23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5651018999576068---------------------------
|
|
|
|
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: 2023-04-29T06:16:34.536
|
|
Launch V∞: [6.477729493195538, -7.263350955100967, 0.14741297960757918] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0016542164053959937, 0.0019513300391190206, 0.0017476911869680456] km/s
|
|
V∞_out: [-0.0018499484744421012, -0.000988634815020832, 0.002279848647539352] km/s
|
|
time of flight: 1.8749577787506595e8 seconds
|
|
arrival date: 2029-04-07T08:26:11.536
|
|
thrust profile: [0.4526351251388091 -0.10877173810862792 -0.13587300894761867; 0.0780906414898752 0.023249925698847363 -0.07568954621166211; 0.06569374135417444 0.03793232157415433 -0.10770977679203446; 0.06999873958166054 0.056219333339342654 -0.1614129658533437; 0.0531586332416524 0.05186327090442374 -0.15923440811655107; 0.02452632281286743 0.026544949785938972 -0.08937372638794835; 0.011776211052897605 0.013454761969153529 -0.04945860609371328; 0.01335435858731326 0.017249380714841347 -0.06520211224961353; 0.003231322953243732 0.004156020355796067 -0.019894200923952523; 0.0017369357541843421 0.01802182600953636 -0.02016174144352089; -0.002291837508371916 0.006332565872904044 -0.003853373012686485; 0.0008614581273609852 -0.0014359880166971827 -0.0027134776177001664; 0.0007687228644631652 -0.0005492387607231623 -0.0005515160527090591; 0.002887192134282106 0.006138309272945388 -0.00974551487165329; 5.228626957759524e-5 -0.00015466751027305416 0.0004562181723435653; -0.0060122795222949214 0.005747507231309512 -0.020281336804567694; 0.004344788247132222 -0.004740903768744139 -0.0074227513527084146; 0.0015372168656422028 -0.002451124853022121 -0.002332117077683102; -0.00820547425611561 0.0003780511691810113 -0.011595604985993952; -0.00040298414191390717 -0.0001338546713919894 -0.00040209732528484726] %
|
|
|
|
Mass Used: 106.64151703906828 kg
|
|
Launch C3: 94.73897707053824 km²/s²
|
|
||V∞_in||: 0.0030981519204931283 km/s
|