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 itended 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 thecircular. 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 theHohmann transfer in your drawing. [Partial answers: AVTot = 1.6553 km/s or AV Tot= 3.3686 km/s]

Step 1: Step 2: Step 3: Step 4:

Answered: A rocket failed to put a satellite into…

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

See similar textbooks

Similar questions

8.7 On a date when the earth was 147.4(10°) km from the sun, a spacecraft parked in a 200-km- altitude circular earth orbit was launched directly into an elliptical orbit around the sun with perihelion of 120(10°) km and aphelion equal to the earth's distance from the sun on the launch date. Calculate the delta-v required and v. of the departure hyperbola. {Ans.: Av = 3.34 km/s, v = 1.579 km/s} %3D
6.17 A spacecraft is in a 300-km circular earth orbit. Calculate (a) The total delta-v required for the bielliptical transfer to the 3000-km-altitude coplanar circular orbit shown. (b) The total transfer time. {Ans.: (a) 2.039 km/s; (b) 2.86 h} 340 CHAPTER 6 ORBITAL MANEUVERS e = 0.3 3000 km 300 km AUA CAUC AUB
Can Someone solve it step by step including all formulae on paper
NOTE: Wherever applicable, you may use = 398600 km³s-² and R = 6378 km. Problem 1 A spacecraft in a prograde Earth orbit passed periapsis exactly 28.5 hours ago with a specific angular momentum of 81574.30 km²s 2. The spacecraft will reach apoapsis in exactly 7.5 hours. a. Compute the eccentricity, e.
6.20 Satellites A and B are in the same circular orbit of radius r. B is 180° ahead of A. Calculate the semimajor axis of a phasing orbit in which A will rendezvous with B after just one revolution in the phasing orbit. {Ans.: a = 0.63r} PROBLEMS 341 B F Phasing orbit
7. Your spacecraft is in an. initial 200 km altitude circular earth orbit. Performing a Hohmann transfer compute: a) the TOTAL delta-v required for a Hohmann transfer to a 1000 km altitude coplanar circular earth orbit. b) What is the transfer time in minutes?
solve correctly thanks
Find ecentricity of new orbit..do not give copied solution from chegg.. wrong ans will be devoted..
A mission for disaster monitoring is launched in a circular Sun-Synchronous with semi-major axis a = : 7027.46558 km. a. Compute the orbit period. Also determind how many revolutions the spacecraft completes in a repeat cycle of 19 days? [15 points] b. Compute the distance in km between two consecutive tracks at the equator and show that the minimum distance between tracks in one repeat cycle is 143.125 km. [15 points] c. The Earth orbit angular velocity around the Sun is 0.9860/day. Compute the inclination required for this orbit to be Sun-synchronous, considering that the secular variation of the right ascension of ascending node due to Earth's oblateness is given by 3nJ₂R² 2a² (1 — e²)² in which n is the mean motion of the orbit. Show that the orbit is retrograde. [20 points] d. For this spacecraft, compute the minimum field of view of an onboard camera that enables the global coverage of the Earth. In your calculations you can assume a flat Earth and the camera always pointing in…
Q1) A team of engineering students designs a medium-size catapult which launches 8-lb steel spheres. The launch speed is v, = 80 ft/sec the launch angle is 0 = 35° above the horizontal, and the launch positionis 6 ft above ground level. The students use an athletic field with an adjoining slope topped by an 8-ft fence as shown. Determine: (a) the x-y coordinates of the point of first impact. (b) the time duration of the flight. (c) the maximum height h above the horizontal field attained by the ball. (d) the velocity (expressed as a vector) with which the projectile strikes the ground vo = 80 ft/sec fence 8' e = 35° 20 -100- 30
Part A: What is the period of the spacecraft's orbit? T=___s Part B: Using conservation of angular momentum, find the ratio of the spacecraft's speed at perigee to its speed at apogee. (Vperigee)/(Vapogee)=___ Part C: Using conservation of energy, find the speed at perigee and the speed at apogee. Vperigee,Vapogee=___m/s Part D: It is necessary to have the spacecraft escape from the earth completely. If the spacecraft's rockets are fired at perigee, by how much would the speed have to be increased to achieve this? delta(perigee)=___m/s Part E: What if the rockets were fired at apogee? delta(apogee)=___m/s Part F: Which point in the orbit is more efficient to use and why?
6.13 Two geocentric elliptical orbits have common apse lines and their perigees are on the same side of the earth. The first orbit has a perigee radius of r, second orbit r, 32, 000 km and e = 0.5. (a) Find the minimum total delta-v and the time of flight for a transfer from the perigee of the inner orbit to the apogee of the outer orbit. = 7000 km and e = 0.3, whereas for the (b) Do part (a) for a transfer from the apogee of the inner orbit to the perigee of the outer orbit. {Ans.: (a) Avtotal 4.66 h} 2.388 km/s, time of flight (TOF) = 16.2 h; (b) Aviotal = 3.611 km/s, TOF = %3D e = 0.5 Earth e = 0.3 1) A B 7000 km 32,000 km

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS