MISSION PLAN - PDS Small Bodies Node

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UHF UTTR v VEGA Vhp,b Ultra High Frequency Utah Test and Training Range Velocity Soviet Mission to Venus & Comet Halley (1984-6) Velocity, hyperbolic, approach VOC Voltage, Open Circuit W Watts w, wk Week W2 Wild-2, comet WE Wild-2-Earth WRT With Respect To yr Year x
Change Log Change Letter Date Affected Sections Original Issue Revision A Revision B 10/7/1995 1/28/1997 2/1/1999 All All 1.1, 1.2, 1.3, 2.2.1, 2.2.2.x, 2.3.1, 2.3.2.1, 2.3.2.2, 2.4.1, 2.4.2.1, 2.4.2.3, 2.4.3, 2.4.4*, 3.2, 3.3, 3.4, 4.1, 4.2, 4.2.x*, 4.3, 5.1, 5.2, 6.1, 6.2.2.1, 6.2.2.3*, 6.2.4, 6.3, 7.1, 7.2.1.1, 7.2.2, 7.3*, 9.2, 9.3, 10.x*, 11.x*, 12.x*, 13.0* (see change paper XF0236) * includes new sections xi
Page 1 and 2: STARDUST MISSION PLAN February 1, 1
Page 4 and 5: STARDUST MISSION PLAN Edward A. Hir
Page 7 and 8: Table of Contents Table of Contents
Page 9 and 10: 10.1.1 Spacecraft Attitude History
Page 11 and 12: Figure 6.2-1.a Wild-2 Encounter Com
Page 13 and 14: Table 10.1-3 Spacecraft Attitude Pr
Page 15: kg km L L/O Kilogram Kilometer Laun
Page 19 and 20: 1.0 Introduction 1.1 Purpose The pu
Page 21 and 22: 2.0 Mission Overview 2.1 Mission Ob
Page 23 and 24: Fairing STARDUST Second Stage Star3
Page 25 and 26: propulsive maneuvers. To avoid pote
Page 27 and 28: The STARDUST camera is necessary to
Page 29 and 30: of-view is smaller, as described in
Page 31 and 32: Backshell Avionics Deck Parachute C
Page 33 and 34: Earth Gravity Assist 01/15/01 Earth
Page 35 and 36: Cruise 2 (Earth-Wild-2) ISP Collect
Page 37 and 38: 2.3.2 Launch Period Strategy 2.3.2.
Page 39 and 40: Table 2.3-2 Baseline Mission Parame
Page 41 and 42: Table 2.3-2 Baseline Mission Parame
Page 43 and 44: *B plane angle (deg) -41.051 -40.96
Page 45 and 46: 2.3.2.2 ∆V Budget The total ∆V
Page 47 and 48: Accumulation of Radiation with Time
Page 49: Table 2.3-4 STARDUST Alternate-2 Mi
Page 52 and 53: calculations will require more deta
Page 54 and 55: 10 17 10 16 10 15 10 14 10 13 Fluen
Page 56 and 57: 8 10 flare, no shielding 6 10 4 10
Page 58 and 59: The orbit of comet Wild-2 was drast
Page 60 and 61: • Dust density = Nucleus density
Page 62 and 63: 2.4.4 Interstellar Dust Science Pla
Page 64 and 65: Launch Initial Acquisition TCM-1 Ac
Page 66 and 67:
Stage II ignition t=277.5 s h=66.4
Page 68 and 69:
Special ‘coming-off-theperiscope
Page 70 and 71:
phases are very similar to the stan
Page 72 and 73:
presented in tables contained in Ap
Page 74 and 75:
Figure 4.2-4.b. Beta Meteoriod Impa
Page 76 and 77:
180 Off-SEP & ORBIT normal angle (d
Page 78 and 79:
2/6 launch Events Attitude 74 days
Page 80 and 81:
yaw, while continuing to meet solar
Page 82 and 83:
Time Image Description images pixel
Page 84 and 85:
(EGA-60d to +30d) TCM 4 (EGA-60 d)
Page 86 and 87:
6.0 Wild-2 Encounter Phase (E-100 t
Page 88 and 89:
the installation of the HGA. The su
Page 90 and 91:
Date Sept-03 Oct-03 Nov-03 Dec-03 J
Page 92 and 93:
Coma images will be acquired primar
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mirror via a simple one dimension t
Page 96 and 97:
The cross track error corresponds t
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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
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Acceleration (1E-11 km/s/s) 12 10 8
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+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
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TRAJECTORY CORRECTION MANEUVERS EVE
Page 152 and 153:
2453509.10737773 50518. 143437. 229
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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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MISSION PLAN - PDS Small Bodies Node

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