23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5562197375115379---------------------------
|
|
|
|
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: 2024-05-14T08:28:50.579
|
|
Launch V∞: [7.956671817294117, -5.6609425768938895, 0.11973664872421869] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.019878572294108564, 0.10427627679277217, 0.12006622688413132] km/s
|
|
V∞_out: [-0.02676632273548786, 0.02189633982126089, -0.1558156646357244] km/s
|
|
time of flight: 1.8749577787445086e8 seconds
|
|
arrival date: 2030-04-23T10:38:27.579
|
|
thrust profile: [0.4648787306776494 -0.0031563383720204694 -0.14915979745654925; 0.04630326927273945 0.02632964781177669 -0.056191469301530655; 0.029571421099710983 0.026564785473289658 -0.06526801184618221; 0.04177086330508981 0.050043352174588586 -0.13280570786583762; 0.022143421392631556 0.03242493024593908 -0.09813955069981342; 0.022863486293339588 0.038555045199634604 -0.1246412950611614; 0.007114131506312907 0.013926363434566557 -0.05247987051428653; 0.007714379756863674 0.018170153570327342 -0.07143606394022103; 0.0026707829113815657 0.008874632353841654 -0.035179848297938264; 0.0008901896187547407 0.005536157616539366 -0.023511368521118164; 3.12433084353212e-5 0.0007284117239459563 -0.005003592753462291; 0.0012524034857838747 0.0010040435889489489 -0.006807836453621714; 0.00018123887032720453 -0.0008460842030461877 6.41196324002581e-5; -2.1448239926234996e-5 -0.00015769869089187302 0.0004623395606891327; 0.00021693698034784946 0.0007395556466645929 -0.002229446767603577; -6.644170939234048e-5 7.879387051352798e-6 0.00022166914151218963; -0.0007977345736629328 -0.0010504694316545993 0.0038839663933359315; -2.9427167962621298e-5 -0.0002383630291785339 -0.0002911089991752324; -0.0003506301789865338 0.0015186669215371544 -0.00020858886800227423; -0.0004353193789490946 -0.00033088004581315647 0.00041390605859531346] %
|
|
|
|
Mass Used: 92.60249465977631 kg
|
|
Launch C3: 95.3692341320602 km²/s²
|
|
||V∞_in||: 0.16026415187560392 km/s
|