23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5683466675267036---------------------------
|
|
|
|
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: 2023-04-25T01:21:40.624
|
|
Launch V∞: [5.9754546044296335, -7.241836639974111, 0.25458454226522614] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.01803061662179582, 0.00029844697329320304, -0.015275612096688302] km/s
|
|
V∞_out: [0.023131960665448384, -0.00018198748799232574, -0.004906556340469408] km/s
|
|
time of flight: 1.8483924682692012e8 seconds
|
|
arrival date: 2029-03-03T09:35:46.624
|
|
thrust profile: [0.8341908258072941 -0.2002065329899016 -0.19207528386364825; 0.3382538734507374 0.12262266400100585 -0.2399114503250459; 0.07669824252257032 0.054464325931664656 -0.10187459168552947; 0.06434291723544268 0.06270827725698544 -0.11924678356168379; 0.02682275739099628 0.032726082782737156 -0.06743478899100504; 0.03328439789261629 0.04722691326648402 -0.0992370048121439; 0.01941431885109006 0.03325990830370922 -0.07705219912454497; 0.015352133501965345 0.025260689488066077 -0.061804218023087436; 0.007327928835236574 0.016425501751587496 -0.03892562155570264; 0.0012490760623421434 0.001067806333104313 -0.002303209495925787; 0.00037129368282611355 0.0010322514035333932 -0.001364722617703139; 0.0020146652997881896 0.00031227415122060307 -0.0002701326439832956; -0.001014799640477716 0.0006988468462337831 -0.0004996049641876896; -0.00045385837265082086 -0.0007208751488436242 0.0006559795454929698; -0.001009581040766414 -0.0013744536960847375 -0.0015039828308622658; 0.0004562659929699687 0.0024859658183435107 -0.00014013087645202383; 0.0016969675294665459 -0.001223328899622554 -0.002132721020728279; 0.0021357231464322864 0.0006665197420646363 -0.0022218695360560164; 0.00033526350689357267 -0.0027930821527431928 -0.0014863025985138124; -4.5272265648774675e-5 -0.0021528737886432523 0.0016716364082425854] %
|
|
|
|
Mass Used: 148.4832099713053 kg
|
|
Launch C3: 88.21506893883124 km²/s²
|
|
||V∞_in||: 0.023633377483688985 km/s
|