MISSION PLAN - PDS Small Bodies Node

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Table 12-9 CIDA #2 Spacecraft Attitude [EME’2000] (cont) TFL i-LAT i-LNG j-LAT j-LNG k-LAT k-LNG (days) (deg) (deg) (deg) (deg) (deg) (deg) _______________________________________________________________ 844.000 -17.788 292.919 -71.033 91.912 6.370 20.867 845.000 -17.727 293.339 -71.034 91.798 6.527 21.243 846.000 -17.666 293.756 -71.034 91.684 6.683 21.617 847.000 -17.603 294.168 -71.034 91.569 6.837 21.988 848.000 -17.539 294.578 -71.034 91.455 6.990 22.357 849.000 -17.475 294.984 -71.034 91.340 7.142 22.723 850.000 -17.410 295.387 -71.033 91.224 7.293 23.087 851.000 -17.343 295.787 -71.033 91.109 7.443 23.449 852.000 -17.276 296.183 -71.032 90.993 7.591 23.808 853.000 -17.209 296.576 -71.031 90.876 7.739 24.164 854.000 -17.140 296.967 -71.030 90.760 7.885 24.519 855.000 -17.071 297.354 -71.029 90.643 8.030 24.871 856.000 -17.001 297.737 -71.027 90.525 8.174 25.221 857.000 -16.930 298.118 -71.026 90.408 8.316 25.568 858.000 -16.858 298.496 -71.024 90.290 8.458 25.914 859.000 -16.786 298.871 -71.022 90.172 8.599 26.257 860.000 -16.713 299.243 -71.020 90.053 8.738 26.598 861.000 -16.639 299.613 -71.018 89.934 8.877 26.937 862.000 -16.565 299.979 -71.015 89.815 9.014 27.274 863.000 -16.490 300.342 -71.012 89.695 9.151 27.609 864.000 -16.414 300.703 -71.010 89.575 9.286 27.942 865.000 -16.338 301.061 -71.007 89.454 9.421 28.273 866.000 -16.261 301.416 -71.003 89.333 9.554 28.602 867.000 -16.184 301.769 -71.000 89.212 9.686 28.929 868.000 -16.106 302.119 -70.997 89.090 9.818 29.255 869.000 -16.027 302.466 -70.993 88.968 9.948 29.578 870.000 -15.948 302.811 -70.989 88.846 10.078 29.900 871.000 -15.868 303.153 -70.985 88.723 10.207 30.219 872.000 -15.788 303.492 -70.980 88.600 10.334 30.537 873.000 -15.707 303.830 -70.976 88.476 10.461 30.853 874.000 -15.625 304.164 -70.971 88.352 10.587 31.168 875.000 -15.543 304.496 -70.966 88.227 10.712 31.480 876.000 -15.461 304.826 -70.961 88.103 10.836 31.791 877.000 -15.378 305.153 -70.956 87.977 10.959 32.101 878.000 -15.295 305.478 -70.951 87.851 11.081 32.408 879.000 -15.211 305.801 -70.945 87.725 11.203 32.714 880.000 -15.126 306.121 -70.939 87.598 11.324 33.018 881.000 -15.042 306.439 -70.933 87.471 11.443 33.321 882.000 -14.956 306.755 -70.927 87.344 11.562 33.622 883.000 -14.870 307.069 -70.921 87.215 11.681 33.922 884.000 -14.784 307.380 -70.914 87.087 11.798 34.220 885.000 -14.697 307.689 -70.907 86.958 11.915 34.517 886.000 -14.610 307.996 -70.900 86.828 12.030 34.812 887.000 -14.523 308.301 -70.893 86.698 12.146 35.105 888.000 -14.435 308.604 -70.885 86.568 12.260 35.398 889.000 -14.346 308.905 -70.878 86.437 12.373 35.688 890.000 -14.257 309.203 -70.870 86.305 12.486 35.978 891.000 -14.168 309.500 -70.862 86.173 12.598 36.266 892.000 -14.078 309.794 -70.853 86.041 12.710 36.552 893.000 -13.988 310.087 -70.845 85.908 12.820 36.837 894.000 -13.898 310.378 -70.836 85.774 12.930 37.121 895.000 -13.807 310.666 -70.827 85.640 13.039 37.403 896.000 -13.716 310.953 -70.818 85.505 13.148 37.685 897.000 -13.624 311.238 -70.808 85.370 13.256 37.964 898.000 -13.532 311.520 -70.799 85.235 13.363 38.243 899.000 -13.440 311.801 -70.789 85.098 13.469 38.520 900.000 -13.347 312.081 -70.779 84.962 13.575 38.796 901.000 -13.253 312.358 -70.768 84.824 13.681 39.071 902.000 -13.160 312.633 -70.758 84.686 13.785 39.345 903.000 -13.066 312.907 -70.747 84.548 13.889 39.617 904.000 -12.972 313.179 -70.736 84.409 13.993 39.888 905.000 -12.877 313.449 -70.724 84.269 14.095 40.158 906.000 -12.782 313.717 -70.713 84.129 14.197 40.427 907.000 -12.686 313.984 -70.701 83.988 14.299 40.695 908.000 -12.590 314.249 -70.689 83.846 14.400 40.961 909.000 -12.494 314.512 -70.676 83.704 14.500 41.227 910.000 -12.398 314.774 -70.664 83.561 14.600 41.491 911.000 -12.301 315.033 -70.651 83.418 14.700 41.754 912.000 -12.203 315.292 -70.638 83.274 14.798 42.016 913.000 -12.106 315.548 -70.624 83.130 14.896 42.277 914.000 -12.008 315.803 -70.610 82.984 14.994 42.537 152
Table 12-10 CIDA #3 Spacecraft Attitude [EME’2000] TFL i-LAT i-LNG j-LAT j-LNG k-LAT k-LNG (days) (deg) (deg) (deg) (deg) (deg) (deg) _______________________________________________________________ 1703.000 -18.287 258.778 -70.652 98.539 -6.105 350.804 1704.000 -18.362 259.509 -70.664 98.435 -5.850 351.458 1705.000 -18.434 260.233 -70.676 98.331 -5.596 352.105 1706.000 -18.501 260.951 -70.688 98.227 -5.344 352.745 1707.000 -18.564 261.662 -70.700 98.123 -5.094 353.377 1708.000 -18.623 262.367 -70.711 98.019 -4.845 354.004 1709.000 -18.679 263.065 -70.723 97.914 -4.597 354.623 1710.000 -18.731 263.758 -70.734 97.810 -4.351 355.236 1711.000 -18.779 264.443 -70.744 97.705 -4.107 355.843 1712.000 -18.823 265.123 -70.755 97.601 -3.865 356.443 1713.000 -18.864 265.796 -70.765 97.496 -3.624 357.037 1714.000 -18.901 266.464 -70.775 97.391 -3.386 357.624 1715.000 -18.936 267.125 -70.785 97.286 -3.148 358.206 1716.000 -18.966 267.780 -70.794 97.181 -2.913 358.782 1717.000 -18.994 268.429 -70.804 97.076 -2.679 359.352 1718.000 -19.019 269.072 -70.813 96.971 -2.447 359.917 1719.000 -19.040 269.710 -70.821 96.866 -2.217 0.475 1720.000 -19.058 270.341 -70.830 96.760 -1.989 1.028 1721.000 -19.074 270.967 -70.839 96.655 -1.762 1.576 1722.000 -19.087 271.587 -70.847 96.549 -1.537 2.119 1723.000 -19.097 272.201 -70.855 96.443 -1.314 2.656 1724.000 -19.104 272.810 -70.863 96.337 -1.092 3.188 1725.000 -19.108 273.413 -70.870 96.231 -0.872 3.715 1726.000 -19.110 274.010 -70.878 96.125 -0.654 4.237 1727.000 -19.110 274.603 -70.885 96.018 -0.438 4.754 1728.000 -19.107 275.189 -70.892 95.912 -0.223 5.267 1729.000 -19.101 275.771 -70.899 95.805 -0.011 5.774 1730.000 -19.094 276.347 -70.905 95.698 0.200 6.277 1731.000 -19.084 276.918 -70.912 95.591 0.410 6.776 1732.000 -19.071 277.483 -70.918 95.484 0.618 7.270 1733.000 -19.057 278.044 -70.924 95.377 0.824 7.759 1734.000 -19.040 278.599 -70.930 95.269 1.028 8.244 1735.000 -19.022 279.150 -70.935 95.161 1.231 8.725 1736.000 -19.001 279.695 -70.941 95.053 1.432 9.202 1737.000 -18.979 280.236 -70.946 94.945 1.631 9.674 1738.000 -18.954 280.771 -70.951 94.837 1.829 10.143 1739.000 -18.928 281.302 -70.956 94.729 2.025 10.607 1740.000 -18.900 281.828 -70.961 94.620 2.219 11.068 1741.000 -18.870 282.350 -70.965 94.511 2.412 11.525 1742.000 -18.838 282.867 -70.970 94.402 2.604 11.978 1743.000 -18.804 283.379 -70.974 94.293 2.793 12.427 1744.000 -18.769 283.886 -70.978 94.184 2.981 12.872 1745.000 -18.733 284.390 -70.981 94.074 3.168 13.314 1746.000 -18.694 284.888 -70.985 93.964 3.353 13.753 1747.000 -18.655 285.383 -70.989 93.854 3.537 14.187 153
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STARDUST MISSION PLAN February 1, 1
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STARDUST MISSION PLAN Edward A. Hir
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Table of Contents Table of Contents
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10.1.1 Spacecraft Attitude History
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Figure 6.2-1.a Wild-2 Encounter Com
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Table 10.1-3 Spacecraft Attitude Pr
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kg km L L/O Kilogram Kilometer Laun
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Change Log Change Letter Date Affec
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1.0 Introduction 1.1 Purpose The pu
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2.0 Mission Overview 2.1 Mission Ob
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Fairing STARDUST Second Stage Star3
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propulsive maneuvers. To avoid pote
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The STARDUST camera is necessary to
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of-view is smaller, as described in
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Backshell Avionics Deck Parachute C
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Earth Gravity Assist 01/15/01 Earth
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Cruise 2 (Earth-Wild-2) ISP Collect
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2.3.2 Launch Period Strategy 2.3.2.
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Table 2.3-2 Baseline Mission Parame
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Table 2.3-2 Baseline Mission Parame
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*B plane angle (deg) -41.051 -40.96
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2.3.2.2 ∆V Budget The total ∆V
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Accumulation of Radiation with Time
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Table 2.3-4 STARDUST Alternate-2 Mi
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calculations will require more deta
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10 17 10 16 10 15 10 14 10 13 Fluen
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8 10 flare, no shielding 6 10 4 10
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The orbit of comet Wild-2 was drast
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• Dust density = Nucleus density
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2.4.4 Interstellar Dust Science Pla
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Launch Initial Acquisition TCM-1 Ac
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Stage II ignition t=277.5 s h=66.4
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Special ‘coming-off-theperiscope
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phases are very similar to the stan
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presented in tables contained in Ap
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Figure 4.2-4.b. Beta Meteoriod Impa
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180 Off-SEP & ORBIT normal angle (d
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2/6 launch Events Attitude 74 days
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yaw, while continuing to meet solar
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Time Image Description images pixel
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(EGA-60d to +30d) TCM 4 (EGA-60 d)
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6.0 Wild-2 Encounter Phase (E-100 t
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the installation of the HGA. The su
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Date Sept-03 Oct-03 Nov-03 Dec-03 J
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Coma images will be acquired primar
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mirror via a simple one dimension t
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The cross track error corresponds t
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14 12 10 24 km 3 sigma distance 1 s
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All 34-m HEF except selective 70-m
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SRC Entry / Descent Atmospheric Ent
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Two TCM’s are planned within this
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It is important to note that, other
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8.0 Planetary Protection The object
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Earth-Probe Range Sun-Earth-Probe A
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9.1 Mission Data Set (cont) 14.00 E
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14.00 MOON-PROBE RANGE Launch Phase
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180.00 SUN-EARTH-PROBE ANGLE EGA Ph
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180.00 SUN-PROBE-MOON ANGLE EGA Pha
Page 120 and 121: 180.00 SUN- WILD-2 -PROBE ANGLE Enc
Page 122 and 123: Cone & Clock Angles of Wild-2 Cone
Page 124 and 125: 180 Cone & Clock Angles of Sun 180
Page 126 and 127: 9.4 Wild-2 Encounter Data Set (cont
Page 128 and 129: 16.00 MOON-PROBE RANGE Return Phase
Page 130 and 131: 10.0 Appendix B: Unbalanced Attitud
Page 132 and 133: spacecraft attitude when the spacec
Page 134 and 135: Time From Launch Off-sun Angle (deg
Page 136 and 137: Acceleration (1E-11 km/s/s) 12 10 8
Page 138 and 139: +z, yaw +y, pitch +x, roll Figure 1
Page 140 and 141: ** vectors evaluated at the time of
Page 142 and 143: Rgt Ascen (deg) [eme'2000] 360 300
Page 144 and 145: Table 10.2-6 Communications Schedul
Page 146 and 147: Table 10.2-6 Communications Schedul
Page 148 and 149: 031228 19180 0 031229 19180 0 03123
Page 150 and 151: TRAJECTORY CORRECTION MANEUVERS EVE
Page 152 and 153: 2453509.10737773 50518. 143437. 229
Page 154 and 155: 50204. 3437. 2189.12 outb SEP = 3 d
Page 156 and 157: Table 12-1 ISP #1 Collection Period
Page 158 and 159: Table 12-2 ISP #2 Collection Period
Page 160 and 161: Table 12-4 ISP #2 Spacecraft Attitu
Page 162 and 163: Table 12-5 CIDA #1 Collection Perio
Page 164 and 165: Table 12-6 CIDA #2 Collection Perio
Page 166 and 167: 908.000 41.659 20.000 9.272 175.100
Page 168 and 169: Table 12-8 CIDA #1 Spacecraft Attit
Page 172 and 173: Table 12-11 CIDA #3 Solar Conjuncti
Page 174 and 175: 13.0 Appendix E: PRD Traceability M
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