23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5750782899471119---------------------------
|
|
|
|
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: 2024-05-12T05:06:59.227
|
|
Launch V∞: [7.896647320013671, -5.80982421471794, 0.07636853936831597] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.9634585067778925e-8, -2.851438850110954e-7, 4.75014456211544e-8] km/s
|
|
V∞_out: [-4.385722073516104e-8, 1.6901295531027886e-7, 2.3282356759227e-7] km/s
|
|
time of flight: 1.8166143638258004e8 seconds
|
|
arrival date: 2030-02-12T18:37:35.227
|
|
thrust profile: [0.34852435074755833 -0.007398245569614951 -0.1120106022319188; 0.098799330290049 0.055102438505709485 -0.11096338904303192; 0.04293062571761016 0.03992722039081983 -0.08909396280363781; 0.030385930253594633 0.03766877090019772 -0.09379926407663279; 0.026050032784164796 0.039307343458040774 -0.106231720284235; 0.02036018321106558 0.03627543086418118 -0.10399646186922526; 0.023609488253762315 0.05016171352941503 -0.15359462413066005; 0.0058324718170537325 0.015750588693384707 -0.05456217007517488; 0.008383153622640608 0.021491455066713967 -0.07404592525389408; 0.0010906277824052337 -0.0004454590769454323 -0.005745932033730177; 0.0002989638937209209 -0.008874438578762902 -0.005669585183994031; -0.008508301600873774 0.003544864954817361 0.0027852535916433577; 0.0029553667093857737 -0.011266440225439982 0.006989203843757818; -0.005324317835681935 -0.014401645178627279 0.016462547820210234; 0.02334704476446995 0.0163077579400831 0.03597424696596237; -0.006837319664585734 -0.00620009014416092 -0.00200040234970943; -0.009620834672729756 -0.0010482614150407715 -0.0016206782342492597; 0.005076737434846611 0.011861810211742423 0.011340994403034434; -0.05419506906939138 -0.04064528802099114 -0.006899783117095585; -0.009540455479000514 -0.04036010926737608 0.025158144533556415] %
|
|
|
|
Mass Used: 110.2425889425881 kg
|
|
Launch C3: 96.11692845640727 km²/s²
|
|
||V∞_in||: 2.905884222185387e-7 km/s
|