23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6069247253106476---------------------------
|
|
|
|
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: 2023-04-12T04:54:57.498
|
|
Launch V∞: [5.8524003945900445, -7.6549350737779465, -0.4459923493644513] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.00862531280179509, 0.011821099304665841, 0.012185124686361657] km/s
|
|
V∞_out: [0.017256258452043878, 0.008071202533803097, 0.0004043512418145332] km/s
|
|
time of flight: 1.549486792354712e8 seconds
|
|
arrival date: 2028-03-09T14:12:56.498
|
|
thrust profile: [0.6336441874553369 -0.30644379655727283 -0.16051849598900667; 0.5064580939086286 0.06943417754318293 -0.3029886330269146; 0.36757596783306656 0.15572596144160036 -0.34064287328661125; 0.2498651888749275 0.15620145251945408 -0.3099651758965332; 0.1381583154245436 0.10883661358684456 -0.2142509326570666; 0.03304014813932945 0.030957992605779583 -0.06316556215285468; 0.006174759772617598 0.006852576378554774 -0.0143758840317424; 0.007124553476478183 0.009048120700531312 -0.018800763834665727; 0.0022608879729786816 0.0028875521195052233 -0.006686582029887532; 0.0008791429029181331 0.001235163420801001 -0.0030198256657251277; 0.0004143947010924598 0.0003077134446903906 -0.0006779676649386065; 2.6241679491617197e-5 0.00012993683349414193 -0.0003560528286848905; 0.00014768046035904057 0.00020006240720788407 -0.0007837311937847217; 0.00016070231820566855 0.0002459390834099463 -0.0006516281516300531; 0.00023560807406733316 0.00029557008757216837 -0.00036379358472368164; 0.0006342846705154926 -0.0002306839171692309 -0.0002047623294853409; 9.313231287481799e-5 0.00012693200256954826 -9.940078890975456e-5; 0.00046991902880634594 0.0003086033307036304 -0.00025398406505432224; -0.00011892248544097131 -8.87772789509491e-5 -0.0002390616958756679; 2.2383574421934324e-5 -2.2344618750113132e-5 0.00039279184389751694] %
|
|
|
|
Mass Used: 165.30158472382573 kg
|
|
Launch C3: 93.04753053804511 km²/s²
|
|
||V∞_in||: 0.019042365223935858 km/s
|