A rocket failed to put a satellite into MEO circular orbit (18,000km altitude). Instead it ended in an elliptical orbit with a perigee altitude of 1500km and an e= 0.66667. a. Draw the intended and failed orbits. b. Calculate the Av for a single maneuver to change the elliptical orbit into the circular. Include: ii. iii. i. Identify in your drawing from (a) where the Av takes place. magnitude and direction of the Av [Partial answer: Av = 2.8614 km/s] the change in the flight-path angle Ay [Answer: 67.910°] c. Calculate the Hohmann transfer & compare total Av's (magnitudes). Identify the Hohmann transfer in your drawing. [Partial answers: AVTot = 1.6553 km/s or AV Tot = 3.3686 km/s]
A rocket failed to put a satellite into MEO circular orbit (18,000km altitude). Instead it ended in an elliptical orbit with a perigee altitude of 1500km and an e= 0.66667. a. Draw the intended and failed orbits. b. Calculate the Av for a single maneuver to change the elliptical orbit into the circular. Include: ii. iii. i. Identify in your drawing from (a) where the Av takes place. magnitude and direction of the Av [Partial answer: Av = 2.8614 km/s] the change in the flight-path angle Ay [Answer: 67.910°] c. Calculate the Hohmann transfer & compare total Av's (magnitudes). Identify the Hohmann transfer in your drawing. [Partial answers: AVTot = 1.6553 km/s or AV Tot = 3.3686 km/s]
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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can someone solve this step by step on a paper specially the figure
![A rocket failed to put a satellite into MEO circular orbit (18,000km altitude). Instead it
ended in an elliptical orbit with a perigee altitude of 1500km and an e= 0.66667.
a. Draw the intended and failed orbits.
b. Calculate the Av for a single maneuver to change the elliptical orbit into the
circular. Include:
ii.
iii.
i. Identify in your drawing from (a) where the Av takes place.
magnitude and direction of the Av [Partial answer: Av = 2.8614 km/s]
the change in the flight-path angle Ay [Answer: 67.910°]
c. Calculate the Hohmann transfer & compare total Av's (magnitudes). Identify the
Hohmann transfer in your drawing. [Partial answers: AVTot = 1.6553 km/s or AV Tot
= 3.3686 km/s]](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fdf700b2b-ee54-42e6-9a3e-c60c572fd501%2Fd2f6301b-8667-4c52-8ad1-6ae840d6af48%2Fom707ue_processed.png&w=3840&q=75)
Transcribed Image Text:A rocket failed to put a satellite into MEO circular orbit (18,000km altitude). Instead it
ended in an elliptical orbit with a perigee altitude of 1500km and an e= 0.66667.
a. Draw the intended and failed orbits.
b. Calculate the Av for a single maneuver to change the elliptical orbit into the
circular. Include:
ii.
iii.
i. Identify in your drawing from (a) where the Av takes place.
magnitude and direction of the Av [Partial answer: Av = 2.8614 km/s]
the change in the flight-path angle Ay [Answer: 67.910°]
c. Calculate the Hohmann transfer & compare total Av's (magnitudes). Identify the
Hohmann transfer in your drawing. [Partial answers: AVTot = 1.6553 km/s or AV Tot
= 3.3686 km/s]
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