Title: Mars Science and Rover Operations
1Slide 1
Mars Science and Rover Operations
Michael H. Sims, Ph.D. Center for Mars
Exploration Computational Sciences Division NASA
Ames October 10, 2002
2Slide 2
Introduction
- Science objectives are coupled with physical and
engineering constraints leading to planetary
rover operations
3Slide 3
Topics of Discussion
- How missions occur
- 3 missions one past (Pathfinder), one present
(MER) one possible future mission (Long Days
Drive) - Players and contraints on rover planetary surface
operations
4Slide 4
1997 Mars Pathfinder Sojourner
- Imaging
- Other instruments
- Sol (24 1/2 hour day) schedule
- Unusual mission
- Science team
- Science operations
5Slide 5
MER 2003 Dual Rover Mission
- Imaging
- Other instruments
- Sol (24 1/2 hour day) schedule
- Science team
- Science operations
http//athena.cornell.edu/the_mission/index.html
6Slide 6
MER Rover
7Slide 7
MER Daily Ops Schedule
8Slide 8
How are missions chosen to go to Mars?
- Main Mars Exploration Program
- Mars Scout Missions
- Human Missions
- Players Congress/OMB, NASA HQ, science
community, design teams, engineering development
teams, operations teams outreach teams.
9Slide 9
Current US Mars Surface Exploration Plans
- Mars Science Exploration Program
- Main program(Orbiters, MER, Mars Smart Lander
2009) - Mars Scout Program (2007)
- Human Exploration of Mars
- ?
10Slide 10
A Long Days Drive on Mars
- Mars Scout Proposal
- Here used an example of the interplay between
science, engineering and operations
11Slide 11
Long Days Drive Mars Scout Proposal
12Slide 12
Long Days Drive (LDD) Proposal to 2007 Mars
Scout Program
- LDD proposes to
- Explore the Northern Polar Region of Mars
- Explore during the Northern Summer (continuous
sunlight) - Explore the polar region with a robot
- Focus on the climate and geologic history in the
polar layered deposits - Although LDD would not carrying any specific life
detection instruments, LDD will look for
signatures of life in what is possibly the most
promising surface region on Mars for the
existence of life.
13Slide 13
Example of Polar Layered TerrainMOC image
14Slide 14
Close up of Example PLD
15Slide 15
Northern Polar PLD distribution and landing
ellipse sizes
16Slide 16
MEPAG - Official voice of the Mars science
community
- The LDD mission will further the following MEPAG
goals - I. Goal - Life Determine whether life ever arose
on Mars. - (Determine if life exists on Mars at present)
- (Determine if life existed on Mars in the past)
- Assess the possible presence of prebiotic
organics - II. Goal - Climate
- (Characterize Mars' present climate and climate
processes) - Characterize Mars' past climate and past climate
processes - III. Goal - Geology
- Determine the geological process(es) that
resulted in the formation of the martian crust
and surface - IV. Goal - Prepare for human exploration
- Acquire appropriate martian environmental data
- Conduct in-situ engineering and science
demonstrations
17Slide 17
MEPAG Goal 1 - LIFE
- Determine whether life ever arose on Mars.
- Determine if life exists on Mars at present
(search for organics with elemental analysis for
C/N and Raman spectroscopy look for evidence of
temperature and pressures consistent with
meltwater formation) - Determine if life existed on Mars in the past
(search for remnant organics preserved in the
polar ice). - Assess the possible presence of prebiotic
organics (search for organics preserved in the
polar ice).
18Slide 18
MEPAG Goal 2 - Climate
- Characterize Mars' present climate and climate
processes (measure the surface texture of the
polar layers and recent dust and ice
accumulation) - Characterize Mars' past climate and past climate
processes (measure the layering of the PLD over
10-100 M-yr of Martian climate history -- many
obliquity cycles)
19Slide 19
MEPAG Goal 3 - Geology
- Determine the geological process(es) that
resulted in the formation of the Martian crust
and surface (measure elemental composition and
trace volatiles in the dust/ice mixture in PLD
showing variations that may relate to geological
processes that influence the dust, such as
volcanic ash, acid weather)
20Slide 20
MEPAG Goal 4 - Prepare for human exploration
- Acquire appropriate Martian environmental data
(determine the ice content of PLD validating the
Odyssey results and giving higher resolution
local data) - Conduct in-situ engineering and science
demonstrations (demonstrate long distance solar
rover functioning and polar operations)
21Slide 21
Specific MEPAG goals are directly relevant to the
LDD mission
- Map the 3-d distribution of ice in all its
forms...temporal (seasonal) changes in
near-surface water budgets (IA1) - Conduct in-situ searches for subsurface water
(IA2a) - Map biogenic elements (C,H,N,O,P and S) (IA4a)
- Determine locations of sedimentary deposits
formed by ancient and recent surface and
subsurface hydrological process ... ground truth
of mineralogy and geochemistry for remote sensing
(IB1) - Perform in situ measurements (laser Raman)(IB1c)
- Determine timing and duration of hydrologic
activities (IB3) - Characterize history of stratigraphic records of
climate change at the polar layered deposits, the
residual ice caps. (IIB2)
- Sense 100s of sites in the visible at 15 cm/pixel
or better to characterize fine scale layers in
the layered deposits (IIB2a) - Perform in situ, local exploration of layered
deposits (IIB2c) - Perform in situ measurements, including traverses
across sedimentary units of different ages, for
several sites to determine physical properties of
rocks and fines and their chemistry, mineralogy,
lithology and petrology. (IIIA2c) - measure engineering properties of the Martian
surface (IVA6) - Conduct in situ engineering science
demonstrations (IVB)
22Slide 22
Science Questions
- A.What is the nature and record of the northern
polar layered deposits? - Determine structure of PLD. ice/ icedust
mixtures - Find well exposed layering
- Imaging of sedimentary mixing
- B.What is the nature and the distribution of
ground ice in polar region? - Seek and examine exposed snow, ice, crystals
- Determine surface structural properties by wheel
digging - Near surface hydrogen GPR search for ice
associated with dielectic boundaries - C. What is the nature of polar terrains?
- Image and spectra of wheel trench
- Survey depth of overlying slag
- Seek exposed outcrops
- Texture and compressibility of surface
- Evaluate large scale topological and geological
formations possible dunes, sand sheets, mounds,
ice penitents, eskers, etc. - D. What is the mineralogy and geochemistry of the
polar region? - Large scale basalt andesite? Small scale
variability? Northern erg of mafic material? - E. Are organics present in the polar region?
- Organics would be preserved by ice and dust -
allow inventory of impact delivered organics - Possible past subsurface liquid water
23Slide 23
Proposed measurements across the PLD
- Ice to dust ratio in the PLD
- Layering in the PLD to 1 mm thickness
- Trace elemental composition of the dust particles
in the PLD - Organic content of the PLD at a sensitivity level
of 1 ppm by mass. - Content of ice in the upper 100 m of the PLD
24Slide 24
Science to instrument mapping
- Geomorphology and mineralogy
- Cameras, spectral instruments
- Water
- remote spectral instruments
- Simple, opportunistic instrumentation
- microphone
25Slide 25
Example of Pre-EDL Operations
Prepare for EDL
Turn on B-side CDH Switch to Semaphores Pressur
ize and Fill Prop System
Initiate Slew to Entry Attitude
Complete Slew to Entry Attitude
Final Star Camera Update
Jettison Cruise Stage
Entry (accel 0.03 g)
UHF TELECOM During EDL
g -14.3 deg
V
5 min
1 min
1 min
10 min
8 min
Nominal Duration
26Slide 26
Example of Terminal Descent Phases
Altitude above Surface
Velocity
Lower Lander
750 m
Inflate Airbags
Nominal VV 43 m/s /- 15 VH /- 20
m/s Design-to VV 50 m/s VH /- 25 m/s
Release Subsonic Chute
500 m
Perform Tip-up manuever on Throttled Thrusters
Initiate Deceleration Profile
375 m
Ignite Fixed thrusters
Constant Velocity
Nominal VV 1 m/s VH /- 0.5 m/s
5 m
UHF TELECOM During EDL
Nominal VV 1 m/s VH 0.5 m/s Design-to
VV 4 m/s VH 2 m/s
Land
0 m
Release Bridle at Touchdown Control Descent
Stage Fly-away via Tether Release Tether
Deflate airbags Self-right Stand-up Egress
27Slide 27
LDDs Operation Stages