23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5615464531929273---------------------------
|
|
|
|
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: 2024-05-11T21:42:57.256
|
|
Launch V∞: [7.5846097550981995, -6.3220874113566, -0.07244335823019693] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0005162842789883797, 0.00033501073627440197, -0.00016572052041179683] km/s
|
|
V∞_out: [-0.00025796008625689546, -0.0005025847486811427, 0.00029516234857622915] km/s
|
|
time of flight: 1.6929591682850966e8 seconds
|
|
arrival date: 2029-09-22T08:21:33.256
|
|
thrust profile: [0.22195148498314274 -0.03572829215405371 -0.08442331392446248; 0.12896607396544 0.04392985107276203 -0.15149642469282634; 0.056360823262788254 0.032618839837332735 -0.11617208410056172; 0.04951587501567428 0.03670572464987528 -0.14412523472566932; 0.03838002823229521 0.03320394758018536 -0.14404539529007976; 0.029811022948689897 0.028791039626656755 -0.13635950306338795; 0.0159687629312017 0.016789756571681247 -0.08677872617220729; 0.017805035203144113 0.018932500292052127 -0.1080916601779779; 0.004058537822088559 0.004644065298101291 -0.02854485811927804; 0.0006778055052861175 0.0006642449770498614 -0.005079156839242796; 0.0005223156020847036 0.00017902555211152073 -0.0016148424867509614; 0.0002917062226554874 -2.220721861227406e-5 -0.0007953550963425999; -0.001634287147248161 0.0003948342870456801 -0.0012736831409392337; 0.00037575939176021935 6.094559171585906e-5 -0.0020121993628792333; 0.00018502272110399657 0.00014608429512133524 -0.001574118981634106; -0.00017836110424175648 0.0014435780590552109 -0.00050928465849916; 9.77529294658943e-5 0.00018313565311791615 -0.0003145824504168686; 0.0004119377550584637 -0.001596513474465847 0.0011369487625414354; 0.00048536545927819227 -0.0003635654907220195 0.0013435598464413662; 0.00010053189721483783 0.00035980594965287537 -0.0033157921074507316] %
|
|
|
|
Mass Used: 86.385531309405 kg
|
|
Launch C3: 97.50034241411603 km²/s²
|
|
||V∞_in||: 0.0006373734706082649 km/s
|