Files
thesis/archive/ES_0.6733538593181823
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6733538593181823---------------------------
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: 2023-04-26T00:22:06.528
Launch V∞: [6.080208184161847, -8.96965295809641, -2.4366693363582135] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.0024714744598132925, 0.0013138490158394005, 0.0025854286769126426] km/s
V∞_out: [-0.001232354207456028, 0.002581500718672633, -0.0025168434859120462] km/s
time of flight: 9.381781238643846e7 seconds
arrival date: 2026-04-15T20:52:18.528
thrust profile: [0.682372547382676 -0.5387547942354074 -0.36304296611926234; 0.25186050720341535 -0.06838730036907337 -0.2242556332915564; 0.0795449367835255 -0.005646748090427428 -0.10225796156118193; 0.06644616441857368 0.002689759181354675 -0.10429752817619402; 0.04203898020352377 0.004334578213772547 -0.07698561142398899; 0.017380191908672054 0.0029156421680470324 -0.03622633828469289; 0.018619196428494182 0.0024036497249933435 -0.042932629889142336; 0.011591860742585933 0.002338624513717791 -0.025498850631466577; 0.006300537477842123 0.0004770962060025901 -0.015924751371575636; 0.0007310148125748527 0.00011876874275950603 -0.0018010948963946957; 0.0001685514179077583 1.55772360221413e-5 -0.00043637371714516464; 0.0002602241931152784 0.00041512466315154453 -0.0008310412495031744; 2.071186016179029e-5 1.4611873249656138e-5 -0.0007025169866656767; 9.856460343198091e-5 1.8315755879970256e-5 -5.9476099538126965e-5; 0.00013801319001896344 3.433702957063582e-5 -0.0003330036139408814; 9.038295300845805e-5 -1.8528597509653974e-5 -0.00029044201734187703; 3.978532255942627e-5 1.810182073146501e-5 -0.0006190971040692845; 4.317397652167491e-5 1.8294993500181508e-5 -9.451130979967783e-5; 3.697001925225701e-6 -3.6846522391306745e-5 -0.0003047174252944887; 3.938632224460381e-6 3.285567300741441e-6 0.0002764502183228792] %
Mass Used: 65.97388383513498 kg
Launch C3: 123.36096320618475 km²/s²
||V∞_in||: 0.003810357815918844 km/s