MISSION PLAN - PDS Small Bodies Node

More documents

Recommendations

Info

List of Acronyms and Abbreviations β Beta ∆V Delta-Velocity λ Wavelength µm Micrometer # Number A-h Acq ACS AD Alt ARIA AU bps Ampere-hour Acquisition Attitude Control System ER Arrival Date Altitude Advanced Range Instrumentation Aircraft Astronomical Unit Bits Per Second Instrument DSM Deep Space Maneuver DSN Deep Space Network DST Deep Space Transponder E, Enc Encounter, Wild-2 Ear Earth EE Earth-Earth EGA Earth Gravity Assist EGAD Earth Gravity Assist Date eng Engineering EPS Electrical Power System ER Earth Return ET Ephemeris Time EW Earth-Wild-2 FOV Field Of View fps Feet Per Second ft Feet C3 cc CCD C&DH CIDA cm CMD conj cos COSPAR d D Dap dB Dec deg DFMI Injection Energy Per Unit Mass Cubic Centimeters Charge Coupled Device Command and Data Handling Cometary and Interstellar Dust Analyzer Centimeter Command Conjunction Cosine Committee On Space Research Day Dimension Declination, approach Decibel Declination Degrees Dust Flux Monitor g g GCR Ghz h h HEF HGA img IMU Unit ISC ISP JPL JSC Grams Unit Of Acceleration Equal To Earth’s Gravity Galactic Cosmic Ray Giga-hertz Altitude Hour High-Efficiency High Gain Antenna Image Inertial Measurement Current, Short Circuit Interstellar Dust Particle Jet Propulsion Laboratory Johnson Space Center viii
kg km L L/O Kilogram Kilometer Launch Liftoff lb lb-f LD LGA LMA Pound Foot-Pound Launch Date Low Gain Antenna Lockheed Martin Astronautics List of Acronyms and Abbreviations (cont) m, min Minute m, M Meter mag Magnitude max Maximum MECO Main Engine Cutoff MEL Mass Element List mem Memory MeV Million Electron Volts MGA Medium Gain Antenna mm Millimeter MSL Mean Sea Level ms Millisecond N North NASA National Aeronautics and Space Administration Nav Navigation NCS Nutation Control System nmi Nautical Miles OD Orbit Determination OPNAV Optical Navigation opp Opposition Rap Rcvr RDM Re Req’d RFS RPM Rs Right Ascension, approach Receiver Radiation Design Margin Range, Earth Required Radio Frequency System Revolutions Per Minute Range, Solar s, sec Second seg Segment S South S Unit Vector Orthogonal To R, In Direction Of Target Body Velocity S/A Solar Array S/C Spacecraft SECO Stage II Engine Cutoff SRC Sample Return Capsule SRM Solid Rocket Motor SSPA Solid-State Power Amplifier Pmax PMS R Ra Potential, refers to Open Circuit Voltage Power Management Subsystem Unit Vector Along Sun- Target Body Line Right Ascension t T TBD TBR TCM TP Time Out Of Plane Unit Vector To Be Determined To Be Resolved Trajectory Correction Maneuver Time Of Perihelion Passage ix
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: Table 10.1-3 Spacecraft Attitude Pr
Page 17 and 18: Change Log Change Letter Date Affec
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
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 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 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
show all

MISSION PLAN - PDS Small Bodies Node

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?