Files
thesis/archive/ES_0.5692513711755627
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5692513711755627---------------------------
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: 2023-04-27T16:49:01.855
Launch V∞: [5.937451918127766, -7.570162563705861, -0.7677535141172369] km/s
Phase 1:
Planet: Saturn
V∞_in: [9.341080822636657e-8, -5.3503828128996896e-8, -7.987099667318609e-8] km/s
V∞_out: [4.032513907950651e-8, -6.36681376257002e-8, 1.0672589468473879e-7] km/s
time of flight: 1.781187793968394e8 seconds
arrival date: 2028-12-18T06:15:20.855
thrust profile: [0.5407646071145349 -0.16659957240102788 -0.15633106575088795; 0.16354459202205995 0.050093389605903926 -0.14934250634923155; 0.06400787277165769 0.038183988741546965 -0.10014057225879563; 0.07423990332112383 0.06189475046906031 -0.1553725071089696; 0.052476235522137295 0.05442088787775859 -0.1424061711616853; 0.025922385493736044 0.03026471110144073 -0.08800332250415613; 0.018389193485294233 0.024698245351059255 -0.07371731672633365; 0.016791551979922804 0.026867521907569084 -0.07983429552259322; 0.0070355159984163956 0.01236768799244874 -0.03757836953731133; 0.00971798483517548 0.015567106966100095 -0.051678414238588516; 0.0037517559770404154 0.007910144071976138 -0.02701308637456469; 0.0012738286568488044 -0.0008785835795091608 -0.0014200101832062733; -0.0014112480835707548 -0.0008075547869730759 -0.002714734064712453; -0.0012231443722408547 0.00042119471917661925 -0.0042182037792661276; 4.1013864156516644e-5 0.0012882873536301806 -0.0024736628330529493; 0.0004570974545297999 0.0055499298010370755 -0.005379728829538609; -0.00044004771408898786 -0.0008311383437379014 -0.0029829428767628695; 0.0009392566972902298 0.0007911519995829732 -0.0017541127499784313; 0.001161537888261734 -0.002008622866058931 -0.002472931575534771; 0.001564880740397125 -0.00025727964360625533 -0.004400148318148649] %
Mass Used: 120.75077149135222 kg
Launch C3: 93.15014197945216 km²/s²
||V∞_in||: 1.3404333190251717e-7 km/s