Files
thesis/archive/ES_0.7708266646318561
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.7708266646318561---------------------------
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: 2024-05-24T07:10:51.626
Launch V∞: [7.18595210949459, -9.497910569534671, -2.2039880539611967] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.9814652002911279, 0.9658003215468179, 0.6660240981857164] km/s
V∞_out: [1.1984019627234141, -0.7224586179867588, -0.6268446670504293] km/s
time of flight: 9.055800002582112e7 seconds
arrival date: 2027-04-07T10:10:51.626
thrust profile: [0.7759669011219986 -0.6805922623340009 -0.3945294350905995; 0.0041468800563150025 -0.00367978028032835 -0.0074920636215688756; 0.0021123569331095754 -0.0006478081961683712 -0.007612067915325479; 0.0019604742842330735 -0.002220223990912737 -0.0011730897376965007; -0.00021458171777894884 -0.00012721101928649852 0.0012572234513397716; 0.0023072257566851126 -0.0030228196438936033 -0.00571703044206111; -0.0021485625552564985 -0.00026710563075453585 -0.0027996567015462683; 0.0010669132561049075 -0.002950888483436479 -0.0049097916766478004; -0.002869602618887232 7.611322682638151e-5 -0.0036221596572486355; 0.00039995921147237734 -0.003341146280407932 -0.01080244976285254; 0.0019463608126379706 -0.0032186600258072885 -0.005983113218490137; -0.0005727570981256588 -0.00012066786593306579 -0.0009991511604624031; -0.002052710973730656 0.0006313943859860066 0.0002829069969618194; -0.0011203672884958406 -4.694584332919148e-6 0.002340427592737097; -0.0007035518843665368 -0.003074118827495869 -0.0037644302591128736; -0.0018609632107715207 -0.0012686040108571895 -0.002568474341576145; -0.008353600657365089 -0.00017100509063236588 -0.003241817613321006; -0.0006160285214324301 0.0003446729012198848 0.0026645904141301426; -0.0027873155857055113 -0.006432445688126773 0.0007389327266060525; 0.000323578505003414 -0.007647816031049866 -0.0014473034329406157] %
Mass Used: 43.51408061897973 kg
Launch C3: 146.70577624883182 km²/s²
||V∞_in||: 1.5295856628010531 km/s