30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-12T02:20:38.349/mission---------------------------
|
|
|
|
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: 2024-06-27T01:02:22.769
|
|
Launch V∞: [6.7386630924747735, 2.681719926533396, -0.33192262753473517] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [7.715602805644678, 2.5340401706785007, 0.59216879433437] km/s
|
|
V∞_out: [8.14158010025008, 0.11467559822796293, -0.05931443388440504] km/s
|
|
time of flight: 9.561374944761689e7 seconds
|
|
arrival date: 2027-07-08T16:24:51.769
|
|
thrust profile: [0.023301022793894528 0.014506194191639996 -0.0023755438375060796; -0.0033183751580871247 0.07336782130026553 -0.010811507865922472; -0.06164727407552523 0.1056496969546475 -0.015161235314008188; -0.11620137406382157 0.10874515644970927 -0.01361354605050158; -0.1601570651283726 0.09921746096307649 -0.012671822225267419; -0.19082531605807282 0.0802558926347972 -0.009996142143905916; -0.20208459146376992 0.05645991756914749 -0.006506293164629694; -0.21544032645611308 0.03523333870753496 -0.003351285055413982; -0.2146729665158058 0.015989911852492572 -0.0006952731036961628; -0.2100243756555401 -0.002329651168066605 0.0017750081369577472; -0.20068199973477896 -0.01650191290529539 0.0032462994310995894; -0.18569841958374314 -0.029823004573719693 0.005192162167569715; -0.17068555643039118 -0.04088645007952001 0.006882136983000742; -0.1544233058448683 -0.05266519452045455 0.008779360398481333; -0.13772295301894258 -0.0660836116852668 0.010909532136160287; -0.1245197103734167 -0.08412870453765404 0.011561357511009963; -0.11864715197412816 -0.10345797348459172 0.012266842139150844; -0.12286715595935756 -0.11968342646377855 0.013379062014771508; -0.1280643838181201 -0.12655169696513147 0.014368799422308797; -0.0584121142412127 -0.09509621902471597 0.021690900981356457] %
|
|
Phase 2:
|
|
Planet: Saturn
|
|
V∞_in: [3.8395108661970547, 1.7159262299086049, -0.5755224531865024] km/s
|
|
V∞_out: [1.585491120038796, 1.6910585908232016, -1.5486076554083772] km/s
|
|
time of flight: 1.9541956884803814e8 seconds
|
|
arrival date: 2033-09-16T11:37:39.769
|
|
thrust profile: [0.6823696785602157 -0.17465970925833899 0.0043786960922660234; 0.6324817977952034 0.37687729714593043 -0.01591902686901882; 0.3277378095890081 0.4273045997113089 -0.028355410420497114; 0.10029194711800075 0.3999364225521307 -0.03982802930015918; -0.020337081717252826 0.3496704764595339 -0.0471085437841163; -0.06953931842857293 0.30506864176347775 -0.050869154269620596; -0.09029458688961563 0.2659041906755343 -0.05171965882195978; -0.09569930804632429 0.23393858191140274 -0.05045687048832852; -0.09135019739026035 0.20289486172260954 -0.0471432021452754; -0.08319328510285766 0.1751518535444896 -0.042866586306264595; -0.07234783813584449 0.14706283938140732 -0.03706890299670858; -0.06147684285523951 0.11875925720287137 -0.030811114879888888; -0.049301448626872475 0.0927610035215594 -0.025105771012088114; -0.040797799440948385 0.07229409923332282 -0.02206113454900311; -0.029504166236854465 0.034043477456934826 -0.01610127680367871; -0.026224768748220457 0.020043015937368583 -0.011941084397735483; -0.02324819576509405 -0.0026427941112453753 -0.03949368883582122; -0.02103554091162609 -0.0003860869927297471 -0.016902655236921048; -0.021394310561898423 -0.019531075903377628 0.0019258727279209144; 0.004724715524274068 -0.038805914811576483 0.005891653322046331] %
|
|
|
|
Mass Used: 495.51091656724066 kg
|
|
Launch C3: 52.71137466891752 km²/s²
|
|
||V∞_in||: 4.244699354754754 km/s
|