23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5658972426706004---------------------------
|
|
|
|
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: 2024-05-16T18:42:02.359
|
|
Launch V∞: [7.8553232824295876, -5.9665855512095245, 0.2238087773225407] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7152808335520007e-9, 3.7301906167482073e-10, -2.4667343973613663e-10] km/s
|
|
V∞_out: [1.1147050397267336e-9, -1.025777955974556e-9, -8.425686417853359e-10] km/s
|
|
time of flight: 1.8561137860938823e8 seconds
|
|
arrival date: 2030-04-04T01:25:00.359
|
|
thrust profile: [0.33258280580026234 -0.017007790786879414 -0.09812589555510388; 0.027261841761143435 0.01366198938698264 -0.030036125735742658; 0.07518712043313905 0.05671089079421305 -0.1440447813647325; 0.024490740887069998 0.027632209687936914 -0.08339478444696485; 0.017136214230039394 0.024623741612814446 -0.08187829361278445; 0.025642196955417314 0.04222030177262362 -0.15767691833943254; 0.006028095678450212 0.012939619778639194 -0.055146364423123685; 0.004811197522729205 0.012776833176922311 -0.04814776864805692; 0.0034800472165802216 0.009470369590946902 -0.045621636893927286; 0.0031309653005505244 0.006239317905712729 -0.027276704127085265; 0.005417263026024088 0.007979457067343118 -0.03871340420967351; 0.0013632600953432416 -0.00014709872846343478 -0.005458994053172038; -0.0030098908583941495 0.006441056105357738 -0.000321372412327194; 0.004706677060195712 -0.002127615141053095 0.006627239018211522; -0.01155399199955304 -0.010622216715312244 0.0014588245808482073; -0.0002702380774045171 -0.019674957027238645 0.0005530576550341663; -0.0010310352159706867 -0.0013986856839811894 0.0061480178401343765; 0.0020934806075177627 0.015954486073465002 -0.008692172246922742; -0.015591653349191673 0.004963672404545424 -0.008309711043314487; 0.002313689037206252 0.011390706689422068 -0.018365665499068096] %
|
|
|
|
Mass Used: 92.30148173126327 kg
|
|
Launch C3: 97.35633738018923 km²/s²
|
|
||V∞_in||: 1.772619345543444e-9 km/s
|