Files
thesis/archive/ES_0.5705418725155025
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5705418725155025---------------------------
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: 2024-05-08T09:13:17.715
Launch V∞: [7.222568819016708, -6.709798116624502, -0.40659172617342976] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.867074101958038e-6, 1.0706162762267287e-5, 5.4339365005164974e-6] km/s
V∞_out: [8.631544687134237e-6, -7.82006037348318e-6, -4.8428296473869095e-6] km/s
time of flight: 1.5183253161300537e8 seconds
arrival date: 2029-02-28T16:55:28.715
thrust profile: [0.33874909245307894 -0.08486776647994551 -0.13919288885787115; 0.09389080669744461 0.022138861501189707 -0.11255922086248099; 0.09525074493188174 0.044588511235513696 -0.18429103552891127; 0.06411520927424953 0.04015445695398257 -0.1757111216996553; 0.04683286801045586 0.035996341449610315 -0.15980233907151192; 0.03747861830830017 0.031230215664376098 -0.15706259756253135; 0.030543092227518085 0.02800644049422719 -0.14758324568083175; 0.01629723832290882 0.015648055177170595 -0.09229826417174505; 0.01329814691581197 0.01189686989324966 -0.07817676630246796; 0.0019030151967065296 0.0018701857341181264 -0.012879795698363204; 0.0014272593511682721 0.0015475232795488705 -0.010493721697634267; -1.686400448433511e-5 3.873383809800809e-5 -0.00019631317852761483; -9.189437470170804e-6 1.8139921347240272e-5 -6.79540451451842e-5; -3.603437974871891e-6 2.5315895688174953e-5 -0.0002564178251713968; -9.316686311563172e-5 -6.611980993648662e-5 -0.0002194872896831197; -5.3439917226698525e-5 2.4617582508925215e-5 -0.00020161021111570577; -2.427675793244202e-5 0.0001647288026235439 -4.821599887020027e-5; -5.256219564526697e-5 -0.00023470980545454978 0.00015767654453347415; 0.00014141815680520408 2.4570826845705596e-5 -0.00010909845788978844; -0.00014607461654514734 -0.0001703269932072313 6.252368156475034e-5] %
Mass Used: 97.74430493343652 kg
Launch C3: 97.35220794308282 km²/s²
||V∞_in||: 1.2613637425177512e-5 km/s