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Penetrators for Enceladus

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An orbital period (~few days) for seismic measurements. (requires RHU) Spacecraft support ... email: rag_at_mssl.ucl.uk. or see penetrator web site at ... – PowerPoint PPT presentation

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Title: Penetrators for Enceladus


1
Penetrators for Enceladus
Dr Rob Gowen on behalf of UK Penetrator Consortium
MSSL/UCL UK
Titan Saturn System Mission Workshop - Paris, Mar
17-19, 2008
2
What are Penetrators ?
  • Low mass projectiles 5KgPDS for Enceladus
  • High impact speed 200-500 m/s
  • Very tough 10-50kgee
  • Penetrate surface few metres
  • Perform science from below surface

3
Penetrator Payload/Science
  • A nominal 2kg payload
  • Accelerometers Probe surface/sub-surface
    material (hardness/composition)
  • Seismometers - Probe interior structure
    (existence/size of water reservoirs) and seismic
    activity of bodies
  • Chemical sensors Probe surface
    refactory/volatile (organic/ astrobiologic)
    chemicals, perhaps arising from interior.
  • Thermal sensors - Determine subsurface
    temperatures and possibly probe deep interior
    processes.
  • Mineralogy/astrobiology camera Probe surface
    mineralogy and possible astrobiological material.
  • other instruments to probe surface magnetic
    field, radiation, beeping transmitter, etc
  • descent camera (surface morphology, landing site
    location, etc)

4
Science/Technology Requirements
  • Target
  • E.g. region of upwelled interior material.
  • 2 penetrators would allow additional target,
    improved seismic results and natural redundancy
    but require 2xmass.
  • Lifetime
  • Only minutes/hours required for camera,
    accelerometer, chemistry, thermal
    mineralogy/astrobiologic measurements.
  • An orbital period (few days) for seismic
    measurements. (requires RHU)
  • Spacecraft support
  • 7-9 years cruise phase, health reporting
  • Delivery
  • Targetting precision.
  • Ejection, descent motors orientation,
    pre-impact separation, communications, impact.
  • Operation
  • Power/thermal (battery/RHU), data handling,
    communications.

5
Preliminary Estimated Mass
() heavy penalty for Enceladus delivery
estimate 8x(penetrator mass) with
deployment from Titan with ?V3.7Km/sec
6
Heritage
  • Lunar-A and DS2 space qualified.
  • Military have been successfully firing
    instrumented projectiles for many years to
    comparable levels of gee forces into concrete and
    steel.
  • 40,000gee qualified electronics exist (and
    re-used).
  • Currently developing similar penetrators for
    MoonLITE.
  • Payload heritage
  • Accelerometers, thermometers, sample drill
    fully space qualified.
  • Seismometers (ExoMars) chemical sensors
    (Rosetta) heritage but require impact
    ruggedizing.
  • Mineralogy camera new but simple.

When asked to describe the condition of a probe
that had impacted 2m of concrete at 300 m/s a UK
expert described the device as a bit scratched!
7
Current Development Status
Full-scale structure impact trial Scheduled May
19-23 2008
8
Current Development Status
  • MoonLITE bids in preparation for -
  • 2 yr development to bring ruggedization of
    penetrator subsystems and instruments up to TRL
    5.
  • Phase-A study for MoonLITE mission, currently in
    discussion with BNSC and NASA.
  • Bids prepared for Cosmic Visions mission support.
  • To study deltas to MoonLITE (impact into ice,
    reduced mass penetrator, long descent,
    communications)

5 inner compartments for full scale penetrator
trial
  • 3 penetrator firings
  • Normal incidence into dry sand at 300m/s

9
Main Technical Challenges
  • Ruggedisation to survive impact into ice (M?C)
  • Likely require RHUs for extended lifetime
    (requires good thermal model) (M?C)
  • Achieve proposed mass savings over MoonLITE
    penetrators (reduced lifetime -gt power saving,
    lighter structure, asics) (M?C)
  • Optimise mass estimates of descent system (M?C)
  • Study descent system in detail including target
    ellipse (C)
  • Study descent and landed communications including
    possible trailing aerial. (M?C)

(M MoonLite, C Cosmic Vision, M?C ?
development for Cosmic Vision)
10
Penetrators for Titan ?
  • Could be delivered from balloon or orbit.
  • Much smaller mass 8.5Kg/probe
  • Delivery from orbit allows -(i) deterministic
    targetting, and (ii) co-temporal placement of
    multiple penetrators for seismic network to allow
    investigation of subsurface oceans,
    interior/core, and seismic activity levels.
  • Multiple penetrators allows examining several
    different terrains (dunes, ice, lake beds)
  • Penetrators allow sampling from sub-surface e.g.
    bottom of lake beds which collect alluvial
    material deposits and possible astrobiologic
    material)

11
Further information and contact details
  • email rag_at_mssl.ucl.uk
  • or see penetrator web site at

http//www.mssl.ucl.ac.uk/planetary/missions/Micro
_Penetrators.php
12
- End -
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