solve correctly thanks Can Someone solve it step by step including all formulae on paperFuture spacecraft (like the HSL HuskySat-3) will orbit the moon on the NASA LunarGateway¹ with a periapsis of 1900km and a period of 6.666 days. Find:a. The semimajor axis a (km) of the orbit.b. The eccentricity e or the orbit.c. The apoapsis of the orbit.d. A spacecraft is released (assume it has the same orbital speed as the gateway, itis released with 0 Av) from the Gateway at a true anomaly of 0=300°. The nextburn must take place at periapsis. How long after release does the burn occur?Show your values for the eccentric anomaly, mean anomaly, and mean angularrate.

Given Data:Periapsis distance(rp=1900km Orbital period T = 6.666 daysTrue anomaly at release =…

Answered: Can Someone solve it step by step…

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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what is the tension T1 in a cord attaching a baby to a scale? what is the tension T2 in the cord attaching the baby to the ceiling? The mass of a rocket sled is 2100KG and the force of friction opposing the motion is 640N. The thrust for the sled is 25900N. What is the acceleration in Metres per second second? A 1140 KG artillery shell is fired from a battleship,.W,hile it is in the barrel of the gun, it experiences an acceleration of 2.2 x 10^4 m/s^2. what net force is exerted on the artillery shell before it leaves the barrel of the gun in Newtons. What is the magnitude of the force exerted on the ship by the artillery shell in Newtons?
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I:56) Solve it in radians per second please
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