23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5558779781677604---------------------------
|
|
|
|
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: 2024-05-15T08:10:09.677
|
|
Launch V∞: [7.894381291534464, -5.785139007377959, -0.08494684631296423] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.9034379560346155e-9, 2.302025376630676e-9, 9.233393374906011e-10] km/s
|
|
V∞_out: [2.508998396217692e-9, -2.308370756981814e-9, -1.8870685581830936e-9] km/s
|
|
time of flight: 1.8749577787470794e8 seconds
|
|
arrival date: 2030-04-24T10:19:46.677
|
|
thrust profile: [0.3795819420374527 -0.003768633453468938 -0.1239326663584129; 0.09794470904025773 0.05578611794694805 -0.11743536837114588; 0.06504884963741392 0.05744204155321652 -0.1393410922487926; 0.027549147915339748 0.03144574045624916 -0.09023581588392661; 0.02843485432910916 0.03967245820343552 -0.12453309035323756; 0.01434010947560126 0.02322679269369038 -0.08178498720083793; 0.01057921776971638 0.019018700672330743 -0.07394958555043603; 0.004791032285740364 0.00972817550556817 -0.041161520238384854; 0.001423368274942205 0.004597516902262278 -0.018419472303710577; 0.0010348087333635588 0.0026947177146075772 -0.011409050605615628; 5.150679715794969e-5 0.00016032361211856425 -0.0006044108486849174; 0.00020403454557339372 0.0005272748954227537 -0.0026084863602975046; 3.084653317123268e-5 -5.281500999293916e-5 -0.00019017181288307898; -0.00011666855441256528 -7.987156532713148e-5 -0.0003686507106282742; 0.00023745646356933872 0.00018793775512487935 -0.00023735984487069752; 1.2671917395674077e-5 -7.244969914968518e-6 -0.00018704249470194272; -9.849995183951334e-5 -3.900843859143215e-5 1.7210650528979242e-5; 9.357834425714433e-5 0.00023348563805860174 8.355049469364135e-5; -0.00023633066851157567 9.058746275186138e-5 0.00020906591152564878; 0.00014150045409054975 0.00026982721645029464 -0.00012436396049234023] %
|
|
|
|
Mass Used: 89.71252707688927 kg
|
|
Launch C3: 95.79630527751392 km²/s²
|
|
||V∞_in||: 3.1264920309001944e-9 km/s
|