23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5887182296621868---------------------------
|
|
|
|
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: 2023-05-12T17:27:16.256
|
|
Launch V∞: [6.255955503892355, -8.07530697763814, -0.2822732349176518] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.0008846803979823591, -0.0010542946613089814, -0.0009071451573117381] km/s
|
|
V∞_out: [0.0010899081207049997, 0.0005419861246243071, -0.001112794826389207] km/s
|
|
time of flight: 1.8746150361263677e8 seconds
|
|
arrival date: 2029-04-20T10:05:39.256
|
|
thrust profile: [0.17419080598013437 -0.08941916475078808 -0.09308596956897426; 0.008770931655852557 -0.0038199555839672247 -0.017283862738088733; 0.023005141556845535 -0.01816729418065593 -0.08114904018591944; 0.029452663855245788 -0.033292570308648954 -0.140987320855788; 0.023315303742795897 -0.031793843060566374 -0.13155558012980836; 0.02032418470183216 -0.03112912423534157 -0.12683015817092128; 0.019226744655813817 -0.0319039103822194 -0.12784162165905152; 0.008918295056795368 -0.012430807656490054 -0.058899348118119726; 0.00533624661774494 -0.006245615087063564 -0.035682610584309035; 0.00280836000663635 -0.003107237436028278 -0.018906761724127686; 0.0010720066958530687 -0.001482513894675018 -0.007401029368018728; 0.0006271583631380213 -0.000720361270954579 -0.002859328808928264; -0.0010695060006075219 -0.005016393100224828 0.0008700619833848476; 0.00020112080208066645 0.001570077616255957 -0.00038918043093766645; 0.0003498722508136566 0.0018728407510114479 -0.00022060182806565057; 0.0033794035573170055 0.007315058113564917 -0.0027693306730730673; -0.0029490650645706933 0.006788747981049089 -0.00032408698285445214; -4.388198840299748e-5 -0.0011714621200090392 -0.00016482531189169905; -0.00038058288008744365 -0.004521895348625492 -0.005499753543580395; 0.0006243974527007343 -0.002919790043643994 -0.006160077014874602] %
|
|
|
|
Mass Used: 77.67903327049953 kg
|
|
Launch C3: 104.42724022892315 km²/s²
|
|
||V∞_in||: 0.0016483655467987017 km/s
|