Files
thesis/archive/ES_0.5564048549413042
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5564048549413042---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-16T02:16:42.076
Launch V∞: [8.106019039293454, -5.749402944357282, -0.01764408852833544] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.019390677124978384, 0.12867779726983442, 0.15438281814718638] km/s
V∞_out: [-0.08442131866292248, 0.06795777202425991, -0.1706277029235823] km/s
time of flight: 1.874957778770099e8 seconds
arrival date: 2030-04-25T04:26:19.076
thrust profile: [0.17696723280162294 -0.0020790192009619373 -0.06544341379978084; 0.04374158706263178 0.022792073987474785 -0.055871474583363265; 0.06289621876219645 0.05328115953628962 -0.14281840185029146; 0.028530354362034265 0.030826009216158152 -0.09527463491435076; 0.01742566069169801 0.022498906394578966 -0.07952436718936659; 0.01781485687928065 0.025869238050137612 -0.09839980452363024; 0.011937582102736273 0.020787422759922857 -0.0842008966417584; 0.0055828563939743035 0.00998359946871324 -0.04528112248971227; 0.005010136992623528 0.009104124168313214 -0.04315612151891958; 0.005804964041417466 0.011787457221582818 -0.061167836610635254; 0.0008206272273259728 0.0016946640207294538 -0.009203598203342737; 2.686020818959074e-5 0.00036729666935340455 -0.0011054273222438529; 0.00017336167881622472 -1.49020818459693e-5 -0.0009694558059525206; 0.00017115674418187693 -0.00025541094195160235 -3.511926122925802e-5; -0.00017899820990559782 -0.00014893296391419207 -0.00031327317420853376; 0.0002537663947340923 -0.0002571052219102797 -0.0007959044251347252; -0.0004378232495403716 0.0005894881730827729 -0.000296695365557894; 0.0004603162509315707 -0.0004462301139326054 -0.000421630776842283; 0.0005010874023713811 0.00025509493559874223 0.0015716556386789887; -1.6135092068641902e-5 -0.00022509537381867287 -0.0004259952321964195] %
Mass Used: 73.01863795583404 kg
Launch C3: 98.76349019583215 km²/s²
||V∞_in||: 0.20191094177544958 km/s