23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5621286397563757---------------------------
|
|
|
|
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: 2024-05-16T07:04:23.608
|
|
Launch V∞: [7.968578445830458, -5.960669267968358, 0.8047883039950808] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.1420855484327564e-9, -3.243123326598524e-10, -1.6452918858033918e-9] km/s
|
|
V∞_out: [4.748694019650393e-10, 1.0053149322255025e-9, 2.4636105753637124e-11] km/s
|
|
time of flight: 1.824442914053039e8 seconds
|
|
arrival date: 2030-02-25T22:02:34.608
|
|
thrust profile: [0.17669695105022745 -0.01866160728560164 -0.06640451136172384; 0.03697197738581524 0.012453791481701152 -0.047682983020009076; 0.04189049072151084 0.02096882863131101 -0.09337828576047232; 0.04428400852820306 0.025803234640496327 -0.13864759910528288; 0.03196582737577009 0.02028366509396404 -0.12688931644925674; 0.029889928070820224 0.019425762856701254 -0.14058214478856396; 0.01762799865662875 0.011702094282918222 -0.09543629401066028; 0.008539063905643213 0.005714177013584387 -0.05209535980225471; 0.0021814821248624734 0.001261426207621375 -0.014885683293231993; 0.0035087366121320366 0.002294434676450036 -0.023125117396643514; 0.0016337731867853845 0.0012769679706175073 -0.010741436045226057; 0.0009264646759724999 0.00101067876081731 -0.006607818774779652; 0.0004925308965674092 -9.475368452419085e-5 -0.0035613783332743443; 0.0003359838861691273 0.004511234120704658 0.0007787869899612884; 0.0016801345749467764 -0.000815832044498923 -0.0014610322393015809; 0.002497542222853041 0.0010175522345523902 0.0015865678006617753; 0.0007546041569397976 -0.0011702545242091244 -0.0032477159601950276; 0.0004289806985069249 -0.0001801945658434692 -0.0031573518325351477; -2.6438745829403005e-5 0.005001598504437729 0.0003363379124340822; 0.002331188785964717 -0.00013233221827901734 -0.009931571375631134] %
|
|
|
|
Mass Used: 74.37630181083478 kg
|
|
Launch C3: 99.67550478370347 km²/s²
|
|
||V∞_in||: 2.028921703404226e-9 km/s
|