23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6040208065083343---------------------------
|
|
|
|
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: 2024-04-27T07:24:33.864
|
|
Launch V∞: [6.703288370549707, -5.970617605544571, -0.23748971011122802] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.4798535099098836e-9, -1.0326489184801556e-9, -1.7764152085438303e-9] km/s
|
|
V∞_out: [4.650365457937631e-10, 9.730075229873963e-10, 2.3883981999578016e-11] km/s
|
|
time of flight: 1.8300007870126346e8 seconds
|
|
arrival date: 2030-02-13T08:45:51.864
|
|
thrust profile: [1.0 -0.07301585804258892 -0.1237770015414152; 0.7833754746348144 0.4879445849891755 -0.3031070721848283; 0.44152773467870926 0.4936362415172658 -0.31328399124279827; 0.16303610530006965 0.2627481053363735 -0.1853472278989174; 0.0366366496208964 0.07230053068229489 -0.051197006322581465; 0.004207588588797904 0.012362420992971154 -0.010736936454929836; 0.002653335881393658 0.009577160006273209 -0.008678458842714848; 0.0005365132027809979 0.0029451672353898906 -0.002954814588082504; 0.00016975666856170499 0.0010119806994246432 -0.0009690293070953282; 0.00019861924424318918 0.0009134572808424962 -0.0010298475397176386; 4.0676257195770935e-5 0.0008380085353454198 -0.001055517552855304; 0.00016422150049238157 0.0005940827428346881 -0.000478511895983275; 2.188115950585868e-5 0.0004547900285850854 -0.0005294372767527854; -0.00012435220841089612 0.0004130711489118855 -5.091536087009613e-5; -1.3785463372680723e-5 0.0005668710515434858 -0.0006969063772872974; 0.00042190563493814805 0.0006368181306577059 -0.0005397840111106373; 2.266809112684005e-5 0.0007853012047203283 -0.0007558872241779837; -8.305818302526276e-6 -2.0346978512382203e-5 0.00011400178788656011; 0.0007592395754721524 0.0002605500178852354 0.00032490700809416177; 0.0002090651713523722 0.00024729137043951886 -0.00012815012925504655] %
|
|
|
|
Mass Used: 234.29822715175578 kg
|
|
Launch C3: 80.63875093279445 km²/s²
|
|
||V∞_in||: 2.5321890120559045e-9 km/s
|