MISSION PLAN - PDS Small Bodies Node

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908.000 41.659 20.000 9.272 175.100 174.073 34.113 0.274 909.000 41.563 20.000 9.152 175.118 174.034 34.291 0.271 910.000 41.467 20.000 9.030 175.134 173.994 34.467 0.268 911.000 41.371 20.000 8.906 175.150 173.954 34.643 0.265 912.000 41.276 20.000 8.780 175.165 173.914 34.819 0.262 913.000 41.180 20.000 8.653 175.179 173.873 34.993 0.259 914.000 41.085 20.000 8.523 175.192 173.832 35.167 0.256 Table 12-7 CIDA #3 Collection Period Characteristics impact +z-off +z-off +y-off +y-off +x-off fov TFL velocity sun earth SEP-N orbit-N ISP exposure (days) (km/s) (deg) (deg) (deg) (deg) (deg) ______________________________________________________________________________________ 1703.000 55.649 20.000 21.719 135.705 177.214 1.338 0.751 1704.000 55.538 20.000 21.839 137.565 177.201 1.746 0.746 1705.000 55.426 20.000 21.961 139.329 177.187 2.149 0.741 1706.000 55.313 20.000 22.086 141.000 177.173 2.549 0.737 1707.000 55.199 20.000 22.213 142.581 177.159 2.946 0.732 1708.000 55.085 20.000 22.342 144.077 177.145 3.338 0.727 1709.000 54.970 20.000 22.474 145.492 177.130 3.727 0.723 1710.000 54.854 20.000 22.608 146.830 177.116 4.113 0.718 1711.000 54.738 20.000 22.744 148.095 177.101 4.495 0.713 1712.000 54.621 20.000 22.882 149.292 177.086 4.873 0.709 1713.000 54.503 20.000 23.022 150.424 177.071 5.248 0.704 1714.000 54.386 20.000 23.164 151.495 177.055 5.620 0.699 1715.000 54.267 20.000 23.308 152.509 177.040 5.988 0.695 1716.000 54.148 20.000 23.454 153.469 177.024 6.353 0.690 1717.000 54.029 20.000 23.601 154.380 177.008 6.715 0.686 1718.000 53.910 20.000 23.751 155.243 176.992 7.073 0.681 1719.000 53.790 20.000 23.902 156.062 176.975 7.428 0.677 1720.000 53.670 20.000 24.055 156.839 176.959 7.781 0.672 1721.000 53.550 20.000 24.210 157.578 176.942 8.130 0.667 1722.000 53.429 20.000 24.366 158.280 176.925 8.476 0.663 1723.000 53.308 20.000 24.523 158.948 176.908 8.819 0.658 1724.000 53.187 20.000 24.682 159.583 176.891 9.159 0.654 1725.000 53.066 20.000 24.843 160.189 176.873 9.497 0.649 1726.000 52.945 20.000 25.004 160.766 176.856 9.831 0.645 1727.000 52.823 20.000 25.167 161.317 176.838 10.163 0.641 1728.000 52.702 20.000 25.332 161.843 176.820 10.491 0.636 1729.000 52.580 20.000 25.497 162.345 176.802 10.818 0.632 1730.000 52.459 20.000 25.664 162.825 176.783 11.141 0.627 1731.000 52.337 20.000 25.831 163.284 176.765 11.462 0.623 1732.000 52.215 20.000 26.000 163.723 176.746 11.780 0.619 1733.000 52.093 20.000 26.170 164.144 176.727 12.095 0.614 1734.000 51.972 20.000 26.341 164.548 176.708 12.408 0.610 1735.000 51.850 20.000 26.513 164.934 176.689 12.718 0.606 1736.000 51.729 20.000 26.686 165.306 176.670 13.026 0.601 1737.000 51.607 20.000 26.859 165.662 176.650 13.332 0.597 1738.000 51.486 20.000 27.034 166.005 176.631 13.635 0.593 1739.000 51.364 20.000 27.209 166.334 176.611 13.935 0.589 1740.000 51.243 20.000 27.386 166.650 176.591 14.234 0.584 1741.000 51.122 20.000 27.563 166.955 176.571 14.530 0.580 1742.000 51.001 20.000 27.741 167.248 176.550 14.823 0.576 1743.000 50.880 20.000 27.919 167.531 176.530 15.115 0.572 1744.000 50.759 20.000 28.098 167.803 176.509 15.404 0.568 1745.000 50.638 20.000 28.278 168.065 176.488 15.691 0.564 1746.000 50.518 20.000 28.459 168.318 176.467 15.976 0.560 1747.000 50.397 20.000 28.640 168.562 176.446 16.259 0.555 148
Table 12-8 CIDA #1 Spacecraft Attitude [EME’2000] TFL i-LAT i-LNG j-LAT j-LNG k-LAT k-LNG (days) (deg) (deg) (deg) (deg) (deg) (deg) _______________________________________________________________ 45.000 -19.837 262.129 -70.047 88.561 -2.061 352.873 46.000 -19.852 262.566 -70.053 88.378 -1.862 353.239 47.000 -19.865 263.000 -70.059 88.194 -1.664 353.601 48.000 -19.877 263.430 -70.064 88.011 -1.468 353.960 49.000 -19.887 263.856 -70.068 87.827 -1.272 354.316 50.000 -19.896 264.279 -70.072 87.643 -1.078 354.669 51.000 -19.903 264.698 -70.075 87.459 -0.884 355.018 52.000 -19.909 265.113 -70.078 87.274 -0.692 355.364 53.000 -19.913 265.525 -70.080 87.090 -0.501 355.706 54.000 -19.917 266.139 -70.081 86.905 -0.245 356.228 55.000 -19.918 267.108 -70.082 86.720 0.124 357.063 56.000 -19.911 268.068 -70.082 86.534 0.491 357.890 57.000 -19.899 269.020 -70.081 86.349 0.855 358.710 58.000 -19.879 269.964 -70.080 86.163 1.217 359.524 59.000 -19.854 270.899 -70.079 85.977 1.576 0.330 60.000 -19.822 271.827 -70.076 85.791 1.932 1.130 61.000 -19.784 272.746 -70.073 85.604 2.285 1.923 62.000 -19.740 273.656 -70.070 85.418 2.635 2.710 63.000 -19.691 274.558 -70.066 85.230 2.982 3.490 64.000 -19.636 275.452 -70.061 85.043 3.327 4.263 65.000 -19.576 276.337 -70.056 84.856 3.668 5.031 66.000 -19.510 277.214 -70.050 84.668 4.006 5.792 67.000 -19.439 278.082 -70.043 84.480 4.341 6.547 68.000 -19.364 278.942 -70.036 84.291 4.673 7.295 69.000 -19.283 279.793 -70.029 84.103 5.002 8.038 70.000 -19.198 280.636 -70.020 83.914 5.327 8.775 71.000 -19.108 281.470 -70.011 83.725 5.650 9.506 72.000 -19.014 282.296 -70.002 83.535 5.969 10.231 73.000 -18.915 283.114 -69.992 83.345 6.285 10.951 74.000 -18.812 283.923 -69.981 83.155 6.598 11.665 75.000 -18.705 284.724 -69.970 82.965 6.908 12.373 76.000 -18.595 285.517 -69.958 82.774 7.214 13.076 77.000 -18.480 286.302 -69.946 82.583 7.517 13.774 78.000 -18.362 287.078 -69.933 82.391 7.817 14.466 79.000 -18.240 287.847 -69.919 82.200 8.114 15.154 80.000 -18.115 288.607 -69.905 82.007 8.408 15.835 81.000 -17.986 289.359 -69.890 81.815 8.698 16.512 82.000 -17.854 290.104 -69.874 81.622 8.985 17.184 83.000 -17.719 290.840 -69.858 81.429 9.269 17.851 84.000 -17.581 291.569 -69.841 81.235 9.550 18.513 85.000 -17.440 292.290 -69.824 81.042 9.828 19.170 86.000 -17.296 293.003 -69.806 80.847 10.103 19.823 87.000 -17.149 293.709 -69.787 80.653 10.375 20.470 88.000 -17.000 294.407 -69.768 80.457 10.643 21.114 89.000 -16.848 295.098 -69.748 80.262 10.909 21.752 90.000 -16.694 295.782 -69.728 80.066 11.171 22.386 91.000 -16.537 296.458 -69.706 79.870 11.431 23.016 92.000 -16.378 297.127 -69.684 79.673 11.687 23.641 93.000 -16.216 297.789 -69.662 79.476 11.941 24.262 94.000 -16.053 298.443 -69.639 79.278 12.191 24.879 95.000 -15.887 299.091 -69.615 79.080 12.439 25.492 96.000 -15.719 299.732 -69.590 78.881 12.684 26.100 97.000 -15.550 300.366 -69.565 78.682 12.926 26.704 98.000 -15.378 300.993 -69.539 78.483 13.165 27.305 99.000 -15.205 301.614 -69.513 78.283 13.401 27.901 100.000 -15.029 302.228 -69.485 78.082 13.635 28.494 101.000 -14.852 302.835 -69.457 77.881 13.866 29.082 102.000 -14.674 303.437 -69.428 77.680 14.094 29.667 103.000 -14.493 304.031 -69.399 77.478 14.319 30.248 104.000 -14.312 304.620 -69.369 77.275 14.542 30.825 105.000 -14.128 305.202 -69.338 77.072 14.762 31.399 106.000 -13.943 305.778 -69.306 76.869 14.980 31.969 107.000 -13.757 306.348 -69.274 76.665 15.195 32.536 108.000 -13.569 306.912 -69.240 76.460 15.408 33.099 109.000 -13.380 307.471 -69.206 76.255 15.618 33.658 110.000 -13.189 308.023 -69.172 76.049 15.825 34.214 111.000 -12.998 308.570 -69.136 75.843 16.030 34.767 112.000 -12.805 309.110 -69.100 75.636 16.233 35.316 113.000 -12.611 309.646 -69.062 75.428 16.434 35.862 114.000 -12.415 310.176 -69.024 75.220 16.632 36.405 115.000 -12.219 310.700 -68.985 75.011 16.828 36.945 116.000 -12.021 311.219 -68.946 74.802 17.021 37.481 117.000 -11.822 311.732 -68.905 74.592 17.213 38.014 118.000 -11.622 312.241 -68.863 74.381 17.402 38.545 119.000 -11.421 312.744 -68.821 74.170 17.589 39.072 149
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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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Page 118 and 119: 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 168 and 169: Table 12-8 CIDA #1 Spacecraft Attit
Page 170 and 171: Table 12-9 CIDA #2 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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