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Is there a need to hasten the exploration of the Mars?

You can read the original text (in GOOGLE’s translation) on the site http://clubideas.ru/  

 

   To form atmosphere of the Red Planet it’s suggested to build factories producing artificial greenhouse gases. Robert Zubrin and Chris Mckay assume that it should be perfluoromethane (CF4). In his recently published book “Entering Space”  Zubrin states if this gas is produced and emitted on the Mars with the same speed as such gases are produced on the Earth (about 1000t an hour), the average temperature on the Red Planet could increase by 10°С in some decades. Such warming would cause the occurrence of a great deal of carbonic acid gas, which is greenhouse gas and could warm this planet in the future. The increased volume of water vapor in the atmosphere also could make it warmer. It could be possible to enhance these effects by using methanogens and bacteria, producing ammonium, as both methane and ammonium are also referred to the category of greenhouse gases. http://galspace.spb.ru/index38-1.html

 
 
 

    

The piloted flight to the Mars will be probably made far in the future, but enthusiasts face remote future and resolve how to adapt this planet to comfortable habitation of a human. It is predicted that the Mars will probably change already in some decades after the first human visiting.

 I don’t wish engaging in controversy against anybody about this topic, considering there should exist different points of view on  such important issue as the colonization of planets, I would like to express my opinion on the methods of the Mars’s exploration. I also share the opinion, that not to allow doing irreversible harm it will be hardly right to change other worlds as you wish, if you don’t have sufficient experience in saving your own environment.   

The piloted flight to the Mars will be probably made far in the future, but enthusiasts face remote future and resolve how to adapt this planet to comfortable habitation of a human. It is predicted that the Mars will probably change already in some decades after the first human visiting.

 I don’t wish engaging in controversy against anybody about this topic, considering there should exist different points of view on  such important issue as the colonization of planets, I would like to express my opinion on the methods of the Mars’s exploration. I also share the opinion, that not to allow doing irreversible harm it will be hardly right to change other worlds as you wish, if you don’t have sufficient experience in saving your own environment.

The line of the quotation reads as follows: “Such warming would cause the occurrence of a great deal of carbonic acid gas, which is greenhouse gas and could warm this planet in the future”. Taking into account that the level of carbonic acid gas in the Mars’s atmosphere is already more than 95 %, it becomes clear that it is dealing with the increasing of atmospheric pressure because of the evaporation of polar caps. As the gravitational field of the Mars cannot hold more compact atmosphere than existing one, its atmosphere can disappear in the environment. It turns out, that it’s a closed process. If substance disappears, weight shrinks. If weight shrinks, disappearance of substance is occurring more quickly. The planet cannot turn into nothing, but a great part of that, what was preserved as permafrost and polar caps, can simply evaporate in some centuries. Everything will depend on the intensity of our activities. In fact our civilization has exists on the Earth for about five millenia, and how long our descendants will still exist, the heavens only knows. I think, it is at least senseless to spray substance in space which we are not capable to use effectively now.

Here is the next topic. The banal question whether there is life on the Mars, has not been answered yet. I am not sure but we are mistaken that we try to find the life on the Mars which is similar to the Earth’s life: bacteria, waterweeds etc.

It can be something, what is carbon and organic, reproduces itself, lives on something and secretes something during its vital activity. Let’s imagine, if life exists on the Mars, it is not less unique, than the earth’s life and is perfectly adapted to existing conditions. Living beings may be adapted worse, we will not find out it in time. The life exists, but we don’t now its occurrence , or it does not exist, but there are intelligent beings, unalive intelligent creatures, perceiving itself, although it’s still unlikely. I understand that I’ve exaggerated, but it is acceptable in our club, in fact there are man-made computers on the Earth, and we are speaking about actually not studied world. 

How will these potential creatures respond to the change of temperature, pressure, oxygen and other pollution?

If we (I mean the mankind) as used to say in the USSR, aspire to gain the space by the way, we should not spend money on the factories of methane production and wait for warming for a long time. It is possible to evaporate cheaply enough and quickly ice caps of the Mars by bombing them with already available thermonuclear charges, although it would be better to do this with helium shells, which don’t exist now. Thus it will probably be possible to walk on the Mars in oxygen masks for a time and with Geiger-Mueller counter during several first years (revise “Total Recall“).

We can specify the ways of creation of living environment on the Mars’s and all the possible consequences of not considered actions, but professional ecologists can do it better, although it is quite evident, that the problem already exists and it should be solved.

I also have decided to share with some ideas concerning this topic.

The answer of the question, what we should do for that our stay on the Mars will be environmentally safe, is simple, we should not pollute it.

It is also clear, that the main pollution agent on the Mars will be none other than people and their life-support systems.

Therefore the following issue arises. Is there a need to hasten the exploration of the Mars? (I mean a flight of a man to the Mars and landing it). Taking into account that the majority of accidents occurs right during starting and landing of spacecrafts, I think, there is no necessity to risk the life of a man in spite of political advantages of this action, which a nation or a state could gain.

I am sure the Mars’s exploration should start with the setting up an orbital station with people on the Mars for a long period. At the first only robots should land the Mars.  During several first years of in-depth study of the Mars robots generally should land it. Too much additional equipment and material are required to provide necessary conditions for life of any Earth’s being on a lifeless planet.

When mineral resources aren’t explored, the planet landing of a man is waste of money. Using of robots is another matter, they are capable to bear multiple overloads, testing safety of the shuttles to the Mars in a mode of economic landing. They have sufficient intelligence and are controlled on-line from an orbit.  They will conduct geological survey, build flight strips and roads, gain oxygen and water for orbital station.                                         

If the answer of the question, whether we are necessary there, is positive, they will

construct hermetical working and accommodation premises with life-support systems from the delivered blocks.

The station, which detailed exploration of the Mars will be carried out at this time on, will be supplied with a system of artificial gravity of centrifugal mode. The start mode of a carrier is described in the previous article “What can one fly in the solar system by?” http://clubideas.ru/space flights/space flights.htm  

In this article I would like to touches in greater detail upon shuttles, namely jet engines and parachute braking system, what they should be to minimize the impact on environment.

Even in the deepest hollows of the Mars where the pressure of atmosphere is the highest, it is less approximately 100 times, than near the Earth’s surface. 

On the Earth such pressure is at height of over 30 000 meters above sea level.

None of high-altitude airplanes as SR-71 “BlackBird”, М-55 “Geofizika”, “Lockheed U-2” flies so high and those, which fly above 26500 meters, I cannot call airplanes. You should be a true optimist as our animation artist, which represented the movements of a shuttle, designed for the flights to the Mars (watch the video). However a railway car can hypothetically be placed in the Earth’s orbit if a launcher has sufficient capacity by the way in the horizontal position and without shrouds. We only have deal with the Mars where gravitational acceleration on the planet surface is g = 3,72 m/c2 in all. It is almost three times less than on the Earth.

Thus it is possible to fly above the Mars’s surface, but rather low and at high speed to achieve a high level of lifting power. It makes an advantage that low atmospheric density means low aerodynamic load. The most important is that it isn’t necessary to speed up a spacecraft to the first space velocity on the Mars for its placement on the orbit.  

Now let’s come back to shuttles. Here is the information, which I found in a polytechnic dictionary.

Space aircraft is a kind of the piloted jet aircraft with a carrying plane (in particular, winged aircraft), designed for flight in atmosphere and in the space. It combines the properties of an airplane and a space vehicle; designed for multiple usage; takes off from an airfield; accelerates to space velocity; makes flight in the space and returns landing an airfield. The basic purpose of a space aircraft is service of piloted orbital stations and crew-exchange. Multiple usage of a space aircraft provides its greater efficiency and cost effectiveness in comparison with modern launchers. The combination of an air-jet engine (for a flight in the atmosphere) and liquid engine (for a flight in the space) is suggested as an engine unit. The issues of designing space aircraft are studied and special projects are developed.

In general I find this information excellent except data on an air-jet engine of this aircraft, because propulsive power of a turbojet engine during the flight in stratosphere at height of 20-25 km reduces to 3% of propulsive power of an engine, being on the Earth, because of decreasing of air density. The Mars’s "stratosphere" starts directly with a surface and parameters of propulsive power will be even worse.

I was looking for more information and have found the following.

 

                                                     Fig.1

AIR-JET ENGINE is a mixed jet engine, which combines cycles of air-jet and rocket engines. The engines, which the cycles of straight-jet engine and liquid engine occur in, are called rocket-ramjet engines (see fig 1). Air-jet engine can probably used as air-space vehicle’s one.

 

Rocket-ramjet engine configuration: 1-an air inlet; 2 – a burner unit; 3 – an exhaust nozzle; 4 – an atomizer of additional fuel injection; 5 – an afterburner.

 

It turns out everything has already invented, it’s possible to dispense with turbines, but the problem is that ducted jet engine is started at the speeds exceeding the sound speed 1,5-2 times and is effective only at higher supersonic speeds. It means to the shuttle on the Mars should start right from place by means of rocket elements of its engines and accelerators. There is one more disadvantage. The atmosphere of the Mars does not contain some oxygen that is why atomizing nozzles of additional fuel injection (see fig.1) will be absolutely useless if, for example, liquid or powder magnesium is not certainly used as fuel. As we speak about ecological exploration of the Mars, we even do not consider using such kinds of fuel. In the least at the speed of 0 a rocket engine, being a part of mixed jet engine will run as an ejector of atmospheric air. I would like to enhance right this effect. In the conditions of such poor quantity of molecules per a volume unit it is not enough to pump air. It should be warmed up regularly to increase the coefficient of efficiency of its running.

To divide in layers and to heat one-by-one is necessary for an equal warming up of atmospheric gases, the rest of the things is almost similar to a straight-jet engine. Ram air is first compressed due to kinetic energy, then warms up not during fuel consumption but in jets, for example, in jets of electrothermal jet engine and performs useful effect, pouring out through a nozzle.

The result is the following (see fig.2-4). The forepart of the case of an engine is also a supersonic air inlet as in the scheme at fig. 1. Rocket engines have the form of rings (see fig.5), the scheme of the arrangement is cascade, i.e. the previous engine pumps and warms up atmospheric air for the following one. If it is necessary nozzles can move along axes of an engine, changing a compression degree of see in such a way (see fig.3).

   

Fig. 2 

 

Fig. 3 

 

Fig. 4

 

Fig. 5 

Fig. 6

 If such engine has been developed one day, the ring of an engine most likely will consist of separate sectors.

It is known, that metals stretch well and compress badly, regarding these properties such design has essential disadvantages. Internal wall will not only compress, it will also overheat. On fig.6 heating and mechanical effects on the walls of a burner unit and a nozzle are marked with color arrows. Stop. In my opinion we are very fascinated with that. Let’s not go into detailed description of the design, leave it for the following pages and continue.

What fuel should environmentally safe Martian engine burn? 

As there is a lot of carbonic acid gas and water on the Mars, an exhaust of jet engines should contain the same substances. To achieve that fuel, oxidizing agents and their components have to be brought from the Earth at least in the beginning.

If the article “http://galspace.spb.ru/index38-1.html “ is true , Russian scientists suggested a fine idea to use an electrothermal jet engine on the Mars. It is even better than a liquid propellant jet engine. Its specific impulse makes more than 10 km/s, what exceeds twice the properties of a liquid propellant jet engine, burning hydrogen fuel. There is an essential difference in a burner unit, but namely in that it is unavailable. It is possible to use either liquid carbon dioxide or water as a control agent. It seems, everything agrees, but it is nothing of the kind. The following issue appears right after the solution of the previous one. This issue lies in how to produce a great volume electric energy for the electrothermal engine of an aircraft.

The installation of a nuclear reactor at the station and on the planet surface, but a nuclear reactor on an aircraft is too much.

Ultralight accumulators will probably be invented in 30 years, but to my mind ultracapacious condensers with the internal resistance will be used, which will produce power portionwise. This information is the topic for another article. If there is anybody, who wishes to cover the issue professionally, please, you are welcome, join us.

There is one more variant. It comprises the using a nuclear rocket engine which was invented very long time ago and most likely there are its environmentally safe prototypes nowadays.

Fig.7

NUCLEAR ROCKET ENGINE is a rocket engine, where an energy source is nuclear fuel. In an nuclear rocket engine with a nuclear reactor a nuclear chain reaction produces heat, being transferred to a control agent (for example, to hydrogen). The active zone of a nuclear reactor can be solid phasic, LIQUID or gas phasic. A rocket with a nuclear rocket engine can achieve essentially greater speed of discharging than a rocket with a chemical rocket engine with significant motive power. Radioisotope rocket engine runs due to the energy of radioactive disintegration. (see fig.7)

Fig.7 Key scheme of an nuclear rocket engine: 1 - a tank with liquid hydrogen; 2 - a pump; 3 - a turbine; 4 – units, releasing heat; 5 – discharging of gases from the turbine; 6- a nozzle; 7 – control cores; 8 - protective shield

 

Such information I found in an old polytechnic dictionary. Two issues still remain unclear for me, whether it will be possible to gather sufficient volume of radioactive substance for maintenance of nuclear reaction in ring section of the engine and how the replacement of liquid hydrogen by liquefied carbonic acid gas will influence technical characteristics of an engine.

 Let’s imagine: So we, namely, robots have taken off from the Mars. Their taking off was environmentally safe. They have brought water, samples (for example, soil samples), oxygen etc. to the station and then they have returned to the Mars. The return in its turn also was environmentally safety.  

 In general the technology of shuttle landing is enough developed on the Earth and there is nothing special to add, besides the speed of a shuttle regarding to the Mars’s surface will be less, and vacuum degree of the atmosphere – higher. Therefore the Martian shuttle should have very long wings, changeable structure of wings, and in my opinion the design of a fuselage, used for delivery of cargoes to the planet surface, should be similar more likely to a transport airplane like “АН-8” or “АН-12” rather than “Buran”. There are evident advantages of such design in loading or unloading under gravitation and without special facilities. As we dream, I have one more wish, because of a number of reasons it would be better if a shuttle  can take off and land vertically even with reduced service load.

Thus in context of special characteristics of the design of the Martian shuttle access to the mode of controlled brakeage differs a little bit from its Earth’s prototype. It will remind more likely pitching, up to six kilometer height above a surface. Why up to this height? Everything is very simple, in 1976 American "Viking" opened the parachute at this height and I didn’t think over and believed American experience as landing was successful. I am probably mistaken, but winged aircrafts on the Mars if those appear some time, will fly not over 1-1,5 km above a surface. Therefore to make a shuttle fly horizontally there are approximately 4 km above the surface. Considering the speed of shuttle falling there is too little time, that’s why the Heavens requested do this movement, using parachutes. Why not, if the atmosphere is vacuum. Moreover parachutes (see fig.) can change canopy surface and have the mechanism of automatic packing. This last property is important for the robotized exploration of the Mars.

I bring to your notice "comics" on the theme of the running of self-packing parachute system.

 

A container with a parachute has such a position when a shuttle enters in the dense atmosphere. 

If we wish to get automatically packing parachute, we should forget about the pulling a canopy from a container by means of an auxiliary parachute. We will blow up a canopy by compressed air.

 

Теперь когда все стропы подтянуты прежде чем втянуть укладчик в контейнер воздух следует удалить.

  In our video we managed to present main special characteristics of a shuttle landing the Mars in spite of strong saving the time.

 Well, that is for this time. I think I should stop at “parachutes”. It is impossible to cover all the interesting facts dealing with the exploration of another planet, on one web-page, but we will try to come back to this topic again and again. We also propose you, our dear colleagues, to participate in the development of new projects.

                                                                                                                            

                                                                                                                                           GSG