Universal gravitational constantG=6.673(10-11) m3/(kg-s2)=3.439(10-8) ft4/(lb-sec4)Mass of Earthme=5.976(1024) kg-4.095(1023) lb-sec2/ftPeriod of Earth's rotation (1 sidereal day)=23 h 56 min 4 s=23.9344 hAngular velocity ofEarthw=0.7292(10-4) rad/sMean angular velocity of Earth-Sun linew'=0.1991(10-6) rad/sMean velocity of Earth's center about Sun-107 200 km/h-66,610 mi/hrBody Mean Distance to Sun km (mi) Eccentricity of Orbit e Period of Orbit solar days Mean Diameter km (mi) Mass Relative to Earth Surface Gravitational Acceleration m/s² (ft/sec²) Escape Velocity km/s (mi/sec)Sun1 392 000333 000274616(865 000)(898)(383)Moon0.05527.323 4760.0123(2 160)384 398¹(238 854)¹57.3 × 106(35.6 x 106)Mercury0.20687.975 0000.054(3 100)Venus108 x 1060.0068224.7012 4000.815(7 700)(67.2 x 106)149.6 x 106Earth0.0167365.2612 742²1.000(7 918)²Mars(92.96 × 106)227.9 x 106(141.6 × 106)0.093686.980.1076 788(4218)Jupiter4778 x 1060.04894333317.8(483 × 106)1 yr139 822(86 884)1.62(5-32)3.47(11.4)8.44(27.7)9.8213(32.22)33.73(12.3)24.79(81.3)2.37(1.47)4.17(2.59)10.24(6.36)11.18(6.95)5.03(3.13)59.5(36.8) Determine the distance h for which the spacecraft S will experience equal attractions from the earth and from the sun. Use Table D/2of Appendix D as needed.Assume L = 210 000 km.SunEarthAnswer: h= iNot to scale(105) km

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Determine the distance h for which the spacecraft S will experience equal attractions from the earth and from the sun. Use Table D/2 of Appendix D as needed. Assume L-210 000 km. SX- Sun Answer: h-i Not to scale Earth L (105) km