23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6241214306441089---------------------------
|
|
|
|
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: 2023-04-24T17:39:05.426
|
|
Launch V∞: [5.240995269171102, -8.7001814592056, -1.9865199784355771] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.004830806646253824, -0.004024940619352588, 8.963339571441347e-5] km/s
|
|
V∞_out: [0.0021528468731978347, -3.073319215626555e-5, -0.005909003059841316] km/s
|
|
time of flight: 1.1520795213209777e8 seconds
|
|
arrival date: 2026-12-18T03:51:37.426
|
|
thrust profile: [0.4936313742483307 -0.38038621164640735 -0.3161802296676532; 0.17297476709444726 -0.038275205828306125 -0.21075793449170077; 0.12149419587633663 -0.00221673124842179 -0.2170246815038619; 0.10982405689027756 0.00998863009789275 -0.24998316605675416; 0.08865598788647155 0.014519515691460289 -0.24043024487457276; 0.03241652614029359 0.007035404672523815 -0.10571439432991937; 0.012961557290907385 0.0014643322392124906 -0.03873958999282058; 0.014673358563725845 0.0037440929768316174 -0.0389839039616038; 0.012285673488781162 -0.005764100910900408 -0.014206496293595999; -0.000632303521775785 0.0034534729021310257 -0.00648219762970412; 0.006533585515685992 -0.004944203506209362 0.006250313200063307; 0.0006231540323463148 -0.0024920790536746363 -0.02566953707815866; -0.0008674479806068848 -0.010884654570266933 0.008431667813966972; 0.012362979166379622 -0.0279002574786595 0.012632751509964202; 0.008231611543093889 -0.02418742257175747 0.02570462742696893; 0.0019357501165303793 -0.00544273283837786 -0.007027209036136757; 0.010918687493579484 0.02495889723863366 0.0002874441357733754; -0.018126339311866246 -0.013484615028862147 0.028434361673165702; 0.006614088653067822 0.03431948532932626 -0.011434494038020835; -0.04419383033004783 -0.016499356360073936 0.01929034265677601] %
|
|
|
|
Mass Used: 103.34820807219603 kg
|
|
Launch C3: 107.10745045930246 km²/s²
|
|
||V∞_in||: 0.006288471514480431 km/s
|