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1 of 8

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Used the Flyby of Main Belt Asteroid Annefrank to Test Wild 2 Approach ... Can Implement Leisurely Trajectory Correction Maneuver Schedule and Miss a Few if Needed ... – PowerPoint PPT presentation

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Title: 1 of 8


1
STARDUST Project CRITICAL EVENTS READINESS
REVIEW COMET P/WILD 2 ENCOUNTER READINESS
PREPARATION T. Duxbury
JPL 303-411 AM / 301-427 PM LMA MSA 1 818
354-1275 0800 AM - 0500 PM PST 20 Nov 2003
2
Total Workforce  
Operations, Science, E/PO and Management at JPL
and LMA
3
SCOPE OF READINESS PREPARATION
  • Used the Flyby of Main Belt Asteroid Annefrank to
    Test Wild 2 Approach Operations, Timelines,
    Interfaces and Encounter Sequence
  • DRR and CERR Held before Event
  • Wild 2 E-3d to E1d Timeline
  • Approach Geometry Significantly More Severe than
    Wild 2Approach
  • Annefrank 30 deg from Sun, Required Large
    Attitude Turns and Performed on Batteries with
    Flyby Speed 7.4 km vrs 6.1 km/s at Wild 2
  • Annefrank Too Dim to See Before Flyby
  • All Operations Performed Within Timelines
  • All Interfaces, Peer Reviews, Command Products
    Implemented/Validated
  • Survived Loss of 1 1/2 DSN Passes - Forced
    Quick Turn Around of Sequences
  • Radio/Optical Nav Performed w/ Encounter
    Annefrank/Star Images
  • Encounter Sequence Completely Successful
  • Collector Deployed, CIDA and DFMI on and Nucleus
    Tracking Captured All 72 Flyby Images
  • Nav too Accurate, Bank Turn Computed but too
    Small to Implement
  • Operations Would Have Succeeded at Wild 2

4
SCOPE OF READINESS PREPARATION
  • Produced New Wild 2 Dust Production Model
  • 10 Times Less Collectable Dust w/ Ten Times More
    Hazardous Dust
  • Peer Reviewed w/ 15 International Comet
    Scientists
  • James Rose Chaired Review
  • Current Model Viewed as Worst Case/Upper Limit to
    Large Dust
  • Recommended Earth-based Observations for
    Additional Validation
  • Produced New Wild 2 Ephemerides
  • Accuracy of Time of Encounter Degraded from 30
    seconds to 180 seconds (1,100 km 1s)
  • Reviewed by Navigation Advisory Group (NAG)
  • Validated New Model
  • Recommended Earth-based Observations for
    Additional Validation

5
SCOPE OF READINESS PREPARATION
  • Reviewed Science Requirements and Spacecraft
    Safety
  • Moved Flyby from 150 km to 300 km for S/C Safety
  • Response to New Dust Model
  • Reduced Collection from 1,000 Particles gt 15 mm
    to 500
  • Effect of New Dust Model
  • Reduced Images Within 2,000 km from 65 to 30
  • Effect of Degraded Time of Encounter Uncertainty
  • New Mission Success Criteria in Approval Cycle at
    NASA HQ
  • Changes to Level 1 Requirements Need OSS
    Associate Administer Approval
  • Is a Given for This Review

6
SCOPE OF READINESS PREPARATION
  • Conducted Readiness Reviews of Key Operational
    Elements
  • Nav Readiness Review by Navigation Advisory Group
    (NAG)
  • Deep Space Mission Systems (DSMS) Readiness
    Review
  • Multi Mission Office (MMO) Ground Data System
    Readiness Review
  • Planetary Data System (PDS) Review of Data
    Archive Formats and Contents - Used for
    Operations as Well
  • Meetings with JPL Office of Communications and
    Education Continuing
  • 20 Full Tests of Encounter Sequence with
    Expected Range in Variables Plus Anomalies
    Nearing Completion in the Spacecraft Test
    Laboratory
  • Conducting Operational Readiness Testing (ORTs)
  • Radio Opt Nav for E-2d TCM Completed
  • E-2d to E-6h ORT Remaining
  • Science ORT Remaining
  • E/PO ORT Remaining
  • Camera Cleanup Performed / Opt Nav Images Started
  • Compliant w/ Flight Project Practices

7
SCOPE OF READINESS PREPARATION
8
READINESS
  • Simple Flyby Trajectory at Encounter
  • Straight Line Motion Past a Massless Body
  • Moved from Previous Planned Flyby of 150 km to
    300 km
  • Reduced Spacecraft Risk at Flyby by a Factor of 2
  • Reduced Delivery Performance by Nav by a Factor
    of 2
  • Successful Flyby Totally Dependent on OpNav
  • Needs DS1 Level of Sensitivity and Geometric
    Accuracy
  • Op Nav Already Detected Wild 2 - Will
    Significantly Ease Encounter Operations
  • Deleted Many Contingency Plans if Detection was
    Late
  • No Need to Take Lots of Pictures and Co-Add on
    the Ground for Detection as Planned
  • Can Implement Leisurely Trajectory Correction
    Maneuver Schedule and Miss a Few if Needed
  • The Remaining Presentations will Demonstrate
  • Relative Ease of Remaining Operations
  • Excellent Preparation and Qualifications of
    Flight Team
  • Robust Timeline w/ Excellent Margin and
    Contingency Strategies
  • The STARDUST Project is Ready for Wild 2
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