23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.560112027904094---------------------------
|
|
|
|
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: 2024-05-15T13:42:26.294
|
|
Launch V∞: [7.97128445884716, -6.039189852305846, -0.011076760865192142] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.0005018020724001508, 0.00139067970483264, 0.003171195995761545] km/s
|
|
V∞_out: [0.00320224452339908, 0.0003835118422356357, -0.0013452814108584465] km/s
|
|
time of flight: 1.8050344377548072e8 seconds
|
|
arrival date: 2030-02-02T17:33:09.294
|
|
thrust profile: [0.09345238076678467 -0.006233315176459761 -0.03717149894926537; 0.03698003211676286 0.016071643316568296 -0.04784717773732191; 0.0275016927928309 0.019248400271576836 -0.06274703044118016; 0.043743880077415725 0.03907807879633793 -0.13957895180076885; 0.03240544634683999 0.033826930232982506 -0.13549574385377708; 0.012192898206894428 0.014166713477045489 -0.06418731907703487; 0.012883539338095381 0.016968617613634825 -0.08455971092663146; 0.00842685470284598 0.012934195702177503 -0.07250701772835554; 0.0063691807744748665 0.009133667324857975 -0.0519618316881585; 0.011740028887172568 0.019583701616838138 -0.12506805232780957; 0.0019698270607186176 0.0029911376698540416 -0.019437415358726312; 0.0005063064013769137 0.0011678798476265223 -0.0008607694858120752; 0.0001820565462460775 -9.586275354528135e-5 0.00035906741847539683; -0.0001948771102976477 -6.453795290699266e-5 0.00010963215031004015; -0.0008447638460168324 -0.00041425337648411055 -0.0004907568475172162; -0.0003985201981213632 0.0018870522788175287 -0.0023246425177014356; -9.271223119133713e-5 -0.002720397310256125 0.0012952819077787555; 8.70958838849762e-6 -0.00020119594321347037 -0.0013362950841379684; -0.002439844244307262 -0.0023861325010015046 0.0005234402114534301; 0.0029763824916962753 -0.0007591777854959055 0.00010168249422386482] %
|
|
|
|
Mass Used: 70.05304185912291 kg
|
|
Launch C3: 100.01331269068342 km²/s²
|
|
||V∞_in||: 0.0034988968839953748 km/s
|