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{"sheet":"Sheet1","index":0,"n_rows":38,"n_cols":3,"rows_kept":38}
["Translunar injection from a construction orbit"]
["translunar.ods","KHL","2018/09/08"]
[]
[398600.4418,"km3/s2","Grav parameter"]
[6430,"km","Entry"]
[8378,"km","Perigee"]
[75950,"km","Apogee"]
[385000,"km","Moon"]
[]
["Construction Orbit"]
[{"$f":"A5","v":6430},"km","Entry"]
[{"$f":"A6","v":8378},"km","Perigee"]
[{"$f":"A7","v":75950},"km","Apogee"]
[{"$f":"(A12+A13)/2","v":42164},"km","semimajor"]
[{"$f":"2*PI()*SQRT(A14^3/$A$4)","v":{"v":86163.5705505783,"d":"86164"}},"sec","period"]
[{"$f":"1000*SQRT(($A$4/A14)*(A13/A12))","v":{"v":9257.45685399497,"d":"9257"}},"m/s","perigee velocity"]
[{"$f":"1000*SQRT(($A$4/A14)*(A12/A13))","v":{"v":1021.18464151112,"d":"1021"}},"m/s","apogee velocity"]
[{"$f":"1000*SQRT(2*$A$4*A11/(A13*(A13+A11)))","v":{"v":905.137564789647,"d":"905"}},"m/s","Entry apogee velocity"]
[{"$f":"1000*SQRT(2*$A$4*A13/(A11*(A13+A11)))","v":{"v":10691.3216245371,"d":"10691"}},"m/s","Entry perigee velocity"]
[{"$f":"A17-A18","v":{"v":116.047076721477,"d":"116"}},"m/s","Entry burn delta V"]
[{"$f":"(1.5/3600)*A15","v":{"v":35.9014877294076,"d":"36"}},"hours","worst case return time"]
[]
["Lunar Transfer Orbit"]
[{"$f":"A5","v":6430},"km","Entry"]
[{"$f":"A6","v":8378},"km","perigee"]
[{"$f":"A8","v":385000},"km","apogee"]
[{"$f":"(A25+A26)/2","v":196689},"km","semimajor"]
[{"$f":"2*PI()*SQRT(A27^3/$A$4)","v":{"v":868122.653011183,"d":"868123"}},"sec","period"]
[{"$f":"1000*SQRT(($A$4/A27)*(A26/A25))","v":{"v":9650.26053475852,"d":"9650"}},"m/s","perigee velocity"]
[{"$f":"1000*SQRT(($A$4/A27)*(A25/A26))","v":{"v":209.999695481057,"d":"210"}},"m/s","apogee velocity"]
[{"$f":"1000*SQRT(2*$A$4*A24/(A26*(A26+A24)))","v":{"v":184.430164446969,"d":"184"}},"m/s","Entry apogee velocity"]
[{"$f":"1000*SQRT(2*$A$4*A26/(A24*(A26+A24)))","v":{"v":11042.8636566225,"d":"11043"}},"m/s","Entry perigee velocity"]
[{"$f":"A30-A31","v":{"v":25.5695310340881,"d":"26"}},"m/s","Entry burn delta V"]
[{"$f":"(1.5/3600)*A28","v":{"v":361.717772087993,"d":"362"}},"hours","worst case return time"]
[]
[{"$f":"A29-A16","v":{"v":392.803680763553,"d":"393"}},"m/s","perigee injection velocity from construction orbit"]
[{"$f":"A32-A19","v":{"v":351.542032085428,"d":"352"}},"m/s","direct launch velocity difference"]
[{"$f":"A36-A37","v":{"v":41.2616486781244,"d":"41"}},"m/s","extra cost of construction orbit "]