Files
thesis/archive/ES_0.5621989816643226
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5621989816643226---------------------------
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: 2023-04-30T07:17:12.747
Launch V∞: [6.687494775745216, -7.294089074810475, 0.019126854878210073] km/s
Phase 1:
Planet: Saturn
V∞_in: [3.6129613683961654e-8, -5.101635911421105e-8, -4.1713186329702775e-8] km/s
V∞_out: [7.3789354185512e-9, -4.071624193723899e-8, 5.703530748215417e-8] km/s
time of flight: 1.8749577783328566e8 seconds
arrival date: 2029-04-08T09:26:49.747
thrust profile: [0.22582244201248858 -0.05526615994875543 -0.07817046906932047; 0.06855006834270154 0.020656905224968356 -0.07229965361234594; 0.03887650796559524 0.02236411171722171 -0.07005331231752769; 0.03532178268794275 0.027305692690194706 -0.08882328553111377; 0.025297810985686817 0.023837843565412395 -0.08236094660281315; 0.0491735708953156 0.06716104521332827 -0.2127694819211813; 0.019664522783905226 0.024134635189577217 -0.0920867674319831; 0.010057377077448394 0.014314230619386088 -0.057617275946609176; 0.017544334473247186 0.02569042203557086 -0.1066545230742764; 0.0019539889174100215 0.0034173819208276135 -0.01500467979890083; 6.442698976082282e-5 0.00011179542492879484 -0.0005050308682284835; 0.0001101359870611409 0.00020716866701098814 -0.0008049135592140957; 1.5190792465668989e-5 4.1789892509894857e-5 -0.00017896326839158874; -2.2633819539221695e-5 1.2160126708256157e-5 -8.172668630405185e-5; 0.0001196871949354795 -4.101279973967388e-5 -0.00014970367416588634; -0.00014329852453907795 3.040353637197372e-5 3.381546591362558e-6; -4.0175384783492504e-6 -2.4096932240609694e-5 -0.00021821038097788266; 8.600001078981663e-6 -6.579421553295329e-7 -2.970739824568325e-5; -4.038543288425409e-5 4.8047708692963644e-5 -2.8835317501567332e-5; 6.541255333878296e-5 -0.0001217183565216518 2.378086678916006e-5] %
Mass Used: 84.65980068815452 kg
Launch C3: 97.92668764346661 km²/s²
||V∞_in||: 7.51532287796004e-8 km/s