23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5607692152333923---------------------------
|
|
|
|
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: 2024-05-12T00:12:05.562
|
|
Launch V∞: [7.573326491396061, -6.265747744730003, -0.09623294973406434] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7476919284538095e-6, 2.589533099060004e-6, 2.4812208024096865e-7] km/s
|
|
V∞_out: [-2.1040046651064808e-7, 9.74587243365498e-7, 2.9791607941254495e-6] km/s
|
|
time of flight: 1.7221647258703893e8 seconds
|
|
arrival date: 2029-10-26T06:06:37.562
|
|
thrust profile: [0.28391275820025785 -0.026256068983924335 -0.1004526029219305; 0.10412635551459114 0.04752852416235016 -0.1186159732560821; 0.07624813070379562 0.0567697992464339 -0.14742906720199986; 0.050414272661946063 0.047530697801217534 -0.13687549642010421; 0.038809156394488696 0.045055724164390826 -0.14374747309034336; 0.03246869396280766 0.03705645769936438 -0.13777812446093818; 0.017373262921246645 0.02701900824518621 -0.09335685351541985; 0.00618964334759234 0.009706572904401712 -0.04328708858446387; 0.007214552759749939 0.015030014470900303 -0.054903607259249816; 0.0005748254951122127 0.0008669637448006584 -0.003910518364589583; 0.00012615898038715164 0.00044590461433890603 -0.001963781575574966; 0.00012574374665302445 0.00035991319978348333 -0.0013734645591182318; -0.0002737706883402017 -0.0006576694304464898 0.003055011438340683; -0.00024747501876675967 0.0006599830666776765 0.0011310310486851722; -0.00018209285153315623 -0.0020536642040541345 -2.347648786279349e-6; 0.0007230874174349142 -0.00019475130984765207 0.001718358034901587; 0.0008132965417519823 -0.0014018141928438554 0.002179824414841402; -0.0001408774655306673 -0.0007225315017399857 0.0018557479132864326; 0.0012188856931849288 -0.00017298776999448168 0.000445681863198373; 0.00016639844293788526 0.0002579081507207042 -0.00019453010504939295] %
|
|
|
|
Mass Used: 90.58999436779504 kg
|
|
Launch C3: 96.62412972648502 km²/s²
|
|
||V∞_in||: 3.1339548999009237e-6 km/s
|