23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5634558495560347---------------------------
|
|
|
|
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: 2023-05-01T01:46:05.374
|
|
Launch V∞: [6.537949329927846, -7.415858177028391, 0.11196031360446669] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [1.263086722908291e-8, -6.044124315992695e-9, 1.875181904434901e-8] km/s
|
|
V∞_out: [5.820232884488108e-9, -1.309186454200684e-8, -1.780894567616227e-8] km/s
|
|
time of flight: 1.860842587886374e8 seconds
|
|
arrival date: 2029-03-23T19:50:23.374
|
|
thrust profile: [0.23424689463362697 -0.054777354976170124 -0.07918590132565981; 0.05160684113726102 0.01526062124760183 -0.055017062826611875; 0.04789914013502554 0.027413381202065025 -0.08410509805345796; 0.04488155835960134 0.036887946797392324 -0.11079639001145755; 0.042636568337112775 0.042348772987631345 -0.13719474121546812; 0.02686409563806282 0.028773175640022564 -0.10078264784348633; 0.019009270720087908 0.022181022626746785 -0.08619652212247397; 0.018322494197053 0.02170861376971749 -0.08923325938710591; 0.009640848169135557 0.013673677776744613 -0.05617063553608763; 0.0074249098457972226 0.011408633988669818 -0.04890968925585291; 0.006175313936728629 0.01046410769050491 -0.044892154106138955; -0.00019247874735156388 0.0003006619389588542 -0.0016088086479142348; 0.0002088529380211267 5.3837265793139715e-5 -0.0021323034657523394; 0.0015730466087762913 0.000709179641058809 -0.00027601603825743424; -0.002247064226712723 -0.001365615753840703 -0.0009099722858373878; -8.27781111024104e-6 -0.0005955372593854599 0.00035873528617422245; -5.868681933898846e-5 -0.0007520217769064106 -0.0018541900514294674; -0.003281525516525979 -0.0009876567469752212 -0.004242880167229079; 0.00025013876808349894 -0.002740505881069171 -0.0035867950527683334; -0.00014861448859564564 -0.00036958274976718283 0.0004976785564129961] %
|
|
|
|
Mass Used: 87.14358833180995 kg
|
|
Launch C3: 97.75226905432524 km²/s²
|
|
||V∞_in||: 2.34030118398873e-8 km/s
|