23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5622200841033569---------------------------
|
|
|
|
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: 2023-05-02T05:46:41.605
|
|
Launch V∞: [6.611431715867652, -7.400491219640692, 0.061429011042091246] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [5.2485050988682736e-8, -5.573980846881966e-8, -3.1756227833310265e-8] km/s
|
|
V∞_out: [2.002195847106908e-8, -4.126849759852372e-8, 6.244255595899809e-8] km/s
|
|
time of flight: 1.874957778728606e8 seconds
|
|
arrival date: 2029-04-10T07:56:18.605
|
|
thrust profile: [0.15750668147938088 -0.04316529072292357 -0.059596126463882994; 0.10683411052827774 0.026724967991195697 -0.12184100330658033; 0.04475091214714592 0.020568027374296815 -0.0889982620415618; 0.035168548193674105 0.02151423334820037 -0.09757979583776802; 0.03795498981991643 0.026846098838507335 -0.13576952899122818; 0.029508422461564758 0.02452522040601386 -0.1282271105562053; 0.01882054005003157 0.01634468121142072 -0.0972215894954363; 0.014709652141519565 0.014208326027451187 -0.08328511836724228; 0.007905295637579593 0.008210929172985507 -0.050763405236315236; 0.0011738657102275366 0.0015197245243501053 -0.008183533567069285; 0.00038014072550110744 -0.0002473851553826959 -0.0008894222908882644; 0.0007336150073081531 -0.0002761384794568057 -0.0030634782472365174; 8.627248624733827e-5 -2.8285341036213447e-5 -0.00037579935543627786; 0.00021050668207135123 -0.0010679131900952685 2.4777854452251273e-5; -0.0002854848574763433 -0.0008693807115906082 -0.001591681156992071; 0.0006543458407903233 -0.0003347832134743593 0.003600937778805033; 5.854772560340933e-5 0.00012049434352917772 0.0015167370205703059; 0.0005825461176490263 -0.00017278558361782345 0.0019325364154206687; 0.00011304903365038847 2.8289784642697847e-5 -0.0021405172103992403; -0.00016927938740393618 -0.001957110414061861 -0.003942828535572883] %
|
|
|
|
Mass Used: 81.44467141833229 kg
|
|
Launch C3: 98.48207314895727 km²/s²
|
|
||V∞_in||: 8.288585423114391e-8 km/s
|