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thesis/archive/ES_0.6177447574889972
2022-04-18 10:59:25 -06:00

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archive/ES_0.6177447574889972---------------------------
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: 2024-05-04T14:23:31.202
Launch V∞: [7.009211720232806, -6.910079728508601, -0.29583880334338625] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.002002926328147358, -0.00291568737765755, -0.0002499256460485314] km/s
V∞_out: [0.00023389895226943306, -0.0011331101284642803, -0.003350047578897057] km/s
time of flight: 1.3671747610867378e8 seconds
arrival date: 2028-09-02T23:28:07.202
thrust profile: [0.45323467708107074 -0.14603085212699762 -0.17789299465203323; 0.194601191561147 0.03538647420343979 -0.1921835776353357; 0.15677571442638022 0.07022456806562496 -0.2513737112547881; 0.10242811973127085 0.057743724351784854 -0.20594691650959446; 0.07849594012371368 0.04883576795327323 -0.19221469336562372; 0.06418527480898882 0.06258383798265342 -0.24550952038317905; 0.0371257975141477 0.04168273610744346 -0.1649246988157082; 0.013568688913991628 0.008094819470986642 -0.05576132748255236; 0.0027654002193214272 -0.0038639664331410195 -0.005334420439501602; 0.01918912392533797 0.025246532203011415 -0.013106827822836536; 0.01344935246260939 0.015897892756120743 -0.07387050620090202; 0.04417114420597643 0.00185690699040226 0.002454103944409791; 0.051808137692743624 -0.02903583967132867 -0.018572529656773366; -0.012170892487920654 -0.0036106248820859197 -0.004904064778645748; -0.009141744830228261 -0.0047834889674437005 0.039693272104181485; 0.027827659025466314 0.03947611651430098 -0.02796548302834502; 0.002235433338646868 -0.023950430356671146 -0.09437893777648805; 0.024569133965316032 0.028600363991244517 0.07649797757436146; -0.017947815702252654 -0.07315698893152581 0.06306861403985178; 0.039461504559884494 0.13541803167114475 -0.14169949395982326] %
Mass Used: 155.0685506232412 kg
Launch C3: 96.96577139095808 km²/s²
||V∞_in||: 0.003546182396432845 km/s