The primary meteoroid flux at the Moon and at the lunar south pole

Page created by Edwin Carrillo
 
CONTINUE READING
The primary meteoroid flux at the Moon and at the lunar south pole
The primary meteoroid flux at the Moon
      and at the lunar south pole

             Althea Moorhead
  NASA Meteoroid Environment Office, MSFC
The primary meteoroid flux at the Moon and at the lunar south pole
We model shower and sporadic meteoroids separately.
                                        Shower meteors occur at a certain time of
                                        year and share similar orbits.
                                        Sporadic meteors occur throughout the year,
                                        have varied orbits, and pose more risk [ref].

                                                            100                         sporadic

                                        flux (m−2 yr−1 )
                                                                                        Geminid
                                                           10−2

                                                           10−4

                                                           10−6

                                                           10−8
         Photographs by David Kingham

                                                                  10−6    10−4   10−2    100
                                                                         limiting mass (g)
                                                                                                   2 / 19
The primary meteoroid flux at the Moon and at the lunar south pole
MEM describes the sporadic component of the meteoroid environment.

                                             Meteoroid models primarily consist of
                                             populations of meteoroid orbits. The
                                             environment varies across interplanetary
                                             distances, not km, which allows us to
                                             extrapolate from Earth-based observations.
                                             The gravity and size of the Earth and Moon
                                             affect the local environment, and the
                                             spacecraft’s motion factors in to the apparent
                                             velocity of the meteoroids it encounters.
                         v̂m − v̂sc
                                             MEM then describes the resulting
                   v̂m
                                             environment relative to a given spacecraft
                                      v̂sc
                                             trajectory [ref, ref, ref, ref, ref].

                                                                                              3 / 19
The primary meteoroid flux at the Moon and at the lunar south pole
MEM provides impactor size, angle, speed, and density.

          flux (m−2 yr−1 )
                              102
                              100
                             10−2
                             10−4
                             10−6
                             10−8
                                          10−6 10−3   100
                                        limiting mass (g)

                                                            flux (m−2 yr−1 )
          flux (m−2 yr−1 )

                             10−1
                                                                               0.15
                             10−2                                               0.1

                             10−3                                              0.05

                             10−4                                                0
                                    0     20    40    60                              0     2     4    6      8

                                        speed (km s−1 )                                   density (g cm−3 )
                                                                                                                  4 / 19
MEM has limitations that we’d like to eventually remove.

                                   Limited to inner solar system: 0.2 – 2 au
                                   Limited to within ∼ 5◦ of the ecliptic
                                   Limited to 10−6 – 10 g

                                                     103

                                   relative flux
                                                   10−6

      1
    0.5
                                                   10−15
      0
                                                       10−11     10−5      101
   −0.5
    −1                                                         limiting mass (g)
          −2    0      2

                                                                                   5 / 19
MEM 3’s improvements include a correct handling of planetary gravity

   Planets (and moons) bend and block the paths of meteoroids

                                                                        MEMR2
                                                        8               MEM 3

                                                        7

                                                 flux
                                                        6

                                                        5

                                                            104           105
                                                              altitude (km)

   This effect was erroneously large in MEMR2, and has been corrected in MEM 3. The
   flux is now lower at low altitudes and higher at high altitudes.

                                                                                      6 / 19
MEM 3’s orbital populations match their observed strength at Earth.
                                                                                    helion
                                                              0.20
                                                                                    tor.
                                        MEMR2
                                                              0.15                  apexl

                                                       flux
   60%                                  MEM 3
                                                                                    total
                                        observed              0.10

   40%                                                        0.05

                                                              0.00

   20%                                                        0.20

                                                              0.15

                                                       flux
    0%
                                                              0.10
            helion       toroidal       lapex
                                                              0.05

                                                              0.00
   This re-weighting of the orbital populations also                 10 20 30 40 50 60 70
   changes the speed distribution.                                     speed (km s−1 )
                                                                                             7 / 19
MEM 3 introduces a new, bimodal density distribution.
                                                  water          rock                iron

                                                         MEMR2
                                                                                            data
                                     20                                                     MEM 3
                                                                                            data
                                                                                            MEM 3
                                     10

                                      0
                                            0.5      1                  3       5       10

                                                             density (g     cm−3 )

   This distribution is based on detailed modeling of meteors in the atmosphere [ref, ref].

                                                                                                    8 / 19
MEM 3 predicts a higher risk for most spacecraft.

                      MEMR2

                                                                     relative freq.
                      MEM 3

                                fraction
   flux

                                                MEMR2
                                                MEM 3

          104         105                  20      40    60     80                    0.5   1       3   5    10

           altitude (km)                   speed (km    s−1 )                          density (g   cm−3 )

   MEM 3 has higher flux (at some altitudes), faster speed distribution, and new high
   densities. All of these factors will increase the risk [ref].
   How do we know that’s justified?

                                                                                                                  9 / 19
MEM 3 matches the available in situ data.

                           no extrapolation

    MEM 3 + CP                                                     MEM 3 + CP
    MEMR2 + CP                                                     MEMR2 + CP

                                                                                                 mets. + debris
                                               observed

                                                                                    meteoroids
   MEM 3 + WA                                                      MEM 3 + WA
   MEMR2 + WA                                                      MEMR2 + WA
                     extrap. to small masses

                 0       0.5      1     1.5         2                           0                50               100
                                               −2
            Pegasus penetration rate (m                   yr−1 )                number of craters on LDEF

   MEM 3 lies between the two best sets of in situ data we have in the threat regime:
   1 µg - 1 g [ref]

                                                                                                                        10 / 19
Cratering rate at the Moon (2-mm-deep in aluminum)

                       0.02
                                equator
                                45◦ S
                      0.015     south pole
   craters per year

                       0.01

                      0.005

                         0
                              east        west   north   south   zenith   nadir   total

                                                                                          11 / 19
Meteor showers are a small but varying fraction of the environment.

   Shower meteoroids constitute 1-5% of the risk, but this risk varies with time.
   We handle meteor showers in separate “forecasts” that describe their activity over the
   course of a year

         150                                                   150
                                                                     QUA                       GEM
                              (λ0 , ZHR0 )                                             PER
         100                                                   100
   ZHR

                                                                                 ARI
                                                                           ETA
         50     ∝ 10Bp (λ   −λ0 )       ∝ 10−Bm (λ   −λ0 )      50

          0                                                     0
          256   258     260         262   264   266      268    Jan        Apr   Jul     Oct
                              λ        ◦
                                      ( )                                        hi
                                                                                                     12 / 19
ZHRs are converted to flux for a given altitude and limiting parameter.

                                                                          13 / 19
We made a series of improvements starting in 2016.
                                   First, we updated many meteor shower
                                   activity profiles using data from CMOR ...
   2020   Radiant dispersions
   2019   Gravitational focusing
   2018   Other altitudes

   2016   Code & data updated

   2014   Python version

                                   Second, we updated the algorithms. For
                                   instance, we improved our calculation of the
   1998   First forecast           average shower contribution to the meteoroid
                                   flux [ref]

                                                                                  14 / 19
We expanded the code to handle other altitudes in 2018.

                                   We generalized the code in 2018 to handle
                                   additional altitudes, the Moon, and Lagrange
   2020   Radiant dispersions
                                   points [ref]
   2019   Gravitational focusing
                                                     L1              Gaia
   2018   Other altitudes
                                         4,000

   2016   Code & data updated

                                   ZHR
                                         2,000

   2014   Python version
                                            0
                                                 195.2          195.4   195.2          195.4
                                                  λ      (◦ )            λ      (◦ )

   1998   First forecast           This was done in part to enable a 2018
                                   Draconid forecast near L1 and L2.

                                                                                               15 / 19
We can now generate forecasts for specific trajectories.

                                    In 2019, we incorporated local gravitational
    2020   Radiant dispersions      focusing and planetary shielding. In 2020, we
    2019   Gravitational focusing   improved this to take stream dispersion into
    2018   Other altitudes          account [ref].

    2016   Code & data updated                               100

                                                                   enhancement
                                    0
    2014   Python version
                                                             10

                                    0
                                                             1
    1998   First forecast                 0       8R⊕

                                                                                    16 / 19
Particularly tricky showers may require more extensive modeling.

   We and colleagues at the University of Western Ontario conducted detailed simulations
   of the Draconids in advance of our 2018 and 2019 forecasts [ref].

                                                                  5000
                MSFC                                                             sims.

                                                 equivalent ZHR
                Egal et al.                                       4000           fit

                                                                  3000
       N

                                                                  2000

                                                                  1000

                                                                    0
       -0.01   -0.005         0   0.005   0.01                           195.1      195.2   195.3      195.4
                    r − r⊕ (au)                                              solar longitude         ◦
                                                                                                    ( )

   Based on these simulations, we issued an advisory for the Sun-Earth L1 point.

                                                                                                               17 / 19
We have begun to issue forecasts for the lunar surface

                                  NASA M ETEOROID E NVIRONMENT O FFICE

              The 2020 meteor shower activity forecast for the lunar surface

                                                 Issued 8 November 2019

           The purpose of this document is to provide a forecast of major meteor shower activity on the lunar
       surface. While the predictions in this document are for the surface, spacecraft orbiting the Moon at low
       altitudes will encounter meteoroids at similar rates. Typical activity levels are expected for nearly all show-
       ers in 2020; only the Geminids, which are gradually increasing in strength over time, are expected to be
       stronger than in previous years. No meteor storms or outbursts are predicted for 2020.

       1 Overview

         No meteor shower outbursts are predicted for 2020. The fluxes and enhancement factors in this docu-
       ment correspond to the “typical” level of activity of the showers in our list in most cases. We have made         18 / 19
Summary

  MEM is our sporadic environment model:
  I It covers the bulk of the meteoroid environment and is useful during the design
    phase of a mission.
  I MEM 3 was released mid-2019 and offers many improvements over previous
    versions. It predicts higher risk but matches meteor and impact data.
  I It’s the most appropriate tool for simulating the primary meteoroid flux onto the
    Moon.

  Separately, we issue meteor shower forecasts:
  I The code we use has gradually increased in complexity and fidelity and is beginning
     to resemble MEM.
  I Inputs are based on both typical shower activity and model predictions.
  I We have begun to issue forecasts specific to the lunar surface.

                                                                                          19 / 19
You can also read