23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.7748330662878514---------------------------
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Spacecraft: mySat
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dry_mass: 200.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.00025 kN
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num_thrusters: 1
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duty_cycle: 1.0
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Launch Mass: 3500.0 kg
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Launch Date: 2023-04-24T13:58:00.709
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Launch V∞: [5.147203335648341, -8.55703438845335, -1.3989752951331347] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.0034143572641559417, -0.002112379057881663, 0.001966984945183975] km/s
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V∞_out: [-0.00262239717744685, 0.0030185398528519277, -0.0019994900767724504] km/s
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time of flight: 1.2530565323584826e8 seconds
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arrival date: 2027-04-13T21:05:33.709
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thrust profile: [0.5097329571885071 -0.3322910490900801 -0.2924882469079728; 0.16128118148984802 0.01110303139917472 -0.2326631418620665; 0.12467286286963243 0.04289469370089566 -0.25849419758611136; 0.07504501108298083 0.04816003765547745 -0.2237257566615222; 0.05390449986720992 0.031108135571247496 -0.1469894043614276; 0.13671176678469926 -0.04769264015729386 -0.22151940845050133; -0.004594636039590046 0.06039024156161144 -0.22336184222254563; 0.048928374835719574 -0.09031000005660203 -0.024597670005029965; -0.01028291515715745 -0.09215958050146772 0.006092576110411391; 0.10412214976959078 0.10074765295491794 0.08306083968740373; -0.08961507169557466 -0.10771528933079508 0.06158654248113635; 0.0034051795740968147 -0.0416788074079853 0.10786902856705305; 0.03747624555677051 -0.06534117202919283 0.036090631094643916; -0.023293328539404946 -0.2281006842726546 0.07224282627473637; 0.14999682227701147 -0.2368658678515012 -0.02412199861247894; -0.5419574045149439 0.5827644109199104 -0.1164539802453482; 0.05171084657264916 0.21649298193619634 -0.0626883091448601; 0.18299713889497177 -0.07955974015787463 -0.06562797141667195; 0.35912605944575887 0.13763657714313646 -0.6933253770889276; 0.3774402444024937 -0.20757774585654276 -0.682777643099127] %
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Mass Used: 310.87549311872 kg
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Launch C3: 101.67367158007544 km²/s²
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||V∞_in||: 0.00447090713234483 km/s
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