23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5620105386071821---------------------------
|
|
|
|
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: 2024-05-15T07:47:36.678
|
|
Launch V∞: [7.575483287810218, -6.151859133019012, 0.258666983658136] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.00035845139602393416, 0.0010756767004340237, 0.0026907153818415378] km/s
|
|
V∞_out: [0.0026638622997824267, 0.0003377384587200819, -0.0011464627700154368] km/s
|
|
time of flight: 1.7945339013027665e8 seconds
|
|
arrival date: 2030-01-21T07:57:26.678
|
|
thrust profile: [0.5305609807710493 -0.04087770692809411 -0.19104057342657405; 0.028857558517522145 0.011418901989977727 -0.03768022304499414; 0.042416266075921354 0.026780041044786224 -0.0947552716953513; 0.06058640925200788 0.04769781733031485 -0.18415729848263815; 0.03422431998650675 0.030118581156556436 -0.13656590002408497; 0.019519026977471016 0.019957538726874297 -0.1015544864860905; 0.013533870630009428 0.01425647351420702 -0.07972268774463265; 0.005460027711824864 0.005418667707435451 -0.03486426980747737; 0.002463703202618409 0.003576061940922237 -0.018467372823634944; 0.003479219517894181 0.003002728035713122 -0.022338420997595358; 0.000344981628034965 -0.0003464297747168214 -0.001702080926922619; 0.002339818597775407 0.004368098827026585 -0.02693211101370859; 0.0004652483650505764 0.0002653911139332614 -0.0023300968152587995; 0.0033072973529778673 -0.0014332356328037327 -0.0003863620240149982; -0.0007496388215667639 0.0017644696024869692 -0.0020034264196425343; -0.0012181789889744133 -0.0023754127505072314 0.0007737224292833859; -0.004965679336955995 -0.0022898391349519265 0.0020487321909431226; -0.004595197396927841 0.0028037259780320086 -0.0024536308390156096; -0.0004229976064235319 0.0004346718205288753 -0.0023603938679771863; 0.0009680268288885009 -0.0009703815899566541 0.0111528831084079] %
|
|
|
|
Mass Used: 99.76097411350156 kg
|
|
Launch C3: 95.30022644483614 km²/s²
|
|
||V∞_in||: 0.002919848803148339 km/s
|