- 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 and 16: kg km L L/O Kilogram Kilometer Laun
- Page 17: Change Log Change Letter Date Affec
- 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
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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
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180.00 SUN- WILD-2 -PROBE ANGLE Enc
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Cone & Clock Angles of Wild-2 Cone
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180 Cone & Clock Angles of Sun 180
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9.4 Wild-2 Encounter Data Set (cont
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16.00 MOON-PROBE RANGE Return Phase
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10.0 Appendix B: Unbalanced Attitud
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spacecraft attitude when the spacec
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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
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** vectors evaluated at the time of
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Rgt Ascen (deg) [eme'2000] 360 300
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Table 10.2-6 Communications Schedul
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Table 10.2-6 Communications Schedul
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031228 19180 0 031229 19180 0 03123
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TRAJECTORY CORRECTION MANEUVERS EVE
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2453509.10737773 50518. 143437. 229
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50204. 3437. 2189.12 outb SEP = 3 d
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Table 12-1 ISP #1 Collection Period
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Table 12-2 ISP #2 Collection Period
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Table 12-4 ISP #2 Spacecraft Attitu
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Table 12-5 CIDA #1 Collection Perio
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Table 12-6 CIDA #2 Collection Perio
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908.000 41.659 20.000 9.272 175.100
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Table 12-8 CIDA #1 Spacecraft Attit
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Table 12-9 CIDA #2 Spacecraft Attit
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Table 12-11 CIDA #3 Solar Conjuncti
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13.0 Appendix E: PRD Traceability M