Spanier

Can you please add support for those radial tanks, so you can storage normal fuels inside and not just monopropellant.

Could you please fix undetached fairings sticking to the ejected payload with the new fairingbase so you can shield your own engine-clusters without splitting the interstage or hide smaller engines inside the fairing.

I mean that the main attachment point of the fairing base is directly on the base, so you need a extra decoupler to remove the stage, the upper limit is free adjustable, and can snap to different parts, but doesn't separate them.

I love the new inline fairings, but could you please add an addapter that doesn't contain a decoupler, so i can shield one half of my craft like the Orion ship?

Is the tank height contiously adjustable or are you planning to add a screen of 25 cm to it, and if you do so it would be awesome if you could do a joint-venture with Editor Extensions, so 1° = 1 cm 5° = 5 cm 15° = 25 cm 30° = 50 cm 45° = 75 cm 90° = 100 cm And what about procedural SRB's and a joint-venture with Advanced SRB (Adjusting the height does increase the thrust and mass, but not burntime)

I had this "bug" recently in 0.9 prerelease, can I fix it myself:

WTF just happened?

This thread will contain calculations of a program called KSPTOT by Arrowstar. These calculations include various flybys in purpose of gravity assits or free-return-trajectories to shorten mission times, get a closer view on another planet or simply to save fuel. This post will be completed over time. All initial orbits from Kerbin are: Semi-major Axis = 675 km Eccentricity = 0 Inclination = 0 deg Right Ascension of AN = 0 deg Argument of Periapse = 0.000 deg For some launch-windows adapted initial orbits are necessary. Eve Free-Return-Trajectories [tr] [td]Kerbin Departure Date = Year 1, Day 106 08:52:38.630 (9103958.630 sec UT) Eve Arrival Date = Year 1, Day 164 00:52:04.151 (14086324.151 sec UT) Kerbin Arrival Date = Year 1, Day 221 03:47:25.444 (19021645.444 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1017.612 km Eccentricity = 1.6633 Inclination = 3.158 deg Right Ascension of AN = 26.212 deg Argument of Periapse = 360.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -2989.106 km Eccentricity = 1.2665 Inclination = 156.553 deg Right Ascension of AN = 22.780 deg Argument of Periapse = 193.061 deg Periapse Radius = 796.710 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.454 km/s Prograde Delta-V = 1439.865 m/s Orbit Normal Delta-V = 205.662 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 26.212 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 143 20:58:54.225 (12344334.225 sec UT) Eve Arrival Date = Year 1, Day 193 15:47:52.162 (16645672.162 sec UT) Kerbin Arrival Date = Year 1, Day 287 23:10:10.728 (24793810.728 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -4223.864 km Eccentricity = 1.1598 Inclination = 17.280 deg Right Ascension of AN = 243.891 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -2966.519 km Eccentricity = 2.211 Inclination = 17.815 deg Right Ascension of AN = 113.966 deg Argument of Periapse = 22.825 deg Periapse Radius = 3592.329 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.359 km/s Prograde Delta-V = 922.473 m/s Orbit Normal Delta-V = -998.549 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 63.891 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 257 04:42:03.534 (22135323.534 sec UT) Eve Arrival Date = Year 1, Day 325 22:34:45.806 (28074885.806 sec UT) Kerbin Arrival Date = Year 1, Day 359 16:39:40.811 (30991180.811 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -732.230 km Eccentricity = 1.9218 Inclination = 3.918 deg Right Ascension of AN = 10.206 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -2822.037 km Eccentricity = 1.2825 Inclination = 151.983 deg Right Ascension of AN = 351.758 deg Argument of Periapse = 1.651 deg Periapse Radius = 797.299 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.635 km/s Prograde Delta-V = 1613.375 m/s Orbit Normal Delta-V = -267.151 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 190.206 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 307 19:22:34.443 (26508154.443 sec UT) Eve Arrival Date = Year 1, Day 353 20:52:19.168 (30487939.168 sec UT) Kerbin Arrival Date = Year 2, Day 74 21:17:58.814 (37919878.814 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 71.000 deg Right Ascension of AN = 254.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -2976.073 km Eccentricity = 1.2268 Inclination = 70.745 deg Right Ascension of AN = 254.030 deg Argument of Periapse = 353.596 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -3590.165 km Eccentricity = 2.4658 Inclination = 80.417 deg Right Ascension of AN = 51.214 deg Argument of Periapse = 238.382 deg Periapse Radius = 5262.612 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.126 km/s Prograde Delta-V = 1125.916 m/s Orbit Normal Delta-V = -15.262 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 353.606 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 109 07:11:04.410 (40893064.410 sec UT) Eve Arrival Date = Year 2, Day 155 09:41:00.664 (44876460.664 sec UT) Kerbin Arrival Date = Year 2, Day 238 10:18:04.874 (52049884.874 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 79.000 deg Right Ascension of AN = 77.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3245.421 km Eccentricity = 1.208 Inclination = 78.977 deg Right Ascension of AN = 76.918 deg Argument of Periapse = 73.875 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -3618.619 km Eccentricity = 2.5547 Inclination = 99.967 deg Right Ascension of AN = 64.496 deg Argument of Periapse = 55.994 deg Periapse Radius = 5625.975 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.112 km/s Prograde Delta-V = 1111.490 m/s Orbit Normal Delta-V = -4.955 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 73.860 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 227 19:09:23.269 (51131363.269 sec UT) Eve Arrival Date = Year 2, Day 299 17:42:14.931 (57346934.931 sec UT) Kerbin Arrival Date = Year 2, Day 333 21:13:24.764 (60297204.764 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -659.965 km Eccentricity = 2.0228 Inclination = 10.041 deg Right Ascension of AN = 247.210 deg Argument of Periapse = 360.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -3636.442 km Eccentricity = 1.3462 Inclination = 175.581 deg Right Ascension of AN = 220.658 deg Argument of Periapse = 170.865 deg Periapse Radius = 1258.824 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.770 km/s Prograde Delta-V = 1628.566 m/s Orbit Normal Delta-V = 693.358 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 247.210 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 278 18:04:17.056 (55533857.056 sec UT) Eve Arrival Date = Year 2, Day 323 06:57:51.329 (59381871.329 sec UT) Kerbin Arrival Date = Year 3, Day 39 05:21:09.569 (66374469.569 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 67.000 deg Right Ascension of AN = 321.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3140.434 km Eccentricity = 1.2149 Inclination = 67.626 deg Right Ascension of AN = 320.993 deg Argument of Periapse = 359.373 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -3749.518 km Eccentricity = 2.4268 Inclination = 118.072 deg Right Ascension of AN = 78.346 deg Argument of Periapse = 227.924 deg Periapse Radius = 5349.760 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.117 km/s Prograde Delta-V = 1116.637 m/s Orbit Normal Delta-V = 37.213 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 359.370 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 92 14:24:24.815 (70986264.815 sec UT) Eve Arrival Date = Year 3, Day 141 20:49:03.556 (75242943.556 sec UT) Kerbin Arrival Date = Year 3, Day 234 16:55:57.817 (83264157.817 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 51.000 deg Right Ascension of AN = 195.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3584.246 km Eccentricity = 1.1883 Inclination = 51.691 deg Right Ascension of AN = 195.001 deg Argument of Periapse = 0.094 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -3201.839 km Eccentricity = 2.2221 Inclination = 26.200 deg Right Ascension of AN = 20.496 deg Argument of Periapse = 242.429 deg Periapse Radius = 3913.016 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.097 km/s Prograde Delta-V = 1096.081 m/s Orbit Normal Delta-V = 40.792 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.095 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Duna Free-Return-Trajectories [tr] [td]Kerbin Departure Date = Year 1, Day 11 06:21:42.579 (886902.579 sec UT) Duna Arrival Date = Year 1, Day 87 20:10:22.573 (7503022.573 sec UT) Kerbin Arrival Date = Year 1, Day 164 07:55:28.024 (14111728.024 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -497.868 km Eccentricity = 2.3558 Inclination = 0.109 deg Right Ascension of AN = 276.183 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -132.734 km Eccentricity = 3.7231 Inclination = 179.675 deg Right Ascension of AN = 317.194 deg Argument of Periapse = 200.423 deg Periapse Radius = 361.450 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.903 km/s Prograde Delta-V = 1902.797 m/s Orbit Normal Delta-V = 7.997 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 276.183 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 236 04:29:17.497 (20320157.497 sec UT) Duna Arrival Date = Year 1, Day 312 20:06:29.882 (26942789.882 sec UT) Kerbin Arrival Date = Year 2, Day 24 03:40:19.995 (33536419.995 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -416.479 km Eccentricity = 2.6207 Inclination = 0.079 deg Right Ascension of AN = 142.329 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -132.925 km Eccentricity = 3.7192 Inclination = 179.672 deg Right Ascension of AN = 313.102 deg Argument of Periapse = 162.837 deg Periapse Radius = 361.447 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 2.065 km/s Prograde Delta-V = 2065.070 m/s Orbit Normal Delta-V = -5.985 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 322.329 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 324 10:41:38.543 (59481698.543 sec UT) Duna Arrival Date = Year 3, Day 36 19:56:56.815 (66167816.815 sec UT) Kerbin Arrival Date = Year 3, Day 116 10:11:54.489 (73044714.489 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -262.556 km Eccentricity = 3.5709 Inclination = 0.133 deg Right Ascension of AN = 243.344 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -131.644 km Eccentricity = 3.7456 Inclination = 179.829 deg Right Ascension of AN = 286.004 deg Argument of Periapse = 42.003 deg Periapse Radius = 361.448 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 2.603 km/s Prograde Delta-V = 2602.911 m/s Orbit Normal Delta-V = -11.367 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 63.344 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 186 17:38:42.174 (79119522.174 sec UT) Duna Arrival Date = Year 3, Day 265 14:27:22.408 (85933642.408 sec UT) Kerbin Arrival Date = Year 3, Day 344 20:38:26.740 (92781506.740 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -251.803 km Eccentricity = 3.6807 Inclination = 0.032 deg Right Ascension of AN = 291.285 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -137.119 km Eccentricity = 3.636 Inclination = 179.707 deg Right Ascension of AN = 303.968 deg Argument of Periapse = 4.183 deg Periapse Radius = 361.447 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 2.661 km/s Prograde Delta-V = 2661.303 m/s Orbit Normal Delta-V = -2.772 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 111.285 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Duna Powered Flybys [tr] [td]Kerbin Departure Date = Year 1, Day 54 04:23:34.618 (4595014.618 sec UT) Duna Arrival Date = Year 1, Day 116 04:29:46.147 (9952186.147 sec UT) Kerbin Arrival Date = Year 1, Day 189 18:52:29.797 (16311149.797 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -4271.608 km Eccentricity = 1.158 Inclination = 2.617 deg Right Ascension of AN = 318.469 deg Argument of Periapse = 0.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -286.099 km Eccentricity = 2.2635 Inclination = 178.230 deg Right Ascension of AN = 63.515 deg Argument of Periapse = 255.160 deg Periapse Radius = 361.483 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -70.810 km Eccentricity = 6.105 Inclination = 178.230 deg Right Ascension of AN = 63.515 deg Argument of Periapse = 255.160 deg Periapse Radius = 361.483 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.080 km/s Prograde Delta-V = 1069.313 m/s Orbit Normal Delta-V = 153.398 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 318.469 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 0.784 km/s Prograde Delta-V = 784.323 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 282 20:18:16.262 (24351496.262 sec UT) Duna Arrival Date = Year 1, Day 347 03:53:05.682 (29908385.682 sec UT) Kerbin Arrival Date = Year 2, Day 56 07:37:53.800 (36315473.800 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -2914.060 km Eccentricity = 1.2316 Inclination = 5.868 deg Right Ascension of AN = 28.855 deg Argument of Periapse = 360.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -348.594 km Eccentricity = 2.0373 Inclination = 175.677 deg Right Ascension of AN = 125.793 deg Argument of Periapse = 261.972 deg Periapse Radius = 361.581 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -65.640 km Eccentricity = 6.5085 Inclination = 175.677 deg Right Ascension of AN = 125.793 deg Argument of Periapse = 261.972 deg Periapse Radius = 361.581 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.165 km/s Prograde Delta-V = 1111.742 m/s Orbit Normal Delta-V = 349.351 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 28.855 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 0.911 km/s Prograde Delta-V = 910.560 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 149 03:13:41.489 (44334821.489 sec UT) Duna Arrival Date = Year 2, Day 218 03:56:58.628 (50299018.628 sec UT) Kerbin Arrival Date = Year 2, Day 288 13:34:14.396 (56381654.396 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3068.459 km Eccentricity = 1.22 Inclination = 3.070 deg Right Ascension of AN = 75.669 deg Argument of Periapse = 0.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -430.166 km Eccentricity = 1.8403 Inclination = 178.317 deg Right Ascension of AN = 191.796 deg Argument of Periapse = 268.990 deg Periapse Radius = 361.469 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -54.545 km Eccentricity = 7.627 Inclination = 178.317 deg Right Ascension of AN = 191.796 deg Argument of Periapse = 268.990 deg Periapse Radius = 361.469 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.131 km/s Prograde Delta-V = 1115.823 m/s Orbit Normal Delta-V = 182.505 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 75.669 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 1.143 km/s Prograde Delta-V = 1143.044 m/s Orbit Normal Delta-V = 0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 10 15:02:36.560 (63903756.560 sec UT) Duna Arrival Date = Year 3, Day 84 12:42:35.601 (70288955.601 sec UT) Kerbin Arrival Date = Year 3, Day 151 13:18:51.687 (76079931.687 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3326.773 km Eccentricity = 1.2029 Inclination = 4.297 deg Right Ascension of AN = 291.886 deg Argument of Periapse = 180.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -424.315 km Eccentricity = 1.8518 Inclination = 176.579 deg Right Ascension of AN = 54.381 deg Argument of Periapse = 80.590 deg Periapse Radius = 361.447 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -49.977 km Eccentricity = 8.2322 Inclination = 176.579 deg Right Ascension of AN = 54.381 deg Argument of Periapse = 80.590 deg Periapse Radius = 361.447 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.127 km/s Prograde Delta-V = 1098.034 m/s Orbit Normal Delta-V = -254.361 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 111.886 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 1.232 km/s Prograde Delta-V = 1232.437 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 233 00:10:30.042 (83117430.042 sec UT) Duna Arrival Date = Year 3, Day 310 05:51:22.356 (89790682.356 sec UT) Kerbin Arrival Date = Year 4, Day 10 22:37:48.840 (95467068.840 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3489.739 km Eccentricity = 1.1934 Inclination = 9.584 deg Right Ascension of AN = 151.188 deg Argument of Periapse = 360.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -375.375 km Eccentricity = 1.9629 Inclination = 174.201 deg Right Ascension of AN = 279.667 deg Argument of Periapse = 263.135 deg Periapse Radius = 361.447 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -52.192 km Eccentricity = 7.9253 Inclination = 174.201 deg Right Ascension of AN = 279.667 deg Argument of Periapse = 263.135 deg Periapse Radius = 361.447 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.195 km/s Prograde Delta-V = 1052.983 m/s Orbit Normal Delta-V = 564.025 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 151.188 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 1.156 km/s Prograde Delta-V = 1156.197 m/s Orbit Normal Delta-V = 0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Eve Assisted Moho Encounter [tr] [td]Kerbin Departure Date = Year 1, Day 2 02:50:43.279 (96643.279 sec UT) Eve Arrival Date = Year 1, Day 46 13:28:00.668 (3936480.668 sec UT) Moho Arrival Date = Year 1, Day 78 02:32:37.610 (6661957.610 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1304.095 km Eccentricity = 1.5176 Inclination = 12.748 deg Right Ascension of AN = 118.390 deg Argument of Periapse = 180.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -794.166 km Eccentricity = 2.005 Inclination = 166.053 deg Right Ascension of AN = 86.375 deg Argument of Periapse = 302.248 deg Periapse Radius = 798.104 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -687.377 km Eccentricity = 2.1611 Inclination = 166.053 deg Right Ascension of AN = 86.375 deg Argument of Periapse = 302.248 deg Periapse Radius = 798.104 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 1.831 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.487 km/s Prograde Delta-V = 1252.516 m/s Orbit Normal Delta-V = -800.868 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 298.390 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.142 km/s Prograde Delta-V = 142.273 m/s Orbit Normal Delta-V = 0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 34 20:57:58.173 (2926678.173 sec UT) Eve Arrival Date = Year 1, Day 74 21:48:55.387 (6385735.387 sec UT) Moho Arrival Date = Year 1, Day 118 10:52:13.511 (10147933.511 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -483.950 km Eccentricity = 2.3948 Inclination = 4.976 deg Right Ascension of AN = 84.576 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -273.323 km Eccentricity = 9.8462 Inclination = 108.030 deg Right Ascension of AN = 40.392 deg Argument of Periapse = 92.341 deg Periapse Radius = 2417.883 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 2.524 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.946 km/s Prograde Delta-V = 1911.191 m/s Orbit Normal Delta-V = 365.584 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 84.576 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 110 02:24:43.064 (9426283.064 sec UT) Eve Arrival Date = Year 1, Day 154 17:56:07.900 (13283767.900 sec UT) Moho Arrival Date = Year 1, Day 172 22:52:36.587 (14856756.587 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -465.836 km Eccentricity = 2.449 Inclination = 7.221 deg Right Ascension of AN = 224.248 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -596.026 km Eccentricity = 2.3367 Inclination = 29.659 deg Right Ascension of AN = 323.355 deg Argument of Periapse = 109.954 deg Periapse Radius = 796.709 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 3.393 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 2.000 km/s Prograde Delta-V = 1926.914 m/s Orbit Normal Delta-V = -533.982 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 44.248 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 124 20:22:47.748 (10700567.748 sec UT) Eve Arrival Date = Year 1, Day 177 07:46:03.260 (15234363.260 sec UT) Moho Arrival Date = Year 1, Day 207 14:21:14.804 (17850074.804 sec UT)[/td] [td]Parking Orbit from Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 52.00 deg Right Ascension of AN = 222.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -2092.441 km Eccentricity = 1.3226 Inclination = 52.142 deg Right Ascension of AN = 222.005 deg Argument of Periapse = 181.454 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -6683.277 km Eccentricity = 1.1192 Inclination = 116.847 deg Right Ascension of AN = 207.749 deg Argument of Periapse = 15.816 deg Periapse Radius = 796.709 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -1781.556 km Eccentricity = 1.4472 Inclination = 116.847 deg Right Ascension of AN = 207.749 deg Argument of Periapse = 15.816 deg Periapse Radius = 796.709 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 2.922 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.199 km/s Prograde Delta-V = 1198.574 m/s Orbit Normal Delta-V = -8.655 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 181.457 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.348 km/s Prograde Delta-V = 347.812 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 168 17:34:45.909 (14492085.909 sec UT) Eve Arrival Date = Year 1, Day 216 20:49:29.781 (18650969.781 sec UT) Moho Arrival Date = Year 1, Day 250 23:10:00.097 (21597000.097 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1533.564 km Eccentricity = 1.4402 Inclination = 14.635 deg Right Ascension of AN = 160.781 deg Argument of Periapse = 360.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -724.729 km Eccentricity = 3.2993 Inclination = 152.670 deg Right Ascension of AN = 124.886 deg Argument of Periapse = 115.125 deg Periapse Radius = 1666.344 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 2.549 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.478 km/s Prograde Delta-V = 1169.792 m/s Orbit Normal Delta-V = 902.771 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 160.781 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 1, Day 306 05:30:38.301 (26371838.301 sec UT) Eve Arrival Date = Year 1, Day 354 05:44:35.897 (30519875.897 sec UT) Moho Arrival Date = Year 2, Day 15 18:57:35.051 (32813855.051 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 31.000 deg Right Ascension of AN = 356.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3631.083 km Eccentricity = 1.1859 Inclination = 30.912 deg Right Ascension of AN = 356.939 deg Argument of Periapse = 279.897 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -4727.481 km Eccentricity = 1.1906 Inclination = 116.402 deg Right Ascension of AN = 243.869 deg Argument of Periapse = 198.339 deg Periapse Radius = 900.976 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -1832.237 km Eccentricity = 1.4917 Inclination = 116.402 deg Right Ascension of AN = 243.869 deg Argument of Periapse = 198.339 deg Periapse Radius = 900.976 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 2.849 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.095 km/s Prograde Delta-V = 1094.324 m/s Orbit Normal Delta-V = -28.983 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 280.702 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.297 km/s Prograde Delta-V = 296.529 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 136 10:28:31.292 (43237711.292 sec UT) Eve Arrival Date = Year 2, Day 185 09:00:08.623 (47466008.623 sec UT) Moho Arrival Date = Year 2, Day 222 03:43:43.832 (50643823.832 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -2027.801 km Eccentricity = 1.3329 Inclination = 12.725 deg Right Ascension of AN = 201.230 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -975.389 km Eccentricity = 3.5681 Inclination = 162.937 deg Right Ascension of AN = 184.312 deg Argument of Periapse = 134.852 deg Periapse Radius = 2504.936 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 3.151 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.359 km/s Prograde Delta-V = 1120.480 m/s Orbit Normal Delta-V = 769.574 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 201.230 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 260 17:54:21.169 (53978061.169 sec UT) Eve Arrival Date = Year 2, Day 322 08:20:30.827 (59300430.827 sec UT) Moho Arrival Date = Year 2, Day 351 10:22:56.518 (61813376.518 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1538.793 km Eccentricity = 1.4387 Inclination = 2.462 deg Right Ascension of AN = 329.323 deg Argument of Periapse = 0.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -5961.956 km Eccentricity = 1.1336 Inclination = 138.538 deg Right Ascension of AN = 277.339 deg Argument of Periapse = 186.418 deg Periapse Radius = 796.712 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -2625.722 km Eccentricity = 1.3034 Inclination = 138.538 deg Right Ascension of AN = 277.339 deg Argument of Periapse = 186.418 deg Periapse Radius = 796.712 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 3.227 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.290 km/s Prograde Delta-V = 1281.328 m/s Orbit Normal Delta-V = 153.414 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 329.323 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.183 km/s Prograde Delta-V = 182.576 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 319 15:46:32.068 (59067992.068 sec UT) Eve Arrival Date = Year 3, Day 1 11:18:22.760 (63112702.760 sec UT) Moho Arrival Date = Year 3, Day 28 18:03:09.111 (65469789.111 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1285.261 km Eccentricity = 1.5252 Inclination = 10.669 deg Right Ascension of AN = 103.367 deg Argument of Periapse = 0.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -613.351 km Eccentricity = 2.8627 Inclination = 162.328 deg Right Ascension of AN = 55.886 deg Argument of Periapse = 101.458 deg Periapse Radius = 1142.461 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -725.539 km Eccentricity = 2.5746 Inclination = 162.328 deg Right Ascension of AN = 55.886 deg Argument of Periapse = 101.458 deg Periapse Radius = 1142.461 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 1.932 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.450 km/s Prograde Delta-V = 1284.613 m/s Orbit Normal Delta-V = 672.907 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 103.367 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.200 km/s Prograde Delta-V = -199.761 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 287 00:11:19.869 (87783079.869 sec UT) Eve Arrival Date = Year 3, Day 335 13:53:33.135 (91979613.135 sec UT) Moho Arrival Date = Year 3, Day 365 10:26:56.092 (94559216.092 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 16.000 deg Right Ascension of AN = 148.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1615.103 km Eccentricity = 1.4179 Inclination = 15.706 deg Right Ascension of AN = 148.014 deg Argument of Periapse = 359.244 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -767.342 km Eccentricity = 2.5689 Inclination = 153.804 deg Right Ascension of AN = 108.717 deg Argument of Periapse = 117.276 deg Periapse Radius = 1203.901 km --------------------------------------------- Inbound Hyperbolic Orbit to Moho --------------------------------------------- Hyperbolic Excess Vel. = 2.093 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.269 km/s Prograde Delta-V = 1269.366 m/s Orbit Normal Delta-V = -18.248 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 359.257 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Eve Assited Duna Encounter [tr] [td]Kerbin Departure Date = Year 1, Day 169 18:11:07.998 (14580667.998 sec UT) Eve Arrival Date = Year 1, Day 217 05:42:39.505 (18682959.505 sec UT) Duna Arrival Date = Year 1, Day 270 10:45:28.710 (23280328.710 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1509.914 km Eccentricity = 1.447 Inclination = 14.264 deg Right Ascension of AN = 160.835 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -716.257 km Eccentricity = 4.5235 Inclination = 17.375 deg Right Ascension of AN = 107.872 deg Argument of Periapse = 115.576 deg Periapse Radius = 2523.712 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 1.814 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.473 km/s Prograde Delta-V = 1180.445 m/s Orbit Normal Delta-V = 881.641 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 160.835 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 113 21:35:33.513 (41290533.513 sec UT) Eve Arrival Date = Year 2, Day 143 21:39:08.666 (43882748.666 sec UT) Duna Arrival Date = Year 2, Day 232 16:39:30.431 (51554370.431 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 27.000 deg Right Ascension of AN = 127.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -2690.014 km Eccentricity = 1.2509 Inclination = 26.426 deg Right Ascension of AN = 127.063 deg Argument of Periapse = 357.158 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -1512.827 km Eccentricity = 1.5282 Inclination = 146.584 deg Right Ascension of AN = 106.761 deg Argument of Periapse = 141.619 deg Periapse Radius = 799.011 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.145 km/s Prograde Delta-V = 1144.213 m/s Orbit Normal Delta-V = -34.414 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 357.214 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 2, Day 283 06:53:35.291 (55925615.291 sec UT) Eve Arrival Date = Year 2, Day 334 20:27:34.796 (60380854.796 sec UT) Duna Arrival Date = Year 3, Day 23 17:41:09.075 (65036469.075 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 43.000 deg Right Ascension of AN = 163.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -3453.009 km Eccentricity = 1.1955 Inclination = 42.733 deg Right Ascension of AN = 162.987 deg Argument of Periapse = 181.970 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -4725.634 km Eccentricity = 2.3763 Inclination = 28.614 deg Right Ascension of AN = 97.406 deg Argument of Periapse = 310.332 deg Periapse Radius = 6503.690 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -1984.586 km Eccentricity = 4.2771 Inclination = 28.614 deg Right Ascension of AN = 97.406 deg Argument of Periapse = 310.332 deg Periapse Radius = 6503.690 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.102 km/s Prograde Delta-V = 1101.819 m/s Orbit Normal Delta-V = 15.782 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 181.960 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.515 km/s Prograde Delta-V = 515.329 m/s Orbit Normal Delta-V = 0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Kerbin Departure Date = Year 3, Day 125 00:55:47.401 (73788947.401 sec UT) Eve Arrival Date = Year 3, Day 171 12:15:49.074 (77804149.074 sec UT) Duna Arrival Date = Year 3, Day 218 12:06:27.257 (81864387.257 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 12.000 deg Right Ascension of AN = 141.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -1209.519 km Eccentricity = 1.5581 Inclination = 12.452 deg Right Ascension of AN = 140.993 deg Argument of Periapse = 179.809 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -650.485 km Eccentricity = 4.3932 Inclination = 11.356 deg Right Ascension of AN = 94.529 deg Argument of Periapse = 288.864 deg Periapse Radius = 2207.215 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.371 km/s Prograde Delta-V = 1370.922 m/s Orbit Normal Delta-V = -28.888 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 179.802 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Moho-Eve-Kerbin-Duna Tour [tr] [td]Moho Departure Date = Year 1, Day 241 14:38:42.949 (20788722.949 sec UT) Eve Arrival Date = Year 1, Day 276 12:16:24.806 (23804184.806 sec UT) Kerbin Arrival Date = Year 1, Day 312 02:39:30.670 (26879970.670 sec UT) Duna Arrival Date = Year 1, Day 362 11:24:02.719 (31231442.719 sec UT)[/td] [td]Parking Orbit around Moho --------------------------------------------- Semi-major Axis = 275.000km Eccentricity = 0.000 Inclination = 0.000 deg Right Ascension of AN = 0.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Moho --------------------------------------------- Semi-major Axis = -38.913 km Eccentricity = 8.067 Inclination = 3.891 deg Right Ascension of AN = 19.328 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -480.945 km Eccentricity = 3.5238 Inclination = 148.603 deg Right Ascension of AN = 101.758 deg Argument of Periapse = 265.404 deg Periapse Radius = 1213.794 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -424.844 km Eccentricity = 2.9649 Inclination = 9.617 deg Right Ascension of AN = 155.755 deg Argument of Periapse = 251.356 deg Periapse Radius = 834.769 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 1.309 km/s[/td] [td]Burn Information to Depart Moho --------------------------------------------- Total Delta-V = 1.577 km/s Prograde Delta-V = 1569.344 m/s Orbit Normal Delta-V = 159.989 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 19.328 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Moho Departure Date = Year 2, Day 254 14:16:51.765 (53446611.765 sec UT) Eve Arrival Date = Year 2, Day 287 16:40:33.127 (56306433.127 sec UT) Kerbin Arrival Date = Year 2, Day 357 04:59:31.791 (62312371.791 sec UT) Duna Arrival Date = Year 3, Day 81 10:43:48.861 (70022628.861 sec UT)[/td] [td]Parking Orbit around Moho --------------------------------------------- Semi-major Axis = 275.000 km Eccentricity = 0.0000 Inclination = 30.000 deg Right Ascension of AN = 300.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Moho --------------------------------------------- Semi-major Axis = -16.261 km Eccentricity = 17.9117 Inclination = 30.252 deg Right Ascension of AN = 299.995 deg Argument of Periapse = 359.395 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -1725.037 km Eccentricity = 1.7858 Inclination = 158.688 deg Right Ascension of AN = 2.525 deg Argument of Periapse = 264.502 deg Periapse Radius = 1355.561 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -946.214 km Eccentricity = 2.4652 Inclination = 176.368 deg Right Ascension of AN = 72.572 deg Argument of Periapse = 64.540 deg Periapse Radius = 1386.379 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 0.877 km/s[/td] [td]Burn Information to Depart Moho --------------------------------------------- Total Delta-V = 2.622 km/s Prograde Delta-V = 2622.124 m/s Orbit Normal Delta-V = 14.981 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 359.390 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Moho Departure Date = Year 3, Day 224 05:02:55.559 (82357375.559 sec UT) Eve Arrival Date = Year 3, Day 253 10:55:39.442 (84884139.442 sec UT) Kerbin Arrival Date = Year 3, Day 290 17:49:34.374 (88105774.374 sec UT) Duna Arrival Date = Year 4, Day 66 13:04:58.215 (100271098.215 sec UT)[/td] [td]Parking Orbit around Moho --------------------------------------------- Semi-major Axis = 275.000km Eccentricity = 0.000 Inclination = 31.000 deg Right Ascension of AN = 330.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Moho --------------------------------------------- Semi-major Axis = -19.207 km Eccentricity = 15.3175 Inclination = 32.897 deg Right Ascension of AN = 329.887 deg Argument of Periapse = 358.239 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -1901.311 km Eccentricity = 1.4155 Inclination = 158.526 deg Right Ascension of AN = 26.034 deg Argument of Periapse = 259.913 deg Periapse Radius = 790.000 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -2124.108 km Eccentricity = 1.3719 Inclination = 158.526 deg Right Ascension of AN = 26.034 deg Argument of Periapse = 259.913 deg Periapse Radius = 790.000 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -1264.652 km Eccentricity = 1.5298 Inclination = 0.934 deg Right Ascension of AN = 115.636 deg Argument of Periapse = 192.165 deg Periapse Radius = 670.001 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 2.779 km/s[/td] [td]Burn Information to Depart Moho --------------------------------------------- Total Delta-V = 2.381 km/s Prograde Delta-V = 2378.254 m/s Orbit Normal Delta-V = 104.735 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 358.143 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.045 km/s Prograde Delta-V = -45.299 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Moho Departure Date = Year 4, Day 32 15:14:43.547 (97341283.547 sec UT) Eve Arrival Date = Year 4, Day 64 15:36:47.419 (100107407.419 sec UT) Kerbin Arrival Date = Year 4, Day 134 15:52:04.800 (106156324.800 sec UT) Duna Arrival Date = Year 4, Day 291 23:22:04.167 (119748124.167 sec UT)[/td] [td]Parking Orbit around Moho --------------------------------------------- Semi-major Axis = 275.000km Eccentricity = 0.000 Inclination = 0.000 deg Right Ascension of AN = 0.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Moho --------------------------------------------- Semi-major Axis = -19.234 km Eccentricity = 15.2979 Inclination = 8.724 deg Right Ascension of AN = 61.707 deg Argument of Periapse = 180.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -1219.418 km Eccentricity = 2.2514 Inclination = 149.108 deg Right Ascension of AN = 74.070 deg Argument of Periapse = 67.920 deg Periapse Radius = 1526.003 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -731.674 km Eccentricity = 2.0118 Inclination = 170.742 deg Right Ascension of AN = 338.537 deg Argument of Periapse = 61.026 deg Periapse Radius = 740.279 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 2.749 km/s[/td] [td]Burn Information to Depart Moho --------------------------------------------- Total Delta-V = 2.390 km/s Prograde Delta-V = 2341.525 m/s Orbit Normal Delta-V = -479.454 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 241.707 deg[/td] [/tr] [/table][table="width: 1024, align: left"] [tr] [td]Moho Departure Date = Year 4, Day 201 04:00:44.748 (111902444.748 sec UT) Eve Arrival Date = Year 4, Day 228 22:25:27.015 (114301527.015 sec UT) Kerbin Arrival Date = Year 4, Day 294 23:43:45.558 (120008625.558 sec UT) Duna Arrival Date = Year 5, Day 18 14:12:42.515 (127663962.515 sec UT)[/td] [td]Parking Orbit around Moho --------------------------------------------- Semi-major Axis = 275.000km Eccentricity = 0.000 Inclination = 0.000 deg Right Ascension of AN = 0.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Moho --------------------------------------------- Semi-major Axis = -22.660 km Eccentricity = 13.1359 Inclination = 2.972 deg Right Ascension of AN = 177.716 deg Argument of Periapse = 180.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -486.583 km Eccentricity = 2.6236 Inclination = 169.165 deg Right Ascension of AN = 84.980 deg Argument of Periapse = 242.290 deg Periapse Radius = 790.000 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Eve --------------------------------------------- Semi-major Axis = -1283.832 km Eccentricity = 1.6153 Inclination = 169.165 deg Right Ascension of AN = 84.980 deg Argument of Periapse = 242.290 deg Periapse Radius = 790.000 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -870.359 km Eccentricity = 2.5629 Inclination = 167.743 deg Right Ascension of AN = 0.782 deg Argument of Periapse = 248.149 deg Periapse Radius = 1360.254 km --------------------------------------------- Inbound Hyperbolic Orbit to Duna --------------------------------------------- Hyperbolic Excess Vel. = 1.129 km/s[/td] [td]Burn Information to Depart Moho --------------------------------------------- Total Delta-V = 2.162 km/s Prograde Delta-V = 2157.011 m/s Orbit Normal Delta-V = -152.616 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 357.716 deg --------------------------------------------- Burn Information to Depart Eve --------------------------------------------- Total Delta-V = 0.921 km/s Prograde Delta-V = -921.005 m/s Orbit Normal Delta-V = -0.000 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Kerbin-Eve-Duna-Kerbin Tour [tr] [td]Kerbin Departure Date = Year 2, Day 74 05:11:33.417 (37861893.417 sec UT) Eve Arrival Date = Year 2, Day 129 12:15:26.284 (42639326.284 sec UT) Duna Arrival Date = Year 2, Day 186 23:17:17.272 (47603837.272 sec UT) Kerbin Arrival Date = Year 2, Day 268 12:32:02.744 (54649922.744 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -564.469 km Eccentricity = 2.1958 Inclination = 8.180 deg Right Ascension of AN = 81.688 deg Argument of Periapse = 0.000 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -973.675 km Eccentricity = 5.9303 Inclination = 161.855 deg Right Ascension of AN = 125.412 deg Argument of Periapse = 209.746 deg Periapse Radius = 4800.485 km --------------------------------------------- Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -102.951 km Eccentricity = 4.5108 Inclination = 169.024 deg Right Ascension of AN = 315.633 deg Argument of Periapse = 76.771 deg Periapse Radius = 361.447 km --------------------------------------------- Inbound Hyperbolic Orbit to Kerbin --------------------------------------------- Hyperbolic Excess Vel. = 3.886 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.854 km/s Prograde Delta-V = 1760.116 m/s Orbit Normal Delta-V = 581.779 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 81.688 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Kerbin-Duna-Eve-Kerbin Tour [tr] [td]Kerbin Departure Date = Year 1, Day 22 20:58:25.817 (1889905.817 sec UT) Duna Arrival Date = Year 1, Day 97 04:20:49.303 (8310049.303 sec UT) Eve Arrival Date = Year 1, Day 160 05:40:04.102 (13758004.102 sec UT) Kerbin Arrival Date = Year 1, Day 184 22:52:10.455 (15893530.455 sec UT)[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -766.800 km Eccentricity = 1.8803 Inclination = 0.056 deg Right Ascension of AN = 300.472 deg Argument of Periapse = 0.000 deg --------------------------------------------- Inbound Hyperbolic Flyby Orbit to Duna --------------------------------------------- Semi-major Axis = -161.019 km Eccentricity = 3.2448 Inclination = 170.687 deg Right Ascension of AN = 63.293 deg Argument of Periapse = 285.613 deg Periapse Radius = 361.450 km --------------------------------------------- Outbound Hyperbolic Flyby Orbit from Duna --------------------------------------------- Semi-major Axis = -92.849 km Eccentricity = 4.8929 Inclination = 170.687 deg Right Ascension of AN = 63.293 deg Argument of Periapse = 285.613 deg Periapse Radius = 361.450 km --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -941.717 km Eccentricity = 4.4784 Inclination = 166.290 deg Right Ascension of AN = 315.791 deg Argument of Periapse = 220.496 deg Periapse Radius = 3275.669 km --------------------------------------------- Inbound Hyperbolic Orbit to Kerbin --------------------------------------------- Hyperbolic Excess Vel. = 1.348 km/s[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.595 km/s Prograde Delta-V = 1594.604 m/s Orbit Normal Delta-V = 3.808 m/s Radial Delta-V = 0.000 m/s --------------------- Burn True Anomaly = 300.472 deg --------------------------------------------- Burn Information to Depart Duna --------------------------------------------- Total Delta-V = 0.335 km/s Prograde Delta-V = 335.332 m/s Orbit Normal Delta-V = 0.000 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 0.000 deg[/td] [/tr] [/table][table="width: 1024, align: left"] Eve + Kerbin Assited Jool Encounter [tr] [td]Kerbin Departure Date = Year 1, Day 252 06:54:23.216 (21711263.216 sec UT) Eve Arrival Date = Year 1, Day 319 13:03:31.445 (27522211.445 sec UT) Kerbin Arrival Date = Year 2, Day 133 11:06:10.385 (42980770.385 sec UT) Jool Arrival Date = Year 3, Day 71 02:10:30.174 (69127830.174 sec UT)[/td] [td]Parking Orbit around Kerbin --------------------------------------------- Semi-major Axis = 675.000 km Eccentricity = 0.0000 Inclination = 19.000 deg Right Ascension of AN = 0.000 deg Argument of Periapse = 0.000 deg[/td] [td]Hyperbolic Departure Orbit from Kerbin --------------------------------------------- Semi-major Axis = -506.159 km Eccentricity = 2.3336 Inclination = 18.496 deg Right Ascension of AN = 0.063 deg Argument of Periapse = 177.666 deg --------------------------------------------- Hyperbolic Flyby Orbit to Eve --------------------------------------------- Semi-major Axis = -1215.149 km Eccentricity = 1.6901 Inclination = 151.915 deg Right Ascension of AN = 33.750 deg Argument of Periapse = 39.255 deg Periapse Radius = 838.593 km --------------------------------------------- Hyperbolic Flyby Orbit to Kerbin --------------------------------------------- Semi-major Axis = -174.408 km Eccentricity = 5.5015 Inclination = 176.316 deg Right Ascension of AN = 302.367 deg Argument of Periapse = 347.481 deg Periapse Radius = 785.101 km[/td] [td]Burn Information to Depart Kerbin --------------------------------------------- Total Delta-V = 1.889 km/s Prograde Delta-V = 1888.755 m/s Orbit Normal Delta-V = 36.741 m/s Radial Delta-V = -0.000 m/s --------------------- Burn True Anomaly = 177.725 deg[/td] [/tr] [/table][table="width: 1024, align: left"]

The idea mining metallic hydrogen from Jupiter is hilarious, you can't reach the interior of Jupiter anyways, or did someone of you recreate the submarine from "The Core", you can barely reach the "surface" of the planet itself due to ludicrous radiation levels. The only thing you could mine from a gas giant is He3 from Saturn, but nothing else.

Assuming one could handle problems resulting of extreme pressures with moderate effort in structural improvements of storage options, what would presumably happen, when I fuel a spaceship with metallic hydrogen and red oxygen? It would give us a whole new level of engine design with extreme thrust. For all who didn't heared about these two guys: Metallic hydrogen: Hydrogen with metallic properties Red oxygen: An allotrope of solid oxygen (O8)

Why does the flyby calculator never return direct encounters with the flyby body, so the transfer orbit cycles around the sun more than once?

Can please add the new maps for the updated planets and maybe a toggleable grid?

Solving differential equations isn't a question of mods, the SAS should be able to realize the inertia of your craft and the torque it can apply to it. From that it could calculate the hysteresis the craft can be stabilized best with.

As you are going to rework the fuels a bit and add hypergolic bipropellant, could you add properties for RCS thrusters that are powered by bipropellant?

Even in real world this would be impossible, as the barycenter lies within the earth

As of now the SAS system is perfect in handling rockets, stations and probes. But it sucks in stabilizing aircrafts. A whole lot of them doesn't fly smoothly but still shake with the all known wobble, because damping mode doesn't work as it should. Instead of bringing the amplitude of oscillation down slowly, it sometimes even produces this waving movement. For example, consider the B9 YF-28 Haldeman flys extremely stable on it's own, but when you kick in SAS and try to turn it, it flys as if it had parkinson afterwards (tested with FAR). I think the algorithm to adjust the differential equations for the damping could be optimized for planes. A feature for optimizing long range atmospheric journeys the also SAS lacks is horizon orientated stabilization. As of now, a aircraft cruising above Kerbin slowly but steadily pulls up as the surface curves away beneath it. Anybody also feels like there still is some potential to put work on the SAS?

Any hint, when the new version arrives?

Some wishs for the next update: Battery Banks for S2, Mk2 and HL format and a HL tail part without a door. How about it?

On airbreathing mode it get's throttled back to 90-95% and as soon as a pump in my internal oxygen it drops to ~60%. BTW I'm using MechJeb for throttle control.

Is there a reason, the SABRE Engines from B9 are constantly overheating? They do so even when I add the precooler infront of it

Xenon is somehow bugged, you can fill 700 Xenon it the stock tank, but only 12.5 in the Oscar-B tank, that has equal size

The B9 tanks are bugged, when you add a tank, it counts it volume twice, but it's mass just once, because LH2 and LOX are implemented twice Edit: Problem solved, I extracted the real fuels folder twice

So, what other mods we get compability for 1.4? B9 and KSPX should be there definitely, and somehow allow Mechjeb to calculate dV and stagetime properly inflight, please

I think it's MechJeb

what is the proper way to use the new stacked booster?