Files
thesis/archive/ES_0.5623901152367882
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5623901152367882---------------------------
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: 2023-04-30T09:39:14.806
Launch V∞: [6.329003028339492, -7.397617727942817, 0.14423451218644542] km/s
Phase 1:
Planet: Saturn
V∞_in: [5.947487418475093e-7, 0.0002113927226540332, -0.00014010352094560188] km/s
V∞_out: [-0.00012807685698547664, -0.0002142102039271571, 4.475057500454035e-5] km/s
time of flight: 1.8749577787496182e8 seconds
arrival date: 2029-04-08T11:48:51.806
thrust profile: [0.4144213745048421 -0.08102842562577636 -0.11225628987362121; 0.0820375819311321 0.02804820588442612 -0.07575844661852414; 0.10172700820036046 0.06815715717969067 -0.14708151441359804; 0.06906553128358375 0.05902988793570194 -0.14854981383377178; 0.03598776171185312 0.03989286933364517 -0.10197255021079284; 0.034895950046913315 0.04089372036241859 -0.11057436644571983; 0.013752891569329479 0.01884116212260843 -0.05697245102451549; 0.007923832273735193 0.013607125452852795 -0.04241990807180692; 0.008664369631303598 0.01423366859795179 -0.05101704499750254; 0.0062965827140621594 0.010989816469281837 -0.03764294221829758; 0.0025504200949055507 0.00485119749812786 -0.01989852678448461; 1.2989382668328239e-5 9.681322105175669e-5 -0.0001674431398736763; -0.00021766507498304017 -0.00010739888709358857 -0.0008851971654125462; 0.00016079195088456065 -0.00017629447877917585 -0.00033709965275404753; -0.0002547072937789358 -0.000283011476502501 -0.00040585009902954647; 0.00017408505031600948 0.00013869385693611984 0.00016378272356397394; -0.00013132284819707173 0.00017948945895027559 0.00010547055069032578; 0.0009800326779366383 -0.0001886487996328301 0.00019047002446191024; 0.0001255648251015036 -0.0002173648443549598 -0.00014756477291466268; 0.00043656233871160335 -0.0003283118479496399 -8.22662303364465e-5] %
Mass Used: 103.11112041619481 kg
Launch C3: 94.80183097600995 km²/s²
||V∞_in||: 0.0002536064539764429 km/s