~This Site and Project is Under Development

Mars Mission

Planetary Biological Hazard Identification Process
Design process for assessing potential and possible hazards for integrating life to another planet.
Create paper on the ethics and potential dangers of landing any vehicles and especially human visitation of planets. The danger of inoculating life forms on another planet.

An international conference and summit should be conducted to deal with rights and uses, and provide a legal framework to coordinate future endeavors in space.
Procedures for hazardous processes identification should be specified for all future space-exploration.
Also, the question of whether the introduction of life will permanently poison a planet, rendering its environment uninhabitable must be thoroughly addressed.
Slime mold and penicillin are among the most robust life-forms, many of which are extraordinarily hard to eliminate from all forms of equipment and pose a nearly impossible job of abating. Slime organisms, as an example, are so pervasive, forms are found in deep caves, - are sulfur based, and need no sunlight.
If we go to Mars, there will be an absolute, 100% result. The many possibilities need to be examined under the full scrutiny of the scientific community. This proposed Hazard ID Project is paramount, wholly necessary preparatory work and not small. It needs to be an international effort.
The importance of doing such a project needs to be communicated and considered by the wider science community.

Procedures for hazardous processes identification will need to be specified under international treaty for all future space-exploration.

At the present time, inquiries for present work on this subject finds people pressing forward on their various projects without any apparent concern nor even notion of this problem.

Over-all Operations Protocol
Articulate the Over-all Operations Protocol to define all parameters including financing by member states and corporations.

Mars Development Project
Mars station, living, working, energy - and purpose/products project proposal, including mining and sciences.
Design overall Mars Development Project. Create purpose statement.
Articulate contracts of ownership and licensing for lands, products and materials to the corporation and investors.

Examine notion of Refueling and vehicle dump - /repair and retrofit station for general space activities support, midway between Earth and Mars.

Mission Structure:

Earth to orbit system of aircraft towed orbiter-vehicles, transverse shipping, stationary satellites and lander vehicles. These will include a schematic of public and private companies and endeavors.
Life support system includes self-sustaining septic, water and air to accommodate space vehicles and planetary installations.
There shall be countervail schemes and systems in space-craft with rotating domiciles. One scheme could have certain outside functions arranged on movable panels, where sensor-driven computer logs dictate to panel positioning, a continuing operations off-set.
Life support craft will be designed to accommodate and integrate with all uses including space vehicles, asteroid mining environments and planetary installations.

All work stations can become future science laboratories.
Plans will be constructed for science labs and multi-array observatories on Mars, or around the Mars orbiting descent and launch station, or around the mid travel-point fuels-dump space station.

It will be necessary to build a materials processing and purification center for mining of planets, planetoids, asteroids and comets. There also needs to be a fuels storage depot. This evokes the necessity of beginning the process of designing large mid-travel point fuels station. The make-up of such a craft should follow the modular designs model so that multiple crafts can be built and added upon over time. Of course, large crafts must account the fragility of structures as mass builds. Any structure has a "critical mass" threshold or limit, and a fuels station structure will see a grossly changing mass index. This should be ameliorated to an extent by careful mass off-set design principles.

Orbital Protocols
Design orbital regimes and create orbital protocols and integrate with Over-all Operations Protocol

Constant Operations Parameters
Requisites for sustained operations shall be integrated with Over-all Operations Protocol

       It is possible, in the future, to design a Satellite array which might supply focused energy for surface power generation.

Initial systems, Building and Growth
    Manufacturing is a prime focus for the first settlement. - Manufacturing, mining, machining and fabrication methods and systems are to be designed carefully.
Establish First Structures
    domiciles and workstations
    Power and Utilities
        Design initial power station and utilities and integrate with Over-all Operations Protocol.
        Process for water supply. - Water treatment units that accompany spacecraft will be designed for use on the planet to integrate into a larger water-systems scheme to feed the various “life-domes”, structures and work-stations.
        There should be careful management of water colors, white, gray, black, etc. These would be treated in the garden corridors. [Check plant pistil/pollen reproductive systems and growth rate on low gravity.] This system needs to be dynamically integrated into the overall recycling regime and with the energy & power systems. Solar to Hydrogen and Oxygen are initial goals.

It may be possible to build an extraordinarily high, by earth standards, landing and platform on Olympia Mons on Mars.The mountain is high because gravity-defined weight is low. Therefore, a wide base but very high platform could be
erected. With, perhaps an elevator.

Operations and Management
Define general operations and management systems and integrate with Over-all Operations Protocol
Resource Development
Design Transport and Living Quarters - See Exploration-Habitats
Create controlled centrifugal, integrated modular habitats design to accommodate space vehicles and planetary installations.

1): Design hexagonal cells, or other geometries for modular units that will disengage from their Earth-to-Mars vehicle, be transported by shuttle to the surface and then stack and ride in carrousels on a circular track, around the center access hub. Gondolas transport to and from living quarters to the center hub where people descend or ascend from tram tunnels under ground.

Life-domes are a covered carrousel of the hex living quarters that were the living quarters in the spacecraft and ride as a carrousel in the domes to create a faux-gravity - having had the same function on the inter-planetary spacecraft. These should be designed so that smaller domes will eventually become much larger units to take best advantage of the flywheel effect.
Figure angle of flooring to carrousels diameter for best weight to speed false-gravity effect.
Life-domes should covered with a skin that provides view and insulation. This could be a layered net. Viewing decks can be integrated.

Work Stations
Multiple and heavy-use, gravity units are, of course, separate from normal living quarters and must be so designed.
There should be trams that connect life-domes. These corridors will be modular and will also provide gardens and utilities runs for the modular and expandable recirculation life support system

Getting there


Engines can be assembled into configurations of two, three, four, five and six Vehicle Acceleration Rings.

Integrated Lander
   Skins shall be designed to absorb spurious charge and integrate to storage.

Note - Possible finance goal: Investment monies are to go to the actual space project - not inflated salaries. Everyone will work for subsistence wage but own stock. Shares are divided by investment, either in monies or effort.