Files
thesis/archive/ES_0.5630631648261913
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5630631648261913---------------------------
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: 2023-04-29T01:07:35.531
Launch V∞: [6.473853066214604, -7.400813387927307, 0.23963749238474422] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.735958240492556e-9, -1.9667746935844906e-9, 2.2240772839401556e-9] km/s
V∞_out: [1.154847191472112e-9, -2.5983876882726016e-9, -3.6819817926519858e-9] km/s
time of flight: 1.8314440099299255e8 seconds
arrival date: 2029-02-15T18:34:15.531
thrust profile: [0.28071074920635064 -0.07484755036983709 -0.09592365726491085; 0.09404541411916874 0.0246164552910271 -0.0987469544860376; 0.07354345189873944 0.038529718194958165 -0.12957530051944569; 0.06526551318777771 0.04633548771353377 -0.15733537160734423; 0.03761099471503422 0.03167041211148011 -0.11845090488234719; 0.03629240637719523 0.03546379762271363 -0.13710599141609814; 0.018532187781973714 0.020289561282564837 -0.08504687122771182; 0.010087964995721843 0.01187416455536031 -0.05313416768672633; 0.004237476881405259 0.005264193443994852 -0.02518856640015477; 0.003735780964925187 0.0049650269798863075 -0.024530990479675108; 0.0005197347059156114 0.0005396521972644817 -0.003577020751109039; -1.9719668063105045e-5 -0.00015291634379638113 -0.0006527150737134777; 0.0003045517804660296 -0.002153171104129723 -0.0018630002504553649; -0.0001495769668096399 0.0017664866532470505 -0.0024323712289031456; -0.000650426480707065 0.002265119336136655 -0.001566345223902477; -0.0010620618236613238 0.0010554498544321242 0.0007860439064891231; 0.0005351598542063939 0.0038271807204712715 0.0002212142424178041; 0.0016822025024848444 -0.0006855344180547085 -0.0009415252720606372; 0.0004107557927216973 -0.002118180134767202 -0.001640093217267277; 0.00031688916877870097 0.0005032185407223627 -0.000484189182457439] %
Mass Used: 92.58896798445903 kg
Launch C3: 96.74023845361673 km²/s²
||V∞_in||: 4.037349372296397e-9 km/s