23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5601962119561941---------------------------
|
|
|
|
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: 2024-05-17T10:55:27.622
|
|
Launch V∞: [8.081766079635731, -5.877570386667416, 0.06796524073399662] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.024064294226755e-5, 1.6156659530849994e-5, -1.2844293124200135e-5] km/s
|
|
V∞_out: [4.270930722937318e-6, 2.8530232856018443e-5, -1.3821368641941062e-6] km/s
|
|
time of flight: 1.861720781146942e8 seconds
|
|
arrival date: 2030-04-11T05:23:25.622
|
|
thrust profile: [0.13187444975255894 -0.007590036424381059 -0.05386614551548289; 0.04569960800328174 0.018923529598819846 -0.06025147419155559; 0.026976734449080216 0.016538195714416698 -0.06265193542864204; 0.03694794149186058 0.02875598234895544 -0.12732615468540906; 0.026631061198844303 0.022657285598313835 -0.11668083157258141; 0.01751857771912978 0.015738061545899594 -0.0925886837265248; 0.017101340940077814 0.017022845838557222 -0.10852884325737047; 0.010112725577869876 0.008841207040117774 -0.06258885039121123; 0.002872017371931751 0.0033513051098649897 -0.03386170920376252; 0.0041202592061827395 0.0008071556430445659 -0.014327872610851767; 0.0019806542743509292 0.0019544526712058597 -0.013158595662103843; 0.0019293134242888183 -9.548056371100691e-5 -0.01660435101835138; 0.0005690109052957683 0.0006569692392500925 -0.0028387852336698126; 0.0007088019246543095 0.0009783520756794194 -0.00644056072087178; -0.004099802420881812 0.0017413363419950157 -0.007103410838114076; -0.0065267056483321075 -0.0028557812245937012 -0.012624619875742382; -0.0008744842174607358 0.0009989637301796358 0.0021840337803842877; -0.000258007030652672 0.0022278744913426865 -0.010080965922042183; -0.003085678965488053 0.001979495481119047 -0.0044153204740704196; -0.0005554736367812479 0.007997168574162342 -0.003323582913587869] %
|
|
|
|
Mass Used: 71.01410458981036 kg
|
|
Launch C3: 99.86539589012847 km²/s²
|
|
||V∞_in||: 2.8908426795184584e-5 km/s
|