23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5655478212115105---------------------------
|
|
|
|
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: 2023-04-28T15:24:46.143
|
|
Launch V∞: [6.128203578254339, -7.686343729407135, -0.03500972098868396] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [1.2887990751935201e-6, 0.00039874169529633807, -0.00025955064601353547] km/s
|
|
V∞_out: [-0.00039410492639327936, -0.00020534506195747727, 0.00016976760879803578] km/s
|
|
time of flight: 1.745445239920196e8 seconds
|
|
arrival date: 2028-11-07T20:00:09.143
|
|
thrust profile: [0.28044112674956456 -0.09566806823797479 -0.10269323102436277; 0.09142465217261386 0.015764228832547984 -0.10081662507818318; 0.0739018276910412 0.030931546095104623 -0.13506427487548536; 0.04990847447007657 0.027442454677229545 -0.12414136525794796; 0.08399684599634542 0.05805460876409924 -0.26090220432340977; 0.026120862533180314 0.020493507637248855 -0.09809686177865354; 0.020848223390251455 0.01791513321821064 -0.0910715644121864; 0.01257204340215564 0.010896823832691842 -0.06210556979597466; 0.006418855694108041 0.006692723437044422 -0.03706601141209105; 0.0021270067286035532 0.0024054554712513903 -0.015010875401455698; 0.0010854550130022559 -0.00022118405560285785 -0.0008760035903036139; -0.000475324305713376 0.0005148568200567165 -0.0009137503654855445; -0.00037327423507824375 0.00048300518411515775 -0.00038513762113480713; -0.00040271592903911365 -0.0018244240684215153 0.0013790479654447975; 0.0004120171738210784 0.0005735333216489417 -0.005278156030340447; 0.0013635824476862391 0.0006009781061589142 0.0012733720737184207; 0.004196261463953211 -0.00045336813977548676 -0.0007637759699019261; 0.00563827500080199 -0.004090705401608233 -0.008254758017550854; 0.0012586480945702794 -0.0010197960950297737 0.0017120432256820357; -0.007395879607503165 0.0015268446943400363 -0.008470942825710377] %
|
|
|
|
Mass Used: 96.09588064190757 kg
|
|
Launch C3: 96.63598470368937 km²/s²
|
|
||V∞_in||: 0.00047577635336037614 km/s
|