II. With external gravitational field In this second part you are asked to analyze rocket propulsion with the present of gravitational field g. This appears for instance when the rocket is launching from the surface of a planet. (1) Describes why you are not allowed to use the momentum conservation here. (2) Evaluate the speed of the rocket measure by inertial observer on the ground as a function of time v(t) if the speed of the gas propulsion with respect to the rocket is vrel and the burning rate is constant dm =constant! dt (3) Plot v(t) that you obtained from point (2) above, for three different values of gravitational field (assuming similar initial mass), which is: • 9moon = 1.62 m/s? Gearth = 9.81 m/s? Ijupiter = 24.79 m/s² %3D %3D in a single plot, if the burn rate is constant dm %3D dt = 1500 kg/s. Analyze your result and describes how the speed increases for each situation!

Principles of Physics: A Calculus-Based Text
5th Edition
ISBN:9781133104261
Author:Raymond A. Serway, John W. Jewett
Publisher:Raymond A. Serway, John W. Jewett
Chapter11: Gravity, Planetary Orbits, And The Hydrogen Atom
Section: Chapter Questions
Problem 57P
icon
Related questions
icon
Concept explainers
Question
I.
With external gravitational field
In this second part you are asked to analyze rocket propulsion with the present of
gravitational field g. This appears for instance when the rocket is launching from the surface
of a planet.
(1) Describes why you are not allowed to use the momentum conservation here.
(2) Evaluate the speed of the rocket measure by inertial observer on the ground as a function
of time v(t) if the speed of the gas propulsion with respect to the rocket is vret and the
burning rate is constant constant!
dm
dt
(3) Plot v(t) that you obtained from point (2) above, for three different values of gravitational
field (assuming similar initial mass), which is:
Imoon = 1.62 m/s?
• Gearth = 9.81 m/s?
Ijupiter = 24.79 m/s?
in a single plot, if the burn
dm
ate is constant
= 1500 kg/s. Analyze your result and
dt
describes how the speed increases for each situation!
20:18
Ai
11/03/2022
Transcribed Image Text:I. With external gravitational field In this second part you are asked to analyze rocket propulsion with the present of gravitational field g. This appears for instance when the rocket is launching from the surface of a planet. (1) Describes why you are not allowed to use the momentum conservation here. (2) Evaluate the speed of the rocket measure by inertial observer on the ground as a function of time v(t) if the speed of the gas propulsion with respect to the rocket is vret and the burning rate is constant constant! dm dt (3) Plot v(t) that you obtained from point (2) above, for three different values of gravitational field (assuming similar initial mass), which is: Imoon = 1.62 m/s? • Gearth = 9.81 m/s? Ijupiter = 24.79 m/s? in a single plot, if the burn dm ate is constant = 1500 kg/s. Analyze your result and dt describes how the speed increases for each situation! 20:18 Ai 11/03/2022
Expert Solution
steps

Step by step

Solved in 5 steps with 1 images

Blurred answer
Knowledge Booster
Gravitational Force
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, physics and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Principles of Physics: A Calculus-Based Text
Principles of Physics: A Calculus-Based Text
Physics
ISBN:
9781133104261
Author:
Raymond A. Serway, John W. Jewett
Publisher:
Cengage Learning
College Physics
College Physics
Physics
ISBN:
9781285737027
Author:
Raymond A. Serway, Chris Vuille
Publisher:
Cengage Learning
Classical Dynamics of Particles and Systems
Classical Dynamics of Particles and Systems
Physics
ISBN:
9780534408961
Author:
Stephen T. Thornton, Jerry B. Marion
Publisher:
Cengage Learning
University Physics Volume 1
University Physics Volume 1
Physics
ISBN:
9781938168277
Author:
William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:
OpenStax - Rice University