23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6141767968241654---------------------------
|
|
|
|
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: 2024-05-02T04:08:59.394
|
|
Launch V∞: [7.136634655337771, -7.045254471736178, -1.2032440557650375] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0020022139904941113, -0.012503611708135545, -0.002397613155078456] km/s
|
|
V∞_out: [-0.01229637520688261, 0.0023926242143178147, -0.0030559097460044174] km/s
|
|
time of flight: 1.1753938948470293e8 seconds
|
|
arrival date: 2028-01-22T13:58:48.394
|
|
thrust profile: [0.5478184382093398 -0.22744810237541457 -0.23421409831882511; 0.3363420179780516 0.027230365800426277 -0.3067960481180026; 0.22703615705484553 0.07177306054143508 -0.3182133583366914; 0.1564235699658163 0.07392566900119239 -0.29286866980921394; 0.11306249675528642 0.06684788164013306 -0.26021189474936574; 0.07134240536469122 0.05032083797261292 -0.19399658641484258; 0.035081013101943725 0.025462932977608172 -0.10763496462944314; 0.025198899285182562 0.01713547638357689 -0.082474567701942; 0.0015809502587933095 0.00165517081847312 -0.011832789408146267; 0.0016011325474623841 0.0009857763587852234 -0.007027884215675552; 0.0015092053393990484 -0.000590717763962132 -0.0020274967033076345; 0.0021815941517990094 -0.0006053341514209982 0.0014807090586726984; 0.0034186345369047926 0.0038378838027332924 -0.005236948176609619; 0.0017610342919540576 0.002698557898251626 -0.0032599523290054704; 0.0015837972641681221 0.00291445135869165 -0.0016438871079851472; 0.000411209617812833 -0.0024269415168879185 -0.003440327160824169; -0.0011835966711058704 -0.0004309926102214355 -0.0001742449020427422; -8.421165898949996e-5 0.0035632182393575784 -0.004062873017900307; 0.002884242898333675 -0.0009327597377030537 -0.0023552221858836376; 0.00041000990493121267 -7.15331007044575e-6 -1.3973560542390062e-5] %
|
|
|
|
Mass Used: 121.45232360223963 kg
|
|
Launch C3: 102.01496103302057 km²/s²
|
|
||V∞_in||: 0.012887890263846907 km/s
|