23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5630344922364472---------------------------
|
|
|
|
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: 2023-04-30T04:54:43.444
|
|
Launch V∞: [6.542500673254356, -7.375135688435655, 0.11097360010191284] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [7.219384081000686e-6, 1.0725723927791248e-6, -2.153903611652116e-8] km/s
|
|
V∞_out: [-1.4204317242572465e-6, 3.008823997189252e-8, 7.1593610072405964e-6] km/s
|
|
time of flight: 1.846182869636346e8 seconds
|
|
arrival date: 2029-03-05T23:46:09.444
|
|
thrust profile: [0.28743855712735367 -0.08157129577562225 -0.10407883219533842; 0.035539880671876384 0.008375955942077958 -0.04110926947053927; 0.05887768179446508 0.028053416578287263 -0.11119071562938006; 0.06720982882608516 0.04305711505828454 -0.17379097015165607; 0.044125069736447274 0.034057547205811584 -0.1476633846109435; 0.02369700858679123 0.020923292769599224 -0.0984582939383155; 0.015574656641342511 0.015276375217991885 -0.07655927499447328; 0.006264641840198678 0.006605113526702042 -0.035502874322729965; 0.004550643866587046 0.005162179514440258 -0.029299076876925435; 0.015128294410176362 0.018246199944017955 -0.10228935572155486; -0.00020113832476557157 -0.00029553900574096797 -0.0001596985843451027; -0.00077151302694723 0.00023091393497799435 -0.0003214563003548878; 0.0007943742114027781 -0.0005714860836585126 0.00014697222976686698; 0.0005726883999519353 0.0006667044264016184 -0.0022212397471806393; 0.00010304988559006272 -0.0008316679988758856 0.0003939291770772037; -0.000363150881369265 0.00014237696682330565 0.0006133953988392949; 0.0009512340965894309 0.0033277264840213617 0.0014613161783278586; -0.0017973985298889552 0.0004555292620725616 -0.00020239703412383304; -7.832722560107749e-5 -5.076224904506792e-7 -0.0011057649605035126; 0.004154020474405757 0.0001006657663348045 -0.0021212936356612274] %
|
|
|
|
Mass Used: 89.8195773124935 kg
|
|
Launch C3: 97.20925662229054 km²/s²
|
|
||V∞_in||: 7.298656176093986e-6 km/s
|