This invention relates to a mar's rover hexagonal main-body component, which is appropriate for severe environmental martian terrain and lava tubes. Background of the Invention
Human space exploration is very risky now a days. After many years humans are travelling to mars from earth. The surface of mars is different as compared to earth. This surface of mars is rocky, volcanoes, dry lakes.
To sustain the living humans in mars is very much difficult. From past fifty years many space companies sent their rovers to mars. It's economically high and used high performing sensors and mechanical subsystems.
When we investigate the previous rovers, the manufacturing cost and placed mechanisms are costly, and budget goes high. No rovers as entered the lava tubes, it's very much complex to communicate the rover to the ground station. We need lot of technology like, high performing antennas. But this rover can able to work on the surface of mars as well as the lava tubes. We used high performing sensors with cost efficient. It is easy to build and can sustain all kind of difficult task in future cases.
W01998046471A

W01998046471 -VEHICLE CHASSIS AND BODY CONSTRUCTION
This invention relates to chassis (5) and body panel (7) structural systems for a wide variety of vehicles, including automotive, water vessels, aircraft and human powered vehicles, principally comprising a node (9) and interlocking spaceframe system that can be hand assembled in the field. The invention also comprises a key (6) and lock system (2) for wedgingly interlocking body panels (7) to the spaceframe. Together these systems comprise novel Frame Integration Technology (FIT) of the invention. Examples of vehicles includes autos, utility vehicles (trucks), public transport vehicles, light boats, human powered vehicles such as bicycles, pedicabs and the like, and light aircraft.
Research gap:
No mention about the Base design which can assist and support the payload.
No information available about the Stage of radiation which will help to assist and protect the payload and itself from radiation effects.
USDOE1 0059468 Space vehicle chassis
A modular space vehicle chassis may facilitate convenient access to internal components of the space vehicle. Each module may be removable from the others such that each module may be worked on individually. Multiple panels of at least one of the modules may swing open or otherwise be removable,

exposing large portions of the internal components of the space vehicle. Such chassis architectures may reduce the time required for and difficulty ofperforming maintenance or modifications, may allow multiple space vehicles to take advantage of a common chassis design, and may further allow for highly customizable space vehicles.
No information available about the parts of doom which will protect the electronic sensor in cold storage condition.
Information related to the web structure of the base of the design found missing.
No mention about the clamp system of the base which will help to hold the doom together.
None of the prior art indicate above either alone or in combination with one another disclose what the present invention has disclosed. This invention relates to
SUMMARY OF THE INVENTION
This summary is provided to introduce a selection of concepts, in a simplified format, that are further described in the detailed description of the invention. This summary is neither intended to identify key or essential inventive concepts of the invention and nor is it intended for determining the scope of the invention.

Discloses herein a mars rover hexagonal main-body component for severe
environmental martian terrain and lava tubes comprises hexagon structure
which is more stable and spacious to place other instruments and sensors;
and Aerogel which is a thermal insulating material it is effective at transmitting
visible light and blocks infrared radiation so it's used for covers the subsystem
inside the chassis.
The chassis architecture of rover is basically of hexagonal shape to acquire
best longitudinal, lateral, and static stability.
The materials which have been used for manufacturing rover has enormous
strength to withstand severe environmental hazards and to explore the lava
tubes.
The wheel is made up of Nitinol composition which can able to overcome
obstacles.Nitinol is a composition of nickel and titanium in a percentage of
49% and 51% respectively.
The robotics arms are used to collect the samples from lava tubes and in
Martian surface; wherein use of nitinol tires, helps in driving of rover over
highly uneven terrains with smooth mobility. The mechanical design creates a
reliable system that traverse rocky Martian terrain.
To further clarify advantages and features of the present invention, a more
particular description of the invention will be rendered by reference to specific

embodiments thereof, which is illustrated in the appended drawings. It is appreciated that these drawings depict only typical embodiments of the invention and are therefore not to be considered limiting of its scope. The invention will be described and explained with additional specificity and detail with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
The illustrated embodiments of the subject matter will be understood by reference to the drawings, wherein like parts are designated by like numerals throughout. The following description is intended only by way of example, and simply illustrates certain selected embodiments of devices, systems, and methods that are consistent with the subject matter as claimed herein, wherein:
Figure 1: Hexagonal shaped rover design and with nitinol wheel.
Figure2: Hexagonal chassis with uniformly distributed loads.
Figure3: Nitinol tyres (super elastic tyres) which can travel in very severe high terrain and also in lava tubes.
The figures depict embodiments of the present subject matter for the purposes of illustration only. A person skilled in the art will easily recognize from the following description that alternative embodiments of the structures

and methods illustrated herein may be employed without departing from the principles of the disclosure described herein.
DETAILED DESCRIPTION OF THE INVENTION
The detailed description of various exemplary embodiments of the disclosure is described herein with reference to the accompanying drawings. It should be noted that the embodiments are described herein in such details as to clearly communicate the disclosure. However, the amount of details provided herein is not intended to limit the anticipated variations of embodiments; on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the scope of the present disclosure as defined by the appended claims.
It is also to be understood that various arrangements may be devised that, although not explicitly described or shown herein, embody the principles of the present disclosure. Moreover, all statements herein reciting principles, aspects, and embodiments of the present disclosure, as well as specific examples, are intended to encompass equivalents thereof.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments. As used herein, the singular forms "a"," "an" and "the" are

intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms "comprises," "comprising," "includes" and/or "including," when used herein, specify the presence of stated features, integers, steps, operations, elements and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components and/or groups thereof.
It should also be noted that in some alternative implementations, the functions/acts noted may occur out of the order noted in the figures. For example, two figures shown in succession may, in fact, be executed concurrently or may sometimes be executed in the reverse order, depending upon the functionality/acts involved.
In addition, the descriptions of "first", "second", "third", and the like in the present invention are used for the purpose of description only, and are not to be construed as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" and "second" may include at least one of the features, either explicitly or implicitly.
Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which example embodiments belong. It will be

further understood that terms, e.g., those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
Present invention discloses the chassis architecture of rover is basically of hexagonal shape to acquire best longitudinal, lateral, and static stability. Additionally, the materials which have been used for manufacturing rover has enormous strength to withstand severe environmental hazards and to explore the lava tubes.
Furtherly, an exclusive use of nitinol tires, helps in driving of rover over highly uneven terrains with smooth mobility. The mechanical design aims to create a reliable system that can not only accomplish the required functions but also traverse rocky Martian terrain.
In this rover we used hexagon structure which is more stable and spacious to place other instruments and sensors. Aerogel is a thermal insulating material it is effective at transmittingvisible light and blocks infrared radiation so it's used for covers the subsystem inside the chassis.
For wheel we used rocker bogie mechanism this helps to maintain tilt stability, it can traverse terrain wheel left and right rockers individually to climb the obstacles, the main advantage of the mechanism is no suspension required and total loads are distributed equally over all wheels.

The wheel is made up of Nitinol composition which can able to overcome obstacles. Nitinol is a composition of nickel and titanium in a percentage of 49% and 51% respectively. And we used robotics arms to collect the samples from lava tubes and in Martian surface. The main advantage is it is protected from corrosion, provides flexibility and to the wheel. BEST FEATURES OF THE INVENTION:
Nitinol tires which can be able to use in any advanced and risk condition.
Six-wheel mechanism with different dimension.
Chassis used is hexagonal shape because it reduces the thermal stress of the rover model.
Material used for mars rover is Aluminum 7075 because of its good ductility, high strength, toughness and resistance to fatigue. ADVANTAGES OF THE INVENTION:
We used Nitinol tires which can be able to use in any advanced and risk condition and can sustain more weight of the complete rover.
Using six-wheel mechanism with different dimension. The distance covered between front wheel to rear wheel and center wheel, the distance is different so, the rover can climb in high terrains as well as in lava tubes.
The chassis we use in hexagonal shape because it reduces the thermal stress of the rover model. The stress is distributed over the dooms

chassis and web and makes it stable even in the high temperature conditions
more than 100 degree centigrade.
The material can be used for this mars rover is Aluminum 7075
because of its good ductility, high strength, toughness and resistance to
fatigue.
This rover can work on surface of mars as well as lava tubes Easy to manufacture and ecofriendly non-plastic materials are used

We Claim:
1. A mars rover hexagonal main-body component for severe environmental
martian terrain and lava tubes comprises hexagon structure which is more
stable and spacious to place other instruments and sensors; and Aerogel
which is a thermal insulating material it is effective at transmitting visible light
and blocks infrared radiation so it's used for covers the subsystem inside the
chassis.
2. The Component as claimed in claim 1, wherein the chassis architecture of rover is basically of hexagonal shape to acquire best longitudinal, lateral, and static stability.
3. The Component as claimed in claim 1, wherein the materials which have been used for manufacturing rover has enormous strength to withstand severe environmental hazards and to explore the lava tubes.
4. The Component as claimed in claim 1, wherein the wheel is made up of Nitinol composition which can able to overcome obstacles.

5. The Component as claimed in claim 4, wherein Nitinol is a composition of nickel and titanium in a percentage of 49% and 51% respectively.
6. The Component as claimed in claim 1, wherein robotics arms are used to collect the samples from lava tubes and in Martian surface; wherein use of nitinol tires, helps in driving of rover over highly uneven terrains with smooth mobility.

7. The Component as claimed in claim 1, wherein the mechanical design creates a reliable system that traverse rocky Martian terrain.