MISSION PLAN - PDS Small Bodies Node

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Table 10.2-6 Communications Schedule Time (dFL) Dur (hrs) Antenna Flip-y? (opt) Slew option 32,35,38,41,44 4 MGA 0 2 51,58,65,72,79 4 MGA 0 3 86,93,100,107,114,121,128,135,142 4 MGA 0 4 149,156,163,170,174,184,191,198,205,212,219, 4 MGA 0 2 226,233,240,247,254 261 4 HGA 0 2 268,275,282 4 MGA 0 2 292 4 HGA 0 2 303,309,319,324 4 MGA 0 2 331 4 HGA 0 2 338, 345 4 MGA 0 2 352 4 HGA 0 2 362, 364, 366, 371, 374, 376, 380, 384-401 4 MGA 0 2 402 4 HGA 0 2 403-409, 412, 415, 417, 419, 422, 425-432 4 HGA 1 4 433-439, 442, 445, 448, 451 4 MGA 0 7 454,457 4 MGA 0 3 464 4 HGA 0 3 471,478,485,492 4 MGA 0 2 499 4 HGA 0 2 506,513,520,527,534,541,548,555,562,569,576, 4 MGA 0 2 583,590,597,604,611,618,623,626,629,632,635- 663,666,669,672,674,676,679,682,685-694 695-707 8 MGA 0 2 728-753,756,759,762,765 4 MGA 0 2 772,779,786,793,800 4 MGA 0 3 807,814,821,828,835,842,849,856,863,870,877, 4 MGA 0 4 884,891,898,905,912 919,926,933 4 MGA 0 2 940 4 HGA 0 2 947,954,961,968 4 MGA 0 2 975 4 HGA 0 2 982, 989, 996, 1003 4 MGA 0 2 1010 4 HGA 0 2 1017, 1024, 1031 3 MGA 0 2 1038 3 HGA 0 2 1046, 1048, 1057, 1066, 1073 3 MGA 0 2 1080 3 HGA 0 2 1087, 1094, 1101, 1104, 1107, 1110, 1113, 3 MGA 0 2 1116, 1118, 1120 1122 3 HGA 0 2 1124, 1126, 1128, 1130, 1132, 1134, 1136, 3 MGA 0 2 1138, 1140, 1142, 1144, 1147 1150 3 HGA 0 2 1153, 1157, 1164, 1171, 1178 3 MGA 0 2 1185 3 HGA 0 2 1192,1199,1206,1213 3 MGA 0 2 1220 3 HGA 0 2 1227,1234,1241,1248,1255,1262 3 MGA 0 2 126
Table 10.2-6 Communications Schedule (cont) Time (dFL) Dur (hrs) Antenna Flip-y? (opt) Slew option 1269,1276,1283 3 MGA 0 7 1290,1297,1304,1311,1318 3 MGA 0 4 1325,1332 4 MGA 0 4 1339 4 HGA 0 4 1346,1353,1360,1367 4 MGA 0 4 1374 4 HGA 0 4 1381,1388,1395 4 MGA 0 4 1402 4 MGA 0 2 1409 4 HGA 0 2 1416,1423,1430,1437 4 MGA 0 2 1444 4 HGA 0 2 1451,1458,1465,1472 4 MGA 0 2 1479 4 HGA 0 2 1486,1493,1500,1507 4 MGA 0 2 1514 4 HGA 0 2 1521,1528,1535,1542 4 MGA 0 2 1549 4 HGA 0 2 1556,1563,1570,1577, 1579, 1582 4 MGA 0 2 1585 4 HGA 0 2 1588, 1591, 1594-1615 4 MGA 0 2 1616 4 HGA 0 2 1617-1630, 1633, 1636, 1639, 1642, 1645, 1647 4 MGA 0 2 1654, 1661 1668 4 HGA 0 2 1675, 1682 4 MGA 0 2 1691 6 HGA 0 2 1698 8 HGA 0 2 1705, 1712 8 HGA 1 3 1719, 1726, 1733, 1739, 1742, 1746 8 HGA 1 4 1747,1748 4 MGA 0 1 1749 8 HGA 0 2 1750-1752 4 MGA 0 1 1753 8 HGA 0 2 1754,1755 4 MGA 0 1 1756 8 HGA 0 2 1757-1759 4 MGA 0 1 1760 8 HGA 0 2 1761,1762 4 MGA 0 1 1763 8 HGA 0 2 1764-1766 4 MGA 0 1 1767 8 HGA 0 2 1768,1769 4 MGA 0 1 1770 8 HGA 0 2 1771-1773 4 MGA 0 1 1774 8 HGA 0 2 1775,1776 4 MGA 0 1 1777 8 HGA 0 2 1778,1779 4 MGA 0 1 1780 8 HGA 0 1 127
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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
Page 94 and 95: mirror via a simple one dimension t
Page 96 and 97: The cross track error corresponds t
Page 98 and 99: 14 12 10 24 km 3 sigma distance 1 s
Page 100 and 101: All 34-m HEF except selective 70-m
Page 102 and 103: SRC Entry / Descent Atmospheric Ent
Page 104 and 105: Two TCM’s are planned within this
Page 106 and 107: It is important to note that, other
Page 108 and 109: 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 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 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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