MISSION PLAN - PDS Small Bodies Node

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Table 12-4 ISP #2 Spacecraft Attitude [EME’2000] TFL i-LAT i-LNG j-LAT j-LNG k-LAT k-LNG (days) (deg) (deg) (deg) (deg) (deg) (deg) _______________________________________________________________ 1267.000 -9.487 44.919 -68.749 160.367 18.833 131.652 1268.000 -9.317 45.031 -68.862 160.141 18.797 131.830 1269.000 -9.150 45.144 -68.974 159.916 18.762 132.008 1270.000 -8.984 45.258 -69.084 159.693 18.726 132.186 1271.000 -8.820 45.374 -69.192 159.471 18.690 132.365 1272.000 -8.658 45.490 -69.299 159.251 18.654 132.544 1273.000 -8.497 45.607 -69.404 159.033 18.617 132.723 1274.000 -8.338 45.726 -69.508 158.816 18.580 132.902 1275.000 -8.181 45.845 -69.610 158.600 18.543 133.081 1276.000 -8.026 45.966 -69.711 158.386 18.506 133.261 1277.000 -7.872 46.087 -69.810 158.174 18.469 133.440 1278.000 -7.720 46.210 -69.909 157.963 18.431 133.620 1279.000 -7.569 46.333 -70.006 157.753 18.393 133.800 1280.000 -7.420 46.457 -70.101 157.545 18.355 133.981 1281.000 -7.273 46.583 -70.196 157.339 18.317 134.161 1282.000 -7.126 46.709 -70.289 157.133 18.278 134.342 1283.000 -6.982 46.836 -70.381 156.930 18.239 134.523 1284.000 -6.839 46.964 -70.472 156.728 18.200 134.705 1285.000 -6.697 47.093 -70.562 156.527 18.161 134.886 1286.000 -6.556 47.223 -70.651 156.328 18.121 135.068 1287.000 -6.417 47.354 -70.738 156.130 18.082 135.250 1288.000 -6.279 47.486 -70.825 155.933 18.042 135.432 1289.000 -6.143 47.619 -70.911 155.738 18.001 135.615 1290.000 -6.008 47.752 -70.995 155.545 17.961 135.797 1291.000 -5.874 47.887 -71.079 155.353 17.920 135.980 1292.000 -5.741 48.022 -71.162 155.162 17.879 136.164 1293.000 -5.610 48.158 -71.244 154.972 17.838 136.347 1294.000 -5.480 48.296 -71.325 154.785 17.796 136.531 1295.000 -5.351 48.433 -71.405 154.598 17.754 136.715 1296.000 -5.223 48.572 -71.484 154.413 17.712 136.899 1297.000 -5.097 48.712 -71.562 154.229 17.670 137.084 1298.000 -4.971 48.852 -71.640 154.047 17.628 137.269 1299.000 -4.847 48.994 -71.717 153.866 17.585 137.454 1300.000 -4.724 49.136 -71.793 153.686 17.542 137.639 1301.000 -4.602 49.279 -71.868 153.508 17.499 137.825 1302.000 -4.481 49.423 -71.943 153.331 17.455 138.011 1303.000 -4.361 49.567 -72.017 153.155 17.411 138.197 1304.000 -4.242 49.713 -72.090 152.981 17.367 138.383 1305.000 -4.124 49.859 -72.163 152.808 17.323 138.570 1306.000 -4.008 50.006 -72.234 152.637 17.278 138.757 1307.000 -3.892 50.154 -72.306 152.467 17.233 138.945 1308.000 -3.777 50.303 -72.376 152.298 17.188 139.132 1309.000 -3.664 50.452 -72.446 152.131 17.143 139.321 1310.000 -3.551 50.603 -72.516 151.964 17.097 139.509 1311.000 -3.439 50.754 -72.585 151.800 17.051 139.698 1312.000 -3.329 50.906 -72.653 151.636 17.005 139.887 1313.000 -3.219 51.058 -72.721 151.474 16.958 140.076 1314.000 -3.110 51.212 -72.788 151.313 16.912 140.266 1315.000 -3.002 51.366 -72.855 151.154 16.865 140.456 1316.000 -2.895 51.522 -72.921 150.996 16.817 140.646 1317.000 -2.789 51.678 -72.987 150.839 16.770 140.836 1318.000 -2.684 51.834 -73.052 150.683 16.722 141.027 1319.000 -2.580 51.992 -73.117 150.529 16.673 141.219 1320.000 -2.476 52.150 -73.181 150.376 16.625 141.411 1321.000 -2.374 52.310 -73.245 150.224 16.576 141.603 1322.000 -2.272 52.470 -73.309 150.074 16.527 141.795 1323.000 -2.172 52.630 -73.372 149.925 16.478 141.988 1324.000 -2.072 52.792 -73.435 149.777 16.428 142.181 1325.000 -1.973 52.955 -73.497 149.631 16.378 142.375 1326.000 -1.875 53.118 -73.559 149.486 16.328 142.568 1327.000 -1.777 53.282 -73.621 149.342 16.277 142.763 1328.000 -1.681 53.447 -73.682 149.200 16.226 142.957 1329.000 -1.585 53.612 -73.743 149.058 16.175 143.152 1330.000 -1.491 53.779 -73.804 148.919 16.124 143.348 1331.000 -1.397 53.946 -73.864 148.780 16.072 143.544 1332.000 -1.303 54.114 -73.925 148.643 16.020 143.740 1333.000 -1.211 54.283 -73.985 148.507 15.967 143.937 1334.000 -1.120 54.453 -74.044 148.372 15.914 144.134 1335.000 -1.029 54.624 -74.104 148.239 15.861 144.331 1336.000 -0.939 54.795 -74.163 148.107 15.808 144.529 1337.000 -0.850 54.967 -74.222 147.976 15.754 144.727 1338.000 -0.761 55.140 -74.280 147.847 15.700 144.926 142
Table 12-4 ISP #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) _______________________________________________________________ 1339.000 -0.674 55.314 -74.339 147.719 15.646 145.125 1340.000 -0.587 55.489 -74.397 147.592 15.591 145.325 1341.000 -0.501 55.664 -74.455 147.467 15.536 145.525 1342.000 -0.416 55.841 -74.513 147.343 15.481 145.726 1343.000 -0.332 56.018 -74.571 147.220 15.425 145.927 1344.000 -0.248 56.196 -74.629 147.099 15.369 146.128 1345.000 -0.165 56.375 -74.686 146.979 15.313 146.330 1346.000 -0.083 56.555 -74.744 146.860 15.256 146.532 1347.000 -0.002 56.736 -74.801 146.743 15.199 146.735 1348.000 0.079 56.917 -74.858 146.627 15.141 146.938 1349.000 0.158 57.100 -74.915 146.513 15.084 147.142 1350.000 0.237 57.283 -74.972 146.399 15.026 147.347 1351.000 0.315 57.467 -75.029 146.288 14.967 147.551 1352.000 0.393 57.652 -75.086 146.177 14.908 147.757 1353.000 0.469 57.838 -75.143 146.069 14.849 147.962 1354.000 0.545 58.025 -75.200 145.961 14.790 148.169 1355.000 0.620 58.213 -75.257 145.855 14.730 148.376 1356.000 0.694 58.401 -75.313 145.751 14.669 148.583 1357.000 0.768 58.591 -75.370 145.647 14.609 148.791 1358.000 0.841 58.781 -75.427 145.546 14.548 148.999 1359.000 0.912 58.972 -75.484 145.446 14.486 149.208 1360.000 0.984 59.165 -75.541 145.347 14.424 149.418 1361.000 1.054 59.358 -75.597 145.250 14.362 149.628 1362.000 1.123 59.552 -75.654 145.154 14.300 149.838 1363.000 1.192 59.747 -75.711 145.060 14.237 150.049 1364.000 1.260 59.943 -75.768 144.968 14.173 150.261 1365.000 1.327 60.140 -75.825 144.877 14.110 150.473 1366.000 1.393 60.338 -75.883 144.788 14.046 150.686 1367.000 1.459 60.537 -75.940 144.700 13.981 150.900 1368.000 1.524 60.736 -75.997 144.614 13.916 151.114 1369.000 1.587 60.937 -76.055 144.530 13.851 151.329 1370.000 1.650 61.139 -76.113 144.447 13.785 151.544 1371.000 1.712 61.342 -76.170 144.366 13.719 151.760 1372.000 1.774 61.545 -76.229 144.287 13.652 151.976 1373.000 1.834 61.750 -76.287 144.209 13.585 152.193 1374.000 1.894 61.956 -76.345 144.133 13.518 152.411 1375.000 1.952 62.163 -76.404 144.060 13.450 152.630 1376.000 2.010 62.370 -76.463 143.988 13.382 152.849 1377.000 2.067 62.579 -76.522 143.917 13.313 153.068 1378.000 2.123 62.789 -76.581 143.849 13.244 153.289 1379.000 2.178 63.000 -76.640 143.783 13.174 153.510 1380.000 2.233 63.212 -76.700 143.719 13.104 153.732 1381.000 2.286 63.425 -76.760 143.656 13.034 153.954 1382.000 2.338 63.639 -76.821 143.596 12.963 154.177 1383.000 2.390 63.854 -76.881 143.538 12.892 154.401 1384.000 2.440 64.070 -76.942 143.482 12.820 154.626 1385.000 2.431 64.029 -77.004 143.428 12.759 154.580 1386.000 2.295 63.427 -77.065 143.377 12.722 153.945 1387.000 2.159 62.822 -77.128 143.328 12.684 153.309 1388.000 2.023 62.216 -77.190 143.281 12.644 152.670 1389.000 1.887 61.609 -77.253 143.236 12.602 152.031 1390.000 1.751 60.999 -77.316 143.194 12.558 151.390 1391.000 1.615 60.389 -77.380 143.155 12.513 150.748 1392.000 1.480 59.778 -77.444 143.118 12.466 150.105 1393.000 1.344 59.165 -77.509 143.084 12.416 149.462 1394.000 1.210 58.553 -77.574 143.053 12.365 148.818 1395.000 1.076 57.940 -77.639 143.024 12.312 148.174 1396.000 0.942 57.326 -77.706 142.998 12.257 147.531 1397.000 0.809 56.713 -77.772 142.976 12.200 146.888 1398.000 0.677 56.100 -77.840 142.956 12.141 146.246 1399.000 0.546 55.488 -77.907 142.939 12.080 145.605 1400.000 0.415 54.877 -77.976 142.926 12.017 144.965 1401.000 0.286 54.266 -78.045 142.916 11.952 144.327 1402.000 0.157 53.657 -78.115 142.910 11.884 143.690 143
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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
Page 110 and 111: Earth-Probe Range Sun-Earth-Probe A
Page 112 and 113: 9.1 Mission Data Set (cont) 14.00 E
Page 114 and 115: 14.00 MOON-PROBE RANGE Launch Phase
Page 116 and 117: 180.00 SUN-EARTH-PROBE ANGLE EGA Ph
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 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 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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