23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5596858105605593---------------------------
|
|
|
|
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: 2024-05-14T02:24:44.634
|
|
Launch V∞: [7.960616452260264, -5.95052844454942, 0.028221467109377136] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-3.7473593756630353e-10, 2.344143416610769e-9, -1.8520621763805487e-9] km/s
|
|
V∞_out: [1.3875506600951575e-9, 2.729481811074717e-9, 6.50296764112395e-11] km/s
|
|
time of flight: 1.7947506554458568e8 seconds
|
|
arrival date: 2030-01-20T08:35:49.634
|
|
thrust profile: [0.18106902927712548 -0.01827501192414253 -0.07070733629418689; 0.022517182488445454 0.008715888053078947 -0.02965049436782695; 0.06937619587557681 0.04392084771700747 -0.15703483387626135; 0.03281390865228707 0.02606352818773926 -0.10947250855728748; 0.027471372431663837 0.02586881129469757 -0.12149139635296961; 0.022122696962951105 0.023516251477962893 -0.12210410650107281; 0.01562623221866588 0.01764803750750416 -0.10109090448212671; 0.01022789593764915 0.011453968126107961 -0.07255568631968785; 0.002176720304819515 0.0025493261573583496 -0.017471889981438154; 0.0018931900112814089 0.0029658676767281614 -0.02093110099642471; 0.004474523825828373 0.005552379242710508 -0.040935546202768534; -0.0014625648996837222 0.0006717790566099385 -0.0015275724901358894; 0.0002186158563580432 0.0012270589660251028 -0.0005099262221814516; 0.0001376283071412728 -0.0002225941169199821 0.0007923694695198736; 0.0055541558465467605 -0.0003418091855326554 0.0008751633603292885; -0.0016609953609748676 -0.0029870087956912917 0.0005867287823295478; -0.00012008767992277558 5.5687639859384956e-5 -0.00036582622244230164; 0.00343735926362706 0.0031897133051696455 -0.0028941751756723037; -0.00249501786825276 0.0008415500109828794 0.005880499360103823; -0.0010816481286788538 -0.003954141460959439 0.00695011846682642] %
|
|
|
|
Mass Used: 76.74428178385233 kg
|
|
Launch C3: 98.78099952059432 km²/s²
|
|
||V∞_in||: 3.0109084485787273e-9 km/s
|