23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6573166130612218---------------------------
|
|
|
|
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: 2023-04-24T21:08:17.152
|
|
Launch V∞: [5.803834252870955, -8.829232626648086, -2.337290536601728] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.08821797177140085, -0.5309806792298443, 0.5364222325119744] km/s
|
|
V∞_out: [-0.47872416044970634, -0.4930284162959207, -0.3252635919652413] km/s
|
|
time of flight: 9.79916839393585e7 seconds
|
|
arrival date: 2026-06-02T01:03:00.152
|
|
thrust profile: [0.7550758441007756 -0.5949095689977306 -0.4306108974774697; 0.3519965660260834 -0.09167012976194024 -0.33379710091426246; 0.10927387550453209 -0.005901484722778477 -0.14968751820503376; 0.07177197814734927 0.004076041106891502 -0.1219472920851041; 0.037022574204826034 0.004880140699838259 -0.07289240890975873; 0.02487378356444231 0.004889814110227541 -0.05330018522707181; 0.01405854804857325 0.0030479424437029304 -0.03396339330400207; 0.00870720639031945 0.0020190502560569487 -0.022670000706623117; 0.0005096620485692552 -0.002019185894479747 0.00010604807096278629; 0.0010557674886518965 0.00046236660796876954 -0.0024258963311709946; -0.0045457785913624645 -0.004604936185267668 -0.004062212532447527; 0.0031325765041829547 -0.0033734306948059647 -0.005784031382471379; 0.0009222166137017423 0.006761816606510674 -0.005302133837198244; 0.002462443933988821 0.008050606021035349 -0.0018567449591174502; -0.0002524112095682855 0.0011460604082883135 -0.0022988769990916324; -0.00022566959277748867 0.0028874684974127293 -0.00749540815713692; 0.004628188953019228 -0.0012431016638244103 -0.008844218536413824; -0.0031356773384072084 -0.003444702016088038 0.004585562383834474; -0.005320480177208811 -0.003170330014802855 0.000845784104122339; 6.581288524274602e-5 0.00013210098613225746 -0.0001144086381091465] %
|
|
|
|
Mass Used: 83.76990270536498 kg
|
|
Launch C3: 117.10276786275321 km²/s²
|
|
||V∞_in||: 0.7599155899124437 km/s
|