23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5620530279762048---------------------------
|
|
|
|
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: 2023-04-30T19:51:17.284
|
|
Launch V∞: [6.298750871620056, -7.480994156656534, 0.04162967784589882] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-2.4999462694909455e-5, -4.00463877365598e-6, 7.009378471820575e-8] km/s
|
|
V∞_out: [4.7757331495445945e-6, -1.1063050744104162e-7, -2.4883018504247365e-5] km/s
|
|
time of flight: 1.8439403305671442e8 seconds
|
|
arrival date: 2029-03-04T00:25:10.284
|
|
thrust profile: [0.34658849429635696 -0.093114152360063 -0.12270421615098169; 0.13863880077480067 0.03475845396966808 -0.14793358822527297; 0.05188061783738573 0.02571052038048276 -0.09418450518463048; 0.05974450221105237 0.03984091717119091 -0.15159911338905246; 0.05187947093024112 0.042267574911727536 -0.16858660096114875; 0.02734624115205894 0.02515720104754133 -0.10927163125562345; 0.013617272647683585 0.013252178456869417 -0.06155142745732977; 0.0100131094822773 0.01123402253127408 -0.05402083395160272; 0.004437104580270183 0.0054774109621785255 -0.02735963317956878; 0.0008735017968103119 0.001407330552043624 -0.00673766860989239; 0.00044212914319373246 0.0005922606871556545 -0.0017989256385994104; -0.0010784256943171529 0.00025144428880657325 -0.001945837950814868; -0.0002957165418531324 7.570853356062712e-5 -0.0005896979277588644; -0.00021634768413778503 0.000704784638518351 -0.0013844625015605318; 0.00011053243321741766 0.0013753487214146186 0.00029147183059130164; 0.0005004306901681161 -2.3906301068757027e-5 -0.00036632227750964144; 0.0001968744494451903 0.0006741942175448328 6.970936101251789e-5; 0.00044099495254149685 -0.0034038667482831223 -0.0007405222818563943; -0.00062952139696636 -0.0011680202240019906 0.002255909239275997; -0.0010075914486373768 -0.000600368035069995 -0.0003610231707352365] %
|
|
|
|
Mass Used: 97.82112929458208 kg
|
|
Launch C3: 95.64126914474119 km²/s²
|
|
||V∞_in||: 2.5318277585181312e-5 km/s
|