{"text_format":"3","workbook":"xlsx","n_sheets":1,"sheets":["Sheet1"],"read":"whole","date_system":"1900"}

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["Stratocatcher",null,"for Apollo Entry"]
[]
[null,11000," m Stratolaunch altitude"]
[null,240," m/s Stratolaunch velocity"]
[null,340," tonne Stratolaunch gross weight"]
[null,590," tonne Stratolaunch takeoff weight"]
[null,1.5," MN Stratolaunch thrust"]
[]
[null,3000," m est runway with full load"]
[null,{"$f":"B6*0.001/B7","v":{"v":0.393333333333333,"d":"0.393"}}," m/s2 estimated takeoff acceleration"]
[null,{"$f":"SQRT(2*B9*B10)","v":{"v":48.5798312059645,"d":"48.580"}}," m/s estimated takeoff velocity"]
[null,{"$f":"9.8*B6/B5","v":{"v":17.0058823529412,"d":"17.01"}}," m/s2 estimated unloaded lift at ground"]
[]
[]
[null,150,"m/s Apollo velocity at 7.3 km"]
[{"v":0.00082342989958662,"d":"8.23430E-4"},null,"estimated Apollo drag scaling"]
[null,{"$f":"(0.3*D33+0.7*D34)-B15","v":0},"m/s drag estimation error"]
[]
["altitude",null,null,"velocity",null,"min speed","max drop","max lift"]
["m","kg/m3",null,"m/s",null,"est m/s","radius m","radius m"]
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