23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5657266555368381---------------------------
|
|
|
|
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: 2023-05-01T17:15:26.566
|
|
Launch V∞: [6.390256732490131, -7.60075621558592, 0.0930468496034348] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0009618571742181429, -0.007012886608941504, 0.009510639615257173] km/s
|
|
V∞_out: [-0.008094035906940853, -0.006810451877103108, -0.005352383530742729] km/s
|
|
time of flight: 1.814654047186895e8 seconds
|
|
arrival date: 2029-01-30T00:18:50.566
|
|
thrust profile: [0.16941567221645448 -0.053891902135307125 -0.06724045045244408; 0.07527658947514758 0.013416721596064383 -0.08957077844165505; 0.04779087976224052 0.018559549684447108 -0.0955442218467054; 0.03819128540359874 0.01985451139596026 -0.10573044053181087; 0.029326596880492592 0.018309709313500455 -0.10372703558958606; 0.02579626924369504 0.01804212829509678 -0.1090849084134074; 0.01993158161631152 0.015153495504552611 -0.0980243989767952; 0.009360368789638215 0.007371444674724689 -0.051991302589770895; 0.021155241182112268 0.017997413462848548 -0.12767352141643443; 0.00023851998339762854 0.00010572710310580456 -0.0026694029898328346; 0.014593664978626627 0.012469884649732204 -0.09763095239419785; 0.0015960159430156075 0.0008797012530082539 -0.004639715461686808; 0.00026656968975342444 0.0006370494845222611 -0.00563037083199505; -0.00018665821948228578 0.0004530677213523274 -0.0032683746808168292; -0.00021692403620151435 0.0002896039996160589 -0.0010475512210532758; -0.00117313011075101 0.0026595215254934528 0.0011536598586807945; -0.0016080086551883825 -0.00020563946433835105 0.0031822293198444174; -0.00045318475486891795 -0.0010106156834970119 0.0009162043585076115; 0.0002644791887368415 0.004285361580044819 -0.005441995939311606; 0.0006265979572653265 -0.0014113790595736923 -0.0015538274013779559] %
|
|
|
|
Mass Used: 84.75715053891781 kg
|
|
Launch C3: 98.61553387212457 km²/s²
|
|
||V∞_in||: 0.011855716499004397 km/s
|