find mass of planet given radius and period

A small triangular area AA is swept out in time tt. centripetal = v^2/r meters. negative 11 meters cubed per kilogram second squared for the universal gravitational By observing the orbital period and orbital radius of small objects orbiting larger objects, we can determine the mass of the larger objects. and you must attribute OpenStax. Since the distance Earth-Moon is about the same as in your example, you can write Imagine I have no access to information outside this question and go from there. Manage Settings From this analysis, he formulated three laws, which we address in this section. Mass of Jupiter = a x a x a/p x p. Mass of Jupiter = 4.898 x 4.898 x 4.898/0.611 x 0.611. How do we know the mass of the planets? I attempted to find the velocity from the radius (2.6*10^5) and the time (2.5hr*60*60=9000s) The next step is to connect Kepler's 3rd law to the object being orbited. (The parabola is formed only by slicing the cone parallel to the tangent line along the surface.) These areas are the same: A1=A2=A3A1=A2=A3. Distance between the object and the planet. Visit this site for more details about planning a trip to Mars. How do I calculate evection and variation for the moon in my simple solar system model? seconds. Comparing the areas in the figure and the distance traveled along the ellipse in each case, we can see that in order for the areas to be equal, the planet must speed up as it gets closer to the Sun and slow down as it moves away. Learn more about our Privacy Policy. However, it seems (from the fact that the object is described as being "at rest") that your exercise is not assuming an inertial reference frame, but rather a rotating reference frame matching the rotation of the planet. xYnF}Gh7\.S !m9VRTh+ng/,4sY~TfeAe~[zqqR f2}>(c6PXbN%-o(RgH_4% CjA%=n o8!uwX]9N=vH{'n^%_u}A-tf>4\n These conic sections are shown in Figure 13.18. Our mission is to improve educational access and learning for everyone. T 1 2 T 2 2 = r 1 3 r 2 3, where T is the period (time for one orbit) and r is the average distance (also called orbital radius). To do that, I just used the F=ma equation, with F being the force of gravity, m being the mass of the planet, and a =v^2/r. meaning your planet is about $350$ Earth masses. Online Web Apps, Rich Internet Application, Technical Tools, Specifications, How to Guides, Training, Applications, Examples, Tutorials, Reviews, Answers, Test Review Resources, Analysis, Homework Solutions, Worksheets, Help, Data and Information for Engineers, Technicians, Teachers, Tutors, Researchers, K-12 Education, College and High School Students, Science Fair Projects and Scientists I'm sorry I cannot help you more: I'm out of explanations. But I come out with an absurdly large mass, several orders of magnitude too large. Nagwa uses cookies to ensure you get the best experience on our website. So, without ever touching a star, astronomers use mathematics and known physical laws to figure out its mass. The Mass of a planet The mass of the planets in our solar system is given in the table below. This yields a value of 2.671012m2.671012m or 17.8 AU for the semi-major axis. Newton's second Law states that without such an acceleration the object would simple continue in a straight line. Find MP in Msol: We assume that the orbit of the planet in question is mainly circular. Is there such a thing as "right to be heard" by the authorities? measurably perturb the orbits of the other planets? = seconds to years: s2hr = seconds to hours: r2d = radians to degrees: d2r = degrees to radians: M = mass: R = radius: rho = density : Ve = escape velocity: Ps = spin period: J2 = oblateness: Hr = Hill Radius: gs = Surface Gravity: tilt = tilt: a = Semimajor axis: i = inclination: e = eccentricity: Po . I need to calculate the mass given only the moon's (of this specific system) orbital period and semimajor axis. Planets in Order from Smallest to Largest. Give your answer in scientific Doppler radio measurement from Earth. You may find the actual path of the Moon quite surprising, yet is obeying Newtons simple laws of motion. We can resolve the linear momentum into two components: a radial component pradprad along the line to the Sun, and a component pperppperp perpendicular to rr. Interpreting non-statistically significant results: Do we have "no evidence" or "insufficient evidence" to reject the null? In practice, that must be part of the calculations. By observing the time between transits, we know the orbital period. then you must include on every digital page view the following attribution: Use the information below to generate a citation. Nagwa is an educational technology startup aiming to help teachers teach and students learn. We know that the path is an elliptical orbit around the sun, and it grazes the orbit of Mars at aphelion. For the Moons orbit about Earth, those points are called the perigee and apogee, respectively. , which is equal to 105 days, and days is not the SI unit of time. For example, the best height for taking Google Earth imagery is about 6 times the Earth's radius, \(R_e\). The values of and e determine which of the four conic sections represents the path of the satellite. The purple arrow directed towards the Sun is the acceleration. divided by squared. 2023 Scientific American, a Division of Springer Nature America, Inc. Once you have arrived at Mars orbit, you will need another velocity boost to move into that orbit, or you will stay on the elliptical orbit and simply fall back to perihelion where you started. If there are any complete answers, please flag them for moderator attention. Until recent years, the masses of such objects were simply estimates, based Then, for Charon, xC=19570 km. In fact, Equation 13.8 gives us Keplers third law if we simply replace r with a and square both sides. distant planets orbit to learn the mass of such a large and far away object as a By observing the time it takes for the satellite to orbit its primary planet, we can utilize Newton's equations to infer what the mass of the planet must be. In Satellite Orbits and Energy, we derived Keplers third law for the special case of a circular orbit. It may not display this or other websites correctly. Finally, if the total energy is positive, then e>1e>1 and the path is a hyperbola. There are four different conic sections, all given by the equation. As before, the Sun is at the focus of the ellipse. When the Moon and the Earth were just 30,000 years old, a day lasted only six hours! But few planets like Mercury and Venus do not have any moons. The time taken by an object to orbit any planet depends on that. Orbital motion (in a plane) Speed at a given mean anomaly. Calculate the lowest value for the acceleration. (T is known), Hence from the above equation, we only need distance between the planet and the moon r and the orbital period of the moon T, So scientists use this method to determine the, Now as we knew how to measure the planets mass, scientists used their moons for planets like, Space probes are one of the ways for determining the gravitational pull and hence the mass of a planet. I attempted to use Kepler's 3rd Law, calculate. Kepler's third law calculator solving for planet mass given universal gravitational constant, . 9 / = 1 7 9 0 0 /. Because the value of and G is constant and known. First, for visual clarity, lets Mar 18, 2017 at 3:12 Your answer is off by about 31.5 Earth masses because you used a system that approximates this system. Apparently I can't just plug these in to calculate the planets mass. Newton, building on other people's observations, showed that the force between two objects is proportional to the product of their masses and decreases with the square of the distance: where \(G=6.67 \times 10^{-11}\) m\(^3\)kg s\(^2\) is the gravitational constant. Recall that a satellite with zero total energy has exactly the escape velocity. Every path taken by m is one of the four conic sections: a circle or an ellipse for bound or closed orbits, or a parabola or hyperbola for unbounded or open orbits. The time taken by an object to orbit any planet depends on that planets gravitational pull. Connect and share knowledge within a single location that is structured and easy to search. the average distance between the two objects and the orbital periodB.) \frac{M_pT_s^2}{a_s^3}=\frac{M_E T_M^2}{a_M^3} \quad \Rightarrow \quad Kepler's 3rd law can also be used to determine the fast path (orbit) from one planet to another. The same (blue) area is swept out in a fixed time period. Whereas, with the help of NASAs spacecraft. Figure 13.19 shows the case for a trip from Earths orbit to that of Mars. $$ Why would we do this? The mass of Earth is 598 x 1022 kg, which is 5,980,000,000,000,000,000,000,000 kg (598 with 22 zeros after that). consent of Rice University. By astronomically This "bending" is measured by careful tracking and 4 0 obj have moons, they do exert a small pull on one another, and on the other planets of the solar system. This gravitational force acts along a line extending from the center of one mass to the center of the second mass. For ellipses, the eccentricity is related to how oblong the ellipse appears. Before we can calculate, we must convert the value for into units of metres per second: = 1 7. In the above discussion of Kepler's Law we referred to \(R\) as the orbital radius. Which reverse polarity protection is better and why? More Planet Variables: pi ~ 3.141592654 . And those objects may be any moon (natural satellite), nearby passing spacecraft, or any other object passing near it. With this information, model of the planets can be made to determine if they might be convecting like Earth, and if they might have plate tectonics. Knowing the mass of a planet is the most fundamental geophysical observation of that planet, and with other observations it can be used to determine the whether another planet has a core, and relative size of the core and mantle. GIVEN: T 2 /R 3 = 2.97 x 10-19 s 2 /m 3. The orbital speed formula is provided by, V o r b i t = G M R Where, G = gravitational constant M = mass of the planet r = radius. formula well use. $$ They use this method of gravitational disturbance of the orbital path of small objects such as to measure the mass of the asteroids. Why the obscure but specific description of Jane Doe II in the original complaint for Westenbroek v. Kappa Kappa Gamma Fraternity? Its pretty cool that given our According to Newtons 2nd law of motion: Thus to maintain the orbital path the gravitational force acting by the planet and the centripetal force acting by the moon should be equal. As with Keplers first law, Newton showed it was a natural consequence of his law of gravitation. use the mass of the Earth as a convenient unit of mass (rather than kg). You do not want to arrive at the orbit of Mars to find out it isnt there. If you would like to change your settings or withdraw consent at any time, the link to do so is in our privacy policy accessible from our home page.. Now we will calculate the mass M of the planet. citation tool such as, Authors: William Moebs, Samuel J. Ling, Jeff Sanny. Identify blue/translucent jelly-like animal on beach. INSTRUCTIONS: Choose units and enter the following: Planetary Mass (M): The calculator returns the mass (M) in kilograms. Whereas, with the help of NASAs spacecraft MESSENGER, scientists determined the mass of the planet mercury accurately. I figured it out. << /Length 5 0 R /Filter /FlateDecode >> Homework Equations I'm unsure what formulas to use, though these seem relevant. This is force is called the Centripetal force and is proportional to the velocity of the orbiting object, but decreases proportional to the distance. of distant astronomical objects (Exoplanets) is determined by the objects apparent size and shape. For the case of orbiting motion, LL is the angular momentum of the planet about the Sun, rr is the position vector of the planet measured from the Sun, and p=mvp=mv is the instantaneous linear momentum at any point in the orbit. With the help of the moons orbital period, we can determine the planets gravitational pull. We and our partners use cookies to Store and/or access information on a device. (You can figure this out without doing any additional calculations.) %%EOF Create your free account or Sign in to continue. understanding of physics and some fairly basic math, we can use information about a It only takes a minute to sign up. The other two purple arrows are acceleration components parallel (tangent to the orbit) and perpendicular to the velocity. In equation form, this is. Space probes are one of the ways for determining the gravitational pull and hence the mass of a planet. Browse other questions tagged, Start here for a quick overview of the site, Detailed answers to any questions you might have, Discuss the workings and policies of this site. group the units over here, making sure to distribute the proper exponents. Continue reading with a Scientific American subscription. $$ A more precise calculation would be based on For an object orbiting another object, Newton also observed that the orbiting object must be experiencing an acceleration because the velocity of the object is constantly changing (change direction, not speed, but this is still an acceleration). The other important thing to note, is that it is not very often that the orbits line up exactly such that a Hohmann transfer orbit is possible. Therefore the shortest orbital path to Mars from Earth takes about 8 months. For elliptical orbits, the point of closest approach of a planet to the Sun is called the perihelion. Is there a scale large enough to hold a planet? that is challenging planetary scientists for an explanation. at least that's what i think?) In order to use gravity to find the mass of a planet, we must somehow measure the strength of its "tug" on another object. We also need the Constant of Proportionality in the Law of Universal Gravitation, G. This value was experimentally determined The Planet's Mass from Acceleration and Radius calculator computes the mass of planet or moon based on the radius (r), acceleration due to gravity on the surface (a) and the universal gravitational constant (G). In these activities students will make use of these laws to calculate the mass of Jupiter with the aid of the Stellarium (stellarium.org) astronomical software. Just like a natural moon, a spacecraft flying by an asteroid We can use these three equalities Explore our digital archive back to 1845, including articles by more than 150 Nobel Prize winners. Stack Exchange network consists of 181 Q&A communities including Stack Overflow, the largest, most trusted online community for developers to learn, share their knowledge, and build their careers. Kepler's third law provides an accurate description of the period and distance for a planet's orbits about the sun. What is the physical meaning of this constant and what does it depend on? By observing the time between transits, we know the orbital period. The most efficient method was discovered in 1925 by Walter Hohmann, inspired by a popular science fiction novel of that time. Can you please explain Bernoulli's equation. Using a telescope, one can detect other planets around stars by observing a drop in the brightness of the star as the planet transits between the star and the telescope. So if we can measure the gravitational pull or acceleration due to the gravity of any planet, we can measure the mass of the planet. For example, NASAs space probes, were used to measuring the outer planets mass. Mars is closest to the Sun at Perihelion and farthest away at Aphelion. areal velocity = A t = L 2m. An ellipse has several mathematical forms, but all are a specific case of the more general equation for conic sections. Since we know the potential energy from Equation 13.4, we can find the kinetic energy and hence the velocity needed for each point on the ellipse. Answer. As you were likely told in elementary school, legend states that while attempting to escape an outbreak of the bubonic plague, Newton retreated to the countryside, sat in an orchard, and was hit on the head with an apple. If the proportionality above it true for each planet, then we can set the fractions equal to each other, and rearrange to find, \[\frac{T_1^2}{T_2^2}=\frac{R_1^3}{R_2^3}\]. \[M_e=\frac{4\pi^2}{G} \left(\frac{R_{moon}^3}{T_{moon}^2}\right) \nonumber\]. 994 0 obj <> endobj Conversions: gravitational acceleration (a) This situation has been observed for several comets that approach the Sun and then travel away, never to return. JavaScript is disabled. Hence from the above equation, we only need distance between the planet and the moon r and the orbital period of the moon T to calculate the mass of a planet. So if we can measure the gravitational pull or acceleration due to the gravity of any planet, we can measure the mass of the planet. Though most of the planets have their moons that orbit the planet. possible period, given your uncertainties. Instead I get a mass of 6340 suns. Substituting them in the formula, Other satellites monitor ice mass, vegetation, and all sorts of chemical signatures in the atmosphere. You can also use orbital velocity and work it out from there. Recall the definition of angular momentum from Angular Momentum, L=rpL=rp. So just to clarify the situation here, the star at the center of the planet's orbit is not the sun. For this, well need to convert to That opportunity comes about every 2 years. This is a direct application of Equation \ref{eq20}. If the total energy is exactly zero, then e=1e=1 and the path is a parabola. These are the two main pieces of information scientists use to measure the mass of a planet. A circle has zero eccentricity, whereas a very long, drawn-out ellipse has an eccentricity near one. To determine the velocities for the ellipse, we state without proof (as it is beyond the scope of this course) that total energy for an elliptical orbit is. $$M=\frac{4\pi^2a^3}{GT^2}$$ Planetary scientists also send orbiters to other planets to make similar measurements (okay not vegetation). The first term on the right is zero because rr is parallel to pradprad, and in the second term rr is perpendicular to pperppperp, so the magnitude of the cross product reduces to L=rpperp=rmvperpL=rpperp=rmvperp. To obtain a reasonable approximation, we assume their geographical centers are their centers of mass. Because we know the radius of the Earth, we can use the Law of Universal Gravitation to calculate the mass of the Earth in terms of the What is the mass of the star? @ZeroTheHero: I believe the Earth-Sun distance is about 8 light-minutes, I guess it's the Earth-Moon distance that is about 1 light-second, but then, it seems, the mass of the planet is much smaller than that of the Earth. Start with the old equation the orbital period and the density of the two objectsD.) used frequently throughout astronomy, its not in SI unit. Knowledge awaits. Now, we calculate \(K\), \[ \begin{align*} K&=\frac{4\pi^2}{GM} \\[4pt] &=2.97 \times 10^{-19}\frac{s^2}{m^3} \end{align*}\], For any object orbiting the sun, \(T^2/R^3 = 2.97 \times 10^{-19} \), Also note, that if \(R\) is in AU (astonomical units, 1 AU=1.49x1011 m) and \(T\) is in earth-years, then, Now knowing this proportionality constant is related to the mass of the object being orbited, gives us the means to determine the mass this object by observing the orbiting objects. k m s m s. We can find the circular orbital velocities from Equation 13.7. The planet moves a distance s=vtsins=vtsin projected along the direction perpendicular to r. Since the area of a triangle is one-half the base (r) times the height (s)(s), for a small displacement, the area is given by A=12rsA=12rs. One of the real triumphs of Newtons law of universal gravitation, with the force proportional to the inverse of the distance squared, is that when it is combined with his second law, the solution for the path of any satellite is a conic section. I have a homework question asking me to calculate the mass of a planet given the semimajor axis and orbital period of its moon. % Is this consistent with our results for Halleys comet? I need to calculate the mass given only the moon's (of this specific system) orbital period and semimajor axis. Use a value of 6.67 times 10 to the Nothing to it. 1999-2023, Rice University. 1024 kg. Both the examples above illustrate the way that Kepler's Third Law can be used determine orbital information about planets, moons or satellites. endstream endobj startxref \( M = M_{sun} = 1.9891\times10^{30} \) kg. then you must include on every physical page the following attribution: If you are redistributing all or part of this book in a digital format, The best answers are voted up and rise to the top, Not the answer you're looking for? In fact, because almost no planet, satellite, or moon is actually on a perfectly circular orbit \(R\) is the semi-major axis of the elliptical path of the orbiting object. For planets without observable natural satellites, we must be more clever. I see none of that being necessary here, it seems to me that it should be solvable using Kepler's Laws although I may be wrong about that. This answer uses the Earth's mass as well as the period of the moon (Earth's moon). In practice, the finite acceleration is short enough that the difference is not a significant consideration.) Equation 13.8 gives us the period of a circular orbit of radius r about Earth: For an ellipse, recall that the semi-major axis is one-half the sum of the perihelion and the aphelion. orbit around a star. Kepler's Third law can be used to determine the orbital radius of the planet if the mass of the orbiting star is known (\(R^3 = T^2 - M_{star}/M_{sun} \), the radius is in AU and the period is in earth years). That is, for each planet orbiting another (much larger) object (the Sun), the square of the orbital period is proportional to the cube of the orbital radius. where \(K\) is a constant of proportionality. distant star with a period of 105 days and a radius of 0.480 AU. Although the mathematics is a bit An ellipse is defined as the set of all points such that the sum of the distance from each point to two foci is a constant. to write three conversion factors, each of which being equal to one. The mass of all planets in our solar system is given below. [closed], Improving the copy in the close modal and post notices - 2023 edition, New blog post from our CEO Prashanth: Community is the future of AI, Calculating specific orbital energy, semi-major axis, and orbital period of an orbiting body. How do I calculate the effect of a prograde, retrograde, radial and anti-radial burn on the orbital elements of a two-dimensional orbit? Since the angular momentum is constant, the areal velocity must also be constant. Physics . The formula equals four And those objects may be any, a moon orbiting the planet with a mass of, the distance between the moon and the planet is, To maintain the orbital path, the moon would also act, Where T is the orbital period of the moon around that planet. Where G is the gravitational constant, M is the mass of the planet and m is the mass of the moon. Now there are a lot of units here, 3 Answers Sorted by: 6 The correct formula is actually M = 4 2 a 3 G P 2 and is a form of Kepler's third law. Use a value of 6.67 10 m/kg s for the universal gravitational constant and 1.50 10 m for the length of 1 AU. are licensed under a, Coordinate Systems and Components of a Vector, Position, Displacement, and Average Velocity, Finding Velocity and Displacement from Acceleration, Relative Motion in One and Two Dimensions, Potential Energy and Conservation of Energy, Rotation with Constant Angular Acceleration, Relating Angular and Translational Quantities, Moment of Inertia and Rotational Kinetic Energy, Gravitational Potential Energy and Total Energy, Comparing Simple Harmonic Motion and Circular Motion, (a) An ellipse is a curve in which the sum of the distances from a point on the curve to two foci, As before, the distance between the planet and the Sun is. The most efficient method is a very quick acceleration along the circular orbital path, which is also along the path of the ellipse at that point. (Velocity and Acceleration of a Tennis Ball), Finding downward force on immersed object. For a circular orbit, the semi-major axis (a) is the same as the radius for the orbit. However, there is another way to calculate the eccentricity: e = 1 2 ( r a / r p) + 1. where r a is the radius of the apoapsis and r p the radius of the periaosis. Where does the version of Hamapil that is different from the Gemara come from? And now multiplying through 105 We can rearrange this equation to find the constant of proportionality constant for Kepler's Third law, \[ \frac{T^2}{r^3} =\frac{4\pi^2}{GM} \label{eq10} \]. Creative Commons Attribution License So lets convert it into radius, , which we know equals 0.480 AU. The constant e is called the eccentricity. By studying the exact orbit of the planets and sun in the solar system, you can calculate all of the masses of the planets. { "3.00:_Introduction" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.01:_Orbital_Mechanics" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.02:_Layered_Structure_of_a_Planet" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.3:_Two_Layer_Planet_Structure_Jupyter_Notebook" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.4:_Isostasy" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.5:_Isostasy_Jupyter_Notebook" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.5:_Observing_the_Gravity_Field" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.7:_Gravitational_Potential,_Mass_Anomalies_and_the_Geoid" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "3.8:_Summary" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()" }, { "00:_Front_Matter" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "01:_Rheology_of_Rocks" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "02:_Diffusion_and_Darcy\'s_Law" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "03:_Planetary_Geophysics" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "04:_Plate_Tectonics" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "05:_Seismology" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "06:_Earthquakes" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()", "zz:_Back_Matter" : "property get [Map MindTouch.Deki.Logic.ExtensionProcessorQueryProvider+<>c__DisplayClass228_0.b__1]()" }, [ "article:topic", "showtoc:no", "license:ccbysa", "authorname:mbillen", "Hohmann Transfer Orbit", "geosynchonous orbits" ], https://geo.libretexts.org/@app/auth/3/login?returnto=https%3A%2F%2Fgeo.libretexts.org%2FCourses%2FUniversity_of_California_Davis%2FGEL_056%253A_Introduction_to_Geophysics%2FGeophysics_is_everywhere_in_geology%2F03%253A_Planetary_Geophysics%2F3.01%253A_Orbital_Mechanics, \( \newcommand{\vecs}[1]{\overset { \scriptstyle \rightharpoonup} {\mathbf{#1}}}\) \( \newcommand{\vecd}[1]{\overset{-\!-\!\rightharpoonup}{\vphantom{a}\smash{#1}}} \)\(\newcommand{\id}{\mathrm{id}}\) \( \newcommand{\Span}{\mathrm{span}}\) \( \newcommand{\kernel}{\mathrm{null}\,}\) \( \newcommand{\range}{\mathrm{range}\,}\) \( \newcommand{\RealPart}{\mathrm{Re}}\) \( \newcommand{\ImaginaryPart}{\mathrm{Im}}\) \( \newcommand{\Argument}{\mathrm{Arg}}\) \( \newcommand{\norm}[1]{\| #1 \|}\) \( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\) \( \newcommand{\Span}{\mathrm{span}}\) \(\newcommand{\id}{\mathrm{id}}\) \( \newcommand{\Span}{\mathrm{span}}\) \( \newcommand{\kernel}{\mathrm{null}\,}\) \( \newcommand{\range}{\mathrm{range}\,}\) \( \newcommand{\RealPart}{\mathrm{Re}}\) \( \newcommand{\ImaginaryPart}{\mathrm{Im}}\) \( \newcommand{\Argument}{\mathrm{Arg}}\) \( \newcommand{\norm}[1]{\| #1 \|}\) \( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\) \( \newcommand{\Span}{\mathrm{span}}\)\(\newcommand{\AA}{\unicode[.8,0]{x212B}}\), Orbital Period or Radius of a Satellite or other Object, The Fastest Path from one Planet to Another.

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find mass of planet given radius and period