Files
thesis/archive/ES_0.5904035063558207
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5904035063558207---------------------------
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: 2023-04-24T10:05:07.987
Launch V∞: [5.239598106899442, -8.496583547486258, -1.0152804008456984] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.0035036200535848, -0.0022142507896770356, 0.0020139905134589986] km/s
V∞_out: [-0.0027542364754951686, 0.0033065006799395938, -0.001908395347139841] km/s
time of flight: 1.3211075236293542e8 seconds
arrival date: 2027-07-01T11:30:59.987
thrust profile: [0.3330762005871614 -0.21788007266013784 -0.18350264284790918; 0.10830335121917552 -0.015159971981119735 -0.12912171380547588; 0.1497816674553335 0.010474570833719195 -0.2652379416904857; 0.12098008814812877 0.02152753842530706 -0.27893434443194925; 0.07846658340691136 0.018967650630853535 -0.2211625501653504; 0.045475614559518915 0.013019409212840595 -0.15148419634988824; 0.027155936021892278 0.009195311391686252 -0.10230320176147038; 0.025038405270160546 0.009150009686416336 -0.10344833761526723; 0.013879796470547092 0.005696376404312933 -0.06444882460324178; 0.0029341155384330292 0.0011456476897700571 -0.016564787129323345; 0.0033314088449101216 0.0014391397431539874 -0.017440076333560803; 0.00018139243920155143 1.1438779012331159e-5 -0.0009220001348893478; 8.52265653588126e-5 -5.127920114149243e-5 -0.00012088536347653017; 0.00014400956365626441 4.377613294150715e-5 -0.0008172621857909176; 8.326810313856236e-5 0.0001469430624901061 -0.0007100274278203394; -6.939757770829376e-5 -6.919882122662888e-5 -0.00025868073924823485; 0.00010234435870014151 -5.917889696433745e-5 -0.00011288072263134375; 2.333473983682691e-5 0.0005744539117598141 -0.00025642291042214275; -0.00037794259765590917 0.00044898418417850484 -2.0493348787493362e-5; 0.000302543839881721 -0.0003939085142243676 0.0001941484425008361] %
Mass Used: 101.52675561924207 kg
Launch C3: 100.67611459357978 km²/s²
||V∞_in||: 0.004608081794821982 km/s