Difference between revisions of "Luna and Mars Characteristics"

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| ''Atmosphere'' || vacuum || 0.1 psi Carbondioxide  
 
| ''Atmosphere'' || vacuum || 0.1 psi Carbondioxide  
 
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| Advantages || no barrier to high speed travel __ allows use of structural materials incompatible with oxygen and water __ no barier to observations __ no wind born dust __ no requirement for structures to withstand weather  || convenient source of carbon & oxygen __ allows use of aerobraking and other aerodynamic effects __ protects against staticly levitated dust and most meteors  
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| Advantages || no barrier to high speed travel __ allows use of structural materials incompatible with oxygen and water __ no barier to observations __ no wind born dust __ no requirement for structures to withstand weather  || convenient source of carbon & oxygen __ allows use of aerobraking and other aerodynamic effects __ protects against electrostaticly levitated dust and most meteors  
 
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| Disadvantages || leads to dewetting of lubricated surfaces __ can not be breathed by people or internal combustion engines __ requires space suit protection of people __ requires pressure chambers for industrial processing involving most liquids __ requires pressure chambers for industrial collection of gas __ no protection against micrometeoroids or staticly levitated dust || can not be breathed by people or internal combustion engines __ requires about the same suit protection of people as a vacuum __ requires pressure chambers for industrial processing involving most liquids __ blows dust storms __ interferes with observations __ requires structural considerations to deal with weather __ does not permit electrical acceleration to orbital velocity
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| Disadvantages || leads to dewetting of lubricated surfaces __ can not be breathed by people or internal combustion engines __ requires space suit protection of people __ requires pressure chambers for industrial processing involving most liquids __ requires pressure chambers for industrial collection of gas __ no protection against micrometeoroids or electrostaticly levitated dust || can not be breathed by people or internal combustion engines __ requires about the same suit protection of people as a vacuum __ requires pressure chambers for industrial processing involving most liquids __ blows dust storms __ interferes with observations __ requires structural considerations to deal with weather __ does not permit electrical acceleration to orbital velocity
 
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| ''Gravity'' || 1.62 meters per second squared || 3.66 meters per second squared  
 
| ''Gravity'' || 1.62 meters per second squared || 3.66 meters per second squared  

Revision as of 02:43, 10 October 2008

Luna's and Mars' Characteristics
Quality Luna Mars
Atmosphere vacuum 0.1 psi Carbondioxide
Advantages no barrier to high speed travel __ allows use of structural materials incompatible with oxygen and water __ no barier to observations __ no wind born dust __ no requirement for structures to withstand weather convenient source of carbon & oxygen __ allows use of aerobraking and other aerodynamic effects __ protects against electrostaticly levitated dust and most meteors
Disadvantages leads to dewetting of lubricated surfaces __ can not be breathed by people or internal combustion engines __ requires space suit protection of people __ requires pressure chambers for industrial processing involving most liquids __ requires pressure chambers for industrial collection of gas __ no protection against micrometeoroids or electrostaticly levitated dust can not be breathed by people or internal combustion engines __ requires about the same suit protection of people as a vacuum __ requires pressure chambers for industrial processing involving most liquids __ blows dust storms __ interferes with observations __ requires structural considerations to deal with weather __ does not permit electrical acceleration to orbital velocity
Gravity 1.62 meters per second squared 3.66 meters per second squared
Advantages lower loading on structures to resist gravity than on Mars __ 04.7% of energy needed to orbit Earth can get to lunar orbit lower loading on structures to resist gravity than on Earth __ 20% of energy needed to orbit Earth can get to Mars orbit
Disadvantages lunar gravity may be insufficient to maintain human health __ low gravity causes problems with low traction for construction work Mars gravity may be insufficient to maintain human health __ low gravity causes problems with low traction for construction work
Round Trip Communications Delay 2.56 seconds about 23 minutes average, about 540 times the delay for Luna