23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6537838056942934---------------------------
|
|
|
|
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: 2023-04-24T11:23:43.744
|
|
Launch V∞: [5.606768555252042, -8.774492701550917, -2.353825136196704] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0001268191581654383, -6.491055548485698e-5, -0.00011371233945810922] km/s
|
|
V∞_out: [5.3497936777423725e-5, -0.00012091016473659612, 0.00012548533729324254] km/s
|
|
time of flight: 1.0243796626085654e8 seconds
|
|
arrival date: 2026-07-23T02:23:09.744
|
|
thrust profile: [0.6599616711153407 -0.5222053395624224 -0.40251877178781975; 0.32403580311379077 -0.08138254073987129 -0.3277444865573433; 0.1499139515908569 -0.007536380968806237 -0.22014775522529226; 0.0612781631292876 0.0012015597792688491 -0.12019275626559674; 0.030080111916457278 -0.0008801466235205998 -0.07251255869794224; 0.018380964263648214 -0.0016899785730604307 -0.05055764751527463; 0.0232088036044783 0.0001642797075402467 -0.05828366250140799; 0.010713787071779116 0.012718826386411081 -0.02423153748459978; 0.00424344498947778 0.0033667512464852414 -0.024319705716766213; 0.01337847412141847 0.001335718730188624 -0.00026464998402602304; 0.005634463076130564 2.804122954395711e-5 -0.013166804841128695; 0.015474606912089434 0.005209611687094462 -0.02793215840291663; 0.024430047454754775 -0.0027249161141387423 0.016895802492884054; 0.00367884890799987 -0.008695245438411894 0.004417699912961176; 0.020212575823320478 0.005381717358728782 0.03929595721829983; -0.02744628015811903 -0.03458452190947478 0.015288819379394622; 0.010321530858425774 0.05720612662958559 0.030423511519756155; -0.008267923280875894 -0.008309164753599845 -0.001783345585193657; -0.039915675266704406 -0.010377538701279321 0.022254341695803162; -0.012682079492003655 0.006320149703781333 0.030200036976940806] %
|
|
|
|
Mass Used: 97.93403996444749 kg
|
|
Launch C3: 113.96806857352482 km²/s²
|
|
||V∞_in||: 0.00018228267947388588 km/s
|