1. Newton's law of gravitation: (i) Gravitational force acting between to bodies, F∝m1m2r2 or F=Gm1m2r2 where G=6.67×1011N m2kg2 is the universal gravitational constant. (ii) In vector form: F→12=Gm1m2r2r^12 & F→21=Gm1m2r2r^21 2. Gravitational field: (i) Gravitational field is related to the force as, E→=F→m (ii) The field produced by a point mass is given by, E→=GMr2r^ 3. Variation of Acceleration due to Gravity: (i) Acceleration due to gravity at height h from the surface gh=GMeRe+h2≃g1-2hRe (ii) Acceleration due to gravity at depth d from the surface, gd=g1-dRe (iii) The equational radius is about 21 km longer than its polar radius. Hence gpole>gequator (iv) Acceleration due to gravity at latitude θ, g'=g-Rω2 cos2θ 4. Escape velocity: It is the speed required from the surface of a planet to get out of the influence of the planet. For earth, ve=2GMeRe=2gRe 5. Satellite in a circular orbit: (i) Satellite orbital Velocity, v0=GMeRe+h12 (ii) Time period of satellite, T=2πRe+h32GMe (iii) Potential energy of a Satellite: P.E.=-GMem(Re+h), Kinetic energy: K.E.=GMem2(Re+h) and total energy E=-GMem2(Re+h) 6. Kepler’s Laws: (i) All planets move in elliptical orbits with the Sun at one of the focal points (ii) The line joining the sun and a planet sweeps out equal areas in equal intervals of time. (iii) The square of the orbital period of a planet is proportional to the cube of the semi-major axis of the elliptical orbit of the planet. The time period T and radius R of the circular orbit of a planet about the sun are related as T2=4π2GMsR3 Given: gd = 90% of g i.e., `"g"_"d"/"g"` = 0.9, To find: Distance below the Earth’s surface (d) Formula: gd = `"g"(1 - "d"/"R")` Calculation: From formula, `"g"_"d"/"g" = (1 - "d"/"R")` ∴ `"d"/"R" = 1 - "g"_"d"/"g"` ∴ d = R`(1 - "g"_"d"/"g")` = 6.4 × 106 × 0.1 = 640 × 103 m = 640 km At distance 640 km below the surface of the Earth, value of acceleration due to gravity decreases by 10%. |