 62 seconds after liftoff. Event Time (s) Velocity (ft/s) Launch Begin roll maneuver End roll maneuver 10 185 15 319 Throttle to 89% Throttle to 67% 20 447 32 742 Throttle to 104% 59 1325 Maximum dynamic pressure Solid rocket booster separation 62 1445 125 4151
. When we estimate distances from velocity data, it is some- times necessary to use times fo, f1, fz, fz, ... that are not equally spaced. We can still estimate distances using the time periods At; = ti – ti-1. For example, on May 7, 1992, the space shuttle Endeavour was launched on mission STS-49, the purpose of which was to install a new perigee kick motor in an Intelsat communications satellite. The table, provided by NASA, gives the velocity data for the shuttle between liftoff and the jettisoning of the solid rocket boosters. Use these data to estimate the height above the earth's surface of the space shuttle Endeavour, 62 seconds after liftoff. Event Time (s) Velocity (ft/s) Launch Begin roll maneuver End roll maneuver 10 185 15 319 Throttle to 89% Throttle to 67% 20 447 32 742 Throttle to 104% 59 1325 Maximum dynamic pressure Solid rocket booster separation 62 1445 125 4151
College Physics
1st Edition
ISBN:9781938168000
Author:Paul Peter Urone, Roger Hinrichs
Publisher:Paul Peter Urone, Roger Hinrichs
Chapter3: Two-dimensional Kinematics
Section: Chapter Questions
Problem 64PE: (a) Use the distance and velocity data in Figure 3.64 to find the rate of expansion as a function of...
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Question
![. When we estimate distances from velocity data, it is some-
times necessary to use times fo, f1, fz, fz, ... that are not
equally spaced. We can still estimate distances using the
time periods At; = ti – ti-1. For example, on May 7, 1992,
the space shuttle Endeavour was launched on mission
STS-49, the purpose of which was to install a new perigee
kick motor in an Intelsat communications satellite. The
table, provided by NASA, gives the velocity data for the
shuttle between liftoff and the jettisoning of the solid
rocket boosters. Use these data to estimate the height
above the earth's surface of the space shuttle Endeavour,
62 seconds after liftoff.
Event
Time (s)
Velocity (ft/s)
Launch
Begin roll maneuver
End roll maneuver
10
185
15
319
Throttle to 89%
Throttle to 67%
20
447
32
742
Throttle to 104%
59
1325
Maximum dynamic pressure
Solid rocket booster separation
62
1445
125
4151](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F8fa03e37-bc1f-4928-ba0b-4a340a51e0a3%2F10d895cd-4e55-4e77-a3c3-aad13fba5a97%2Fwi0t5o.png&w=3840&q=75)
Transcribed Image Text:. When we estimate distances from velocity data, it is some-
times necessary to use times fo, f1, fz, fz, ... that are not
equally spaced. We can still estimate distances using the
time periods At; = ti – ti-1. For example, on May 7, 1992,
the space shuttle Endeavour was launched on mission
STS-49, the purpose of which was to install a new perigee
kick motor in an Intelsat communications satellite. The
table, provided by NASA, gives the velocity data for the
shuttle between liftoff and the jettisoning of the solid
rocket boosters. Use these data to estimate the height
above the earth's surface of the space shuttle Endeavour,
62 seconds after liftoff.
Event
Time (s)
Velocity (ft/s)
Launch
Begin roll maneuver
End roll maneuver
10
185
15
319
Throttle to 89%
Throttle to 67%
20
447
32
742
Throttle to 104%
59
1325
Maximum dynamic pressure
Solid rocket booster separation
62
1445
125
4151
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