Title: PHOBOS SOIL
1PHOBOS - SOIL
Russian academy of sciences
Russian aviation and space agency
- Phobos Sample Return Mission
- 1. goals, methods of study
- A.Zakharov, zakharov_at_iki.rssi.ru
2Goals of the Mission
PHOBOS - SOIL
- Phobos regolith sample return,
- Phobos in situ study,
- Mars and Phobos remote sensing.
- Mars system science
- Phobos investigation (regolith, origin and
evolution of the Martian moons), - Martian environment conditions (dust, plasma,
radiation), - Monitoring of the Martian atmosphere and surface
global dynamics.
3Scientific objections
PHOBOS - SOIL
- study physical and chemical characteristics of
Phobos regolith and subsurface layers in situ and
under laboratory conditions - these data can
provide information on properties of primordial
matter of the Solar system - study of the role played by asteroidal impacts in
the formation of terrestrial planets, in the
evolution of their atmospheres, crusts, and
inventories of volotiles - study of the origin of the Martian satellites and
their relation to Mars - these data can help in
our understanding of their evolution and the
origin of satellite systems near other planets - search of possible life or paleolife
- study of peculiarities of orbital and proper
motion of Phobos, what is important for
understanding their origin, internal structure,
celestial mechanics applications - study physical conditions of the Martian
environment (dust, gas, plasma components) what
is important to study of treatment processes of
small body regolith under influence of external
conditions and creation of engineering model of
the Martian environment for future Martian
missions - Monitoring of dynamic of the Martian atmosphere
and seasons climate changing.
4 Methods of investigation
PHOBOS - SOIL
- 1. Delivery of sample of the matter at the Earth.
With a returned sample it would be possible to
address the following topics - absolute dating, the length of formatting
interval and the subsequent evolution - precise identification of primitive material, its
chemical composition - origin of Phobos / Deimos and their relation to
Mars - search of organic material.
- 2. In-situ study. Measurements on Phoboss
surface will provide the opportunity to establish
a ground truth data need for validation and
interpretation of remote sensing and to do a
detailed, in situ study of regolith samples,
specifically their - elemental and mineral composition, volatile
content - microscopic structure, physical and mechanical
properties of the regolith - celestial mechanic and fundamental physics
experiments - long duration monitoring of Mars.
- 3. Remote sensing Remote sensing of Phobos from
co-orbiting spacecraft will provide global
coverage of data related to both the surface and
internal structure of the satellite, will provide
an opportunity to relate data returned from the
landing site to the all Phoboss surface - global geologic mapping,
- size, shape, mass, bulk density,
- color, albedo, photometric scattering and thermal
properties, - mapping of global elemental and mineral
composition, - internal structure,
- landing site certification and selection,
- The Martian environment (dust tori, solar wind -
Phoboss surface interaction).
5PHOBOS - SOIL
MAIN CHARACTERISTICS OF THE MISSION
Launch vehicleSoyuz-2 Launch
date. September 7-29,
2009 Flight duration (to Mars).....
280-350 days Launch date from Phobos13
.07-12 August 2011 Duration of near-Mars
operation time....not more than 365
days Flight duration (from Mars)...29
5-320 days Date of arrival to Earth
.14.05-8 June 2012 Total duration of the
mission.1005 days
6PHOBOS - SOIL
MISSION PROFILE
The Lavochkin / Babakin space association design
7PHOBOS - SOIL
Payload zone
Payload zone
The Lavochkin / Babakin space association design
8PHOBOS - SOIL
SC CONFIGURATION (on the
Phobos surface)
HGA
Return vehicle
Soil sampling device
Solar array
Landing gear
The Lavochkin / Babakin space association design
9Strawman Payload
PHOBOS - SOIL
10Current status
PHOBOS - SOIL
- The PHOBOS-GRUNT project is the only national
planetary project in the current decade. - The Lavochkin / Babakin space association is the
main contractor of the spacecraft. Mass of the
payload is 50 kg. The project has the resources
to include additional payload with a mass about
120 kg. This mass margin could be used for
including additional element(s) for the
investigation of Mars (i.e. small station on the
surface, balloon, penetrators, etc.) or a probe
for the study of Deimos. - About 30 proposals for scientific experiments
have been received for the project from Russian
scientific teams. The next step is a preselected
search of proposed experiments for the mission
from scientific and technical point of view. -