23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5656224107763604---------------------------
|
|
|
|
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: 2024-05-21T05:36:43.270
|
|
Launch V∞: [8.038933596166302, -6.147955821552678, -0.09016690034013546] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-2.3060076053535517e-8, 1.943002872568467e-7, -3.585465441427411e-8] km/s
|
|
V∞_out: [2.8884169026236803e-8, -1.1543370604513625e-7, -1.559147882980159e-7] km/s
|
|
time of flight: 1.8608742222027668e8 seconds
|
|
arrival date: 2030-04-14T00:33:45.270
|
|
thrust profile: [0.07023734985850105 -0.010820236301619879 -0.03321356610933114; 0.02663653773477778 0.004472334099819988 -0.043877786780785764; 0.06107324579931441 0.009010579760913587 -0.17202373798267837; 0.023256782605692673 0.0032295000677397415 -0.08992516139344181; 0.013143192313307957 0.0003861890099825538 -0.06322585526591966; 0.01183969016248165 -0.0004910486603125554 -0.06175134911051707; 0.02925093775921988 -0.0024043939687518863 -0.16631227049552372; 0.007695818872049882 -0.0009212716694864627 -0.04848153157654403; 0.009671466141311555 -0.000328053980843756 -0.05482143318211164; 0.0023198896781470753 -0.000662154771723579 -0.015716183962517262; 0.0017114022054825217 -0.000846264919395595 -0.013570064531849977; 8.924809067004059e-5 -2.268447477207894e-5 -0.001723470598145647; 0.00015502057435165648 -0.00018319177881715603 -0.0003375348814247325; 0.00019113665467348278 -0.00022045707132575703 -0.0007347176443685666; 6.968872875336466e-5 -3.6763181143812176e-5 -0.000522308370148679; 0.0002898659795303502 -0.00016256626579902006 -0.0003048150919037584; 5.882697087015595e-5 -9.972433111562878e-5 -0.0006367044274405212; -7.432452710782306e-7 9.856607156579473e-5 0.00041086766167709493; 3.6453575683416164e-5 2.773671068330262e-5 -0.00024740286816775684; 5.510936432759491e-5 0.0001812979869122704 0.0002396191502342035] %
|
|
|
|
Mass Used: 62.38480463845235 kg
|
|
Launch C3: 102.42994421725169 km²/s²
|
|
||V∞_in||: 1.9892190673441427e-7 km/s
|