Difference between revisions of "Landing large payloads on the Martian surface"
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| − | '''Landing large payloads on the Martian surface''' is needed for the construction of a base or colony. | + | '''Landing large payloads on the Martian surface'''<ref>https://en.wikipedia.org/wiki/Mars_atmospheric_entry</ref> is needed for the construction of a base or colony. |
This requires untested technologies. | This requires untested technologies. | ||
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| + | This subject is a subset of the [[Landing on Mars]] topic. | ||
Because Mars has a thin atmosphere it is possible to use it for aerobraking. However, the atmosphere is not thick enough to entirely stop a large re-entry vehicle of more than a few tonnes. As the vehicles velocity goes down, the aerodynamic forces are insufficient to sustain flight, and the vehicle crashes before it slows down enough for the use of parachutes. | Because Mars has a thin atmosphere it is possible to use it for aerobraking. However, the atmosphere is not thick enough to entirely stop a large re-entry vehicle of more than a few tonnes. As the vehicles velocity goes down, the aerodynamic forces are insufficient to sustain flight, and the vehicle crashes before it slows down enough for the use of parachutes. | ||
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| + | ==Supersonic Retro-Propulsive landing== | ||
| + | SpaceX and NASA have developed a concept called Supersonic retro-Propulsive Landing that is designed to bridge the gap between aerobraking and propulsive landing. It appears this was tested in the Earth's upper atmosphere during the re-entry of some of the SpaceX Falcon 9 vehicles<ref>https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20170008725.pdf</ref>. Retro propulsion in the supersonic flight regime is used to support and slow the vehicle until conventional retro propulsion can be used to land. SpaceX has demonstrated the capability of very precise landing using these methods on Earth, and these could be transposed to Mars. | ||
| + | This method could be used for landing payloads of 100 tonnes and more. | ||
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==Aeroshell landing== | ==Aeroshell landing== | ||
The Mars Science Laboratory used an aeroshell, parachutes and a rocket powered "skycrane" to land on Mars. This may be used to land medium sized payloads on Mars with great precision. Larger payloads are harder to land, but increasing the size of the aeroshell may help. An inflatable Rogallo wing made out of inconel wire and silicon rubber was considered as a manned rescue vehicle from LEO, and so was a system called [http://www.en.wikipedia.org/wiki/MOOSE MOOSE], using a foldable heatshield as a one-man escape system. Other system to be considered include high speed ballutes. | The Mars Science Laboratory used an aeroshell, parachutes and a rocket powered "skycrane" to land on Mars. This may be used to land medium sized payloads on Mars with great precision. Larger payloads are harder to land, but increasing the size of the aeroshell may help. An inflatable Rogallo wing made out of inconel wire and silicon rubber was considered as a manned rescue vehicle from LEO, and so was a system called [http://www.en.wikipedia.org/wiki/MOOSE MOOSE], using a foldable heatshield as a one-man escape system. Other system to be considered include high speed ballutes. | ||
| − | == Propulsive landing == | + | ==Propulsive landing== |
| − | If enough fuel is available in Low Mars Orbit then fully propulsive landing, as on the | + | If enough fuel is available in Low Mars Orbit then fully propulsive landing, as on the Moon, might be a possibility. |
==Space elevator== | ==Space elevator== | ||
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A space elevator could be used to drop payloads onto the martian surface. A cargo pallet docks with the counterweight, and slides down the the cable to the surface. A space elevator must be built at or near the equator, whereas the cargo might be needed thousands of kilometers away. [[Airship|Airships]] could be used for long distance transport. Construction of a space elevator may require many "conventional" landings on the surface and a large amount of infrastructure in space if it is to be feasible. Even if a space elevator is implausible to construct a colony in the first place, it might be useful in future. | A space elevator could be used to drop payloads onto the martian surface. A cargo pallet docks with the counterweight, and slides down the the cable to the surface. A space elevator must be built at or near the equator, whereas the cargo might be needed thousands of kilometers away. [[Airship|Airships]] could be used for long distance transport. Construction of a space elevator may require many "conventional" landings on the surface and a large amount of infrastructure in space if it is to be feasible. Even if a space elevator is implausible to construct a colony in the first place, it might be useful in future. | ||
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| + | ==References== | ||
[[Category:Settlement Transport Systems]] | [[Category:Settlement Transport Systems]] | ||
| + | <references /> | ||
Latest revision as of 10:59, 26 June 2023
Landing large payloads on the Martian surface[1] is needed for the construction of a base or colony. This requires untested technologies.
This subject is a subset of the Landing on Mars topic.
Because Mars has a thin atmosphere it is possible to use it for aerobraking. However, the atmosphere is not thick enough to entirely stop a large re-entry vehicle of more than a few tonnes. As the vehicles velocity goes down, the aerodynamic forces are insufficient to sustain flight, and the vehicle crashes before it slows down enough for the use of parachutes.
Contents
Supersonic Retro-Propulsive landing
SpaceX and NASA have developed a concept called Supersonic retro-Propulsive Landing that is designed to bridge the gap between aerobraking and propulsive landing. It appears this was tested in the Earth's upper atmosphere during the re-entry of some of the SpaceX Falcon 9 vehicles[2]. Retro propulsion in the supersonic flight regime is used to support and slow the vehicle until conventional retro propulsion can be used to land. SpaceX has demonstrated the capability of very precise landing using these methods on Earth, and these could be transposed to Mars. This method could be used for landing payloads of 100 tonnes and more.
Aeroshell landing
The Mars Science Laboratory used an aeroshell, parachutes and a rocket powered "skycrane" to land on Mars. This may be used to land medium sized payloads on Mars with great precision. Larger payloads are harder to land, but increasing the size of the aeroshell may help. An inflatable Rogallo wing made out of inconel wire and silicon rubber was considered as a manned rescue vehicle from LEO, and so was a system called MOOSE, using a foldable heatshield as a one-man escape system. Other system to be considered include high speed ballutes.
Propulsive landing
If enough fuel is available in Low Mars Orbit then fully propulsive landing, as on the Moon, might be a possibility.
Space elevator
Main article Space elevator
A space elevator could be used to drop payloads onto the martian surface. A cargo pallet docks with the counterweight, and slides down the the cable to the surface. A space elevator must be built at or near the equator, whereas the cargo might be needed thousands of kilometers away. Airships could be used for long distance transport. Construction of a space elevator may require many "conventional" landings on the surface and a large amount of infrastructure in space if it is to be feasible. Even if a space elevator is implausible to construct a colony in the first place, it might be useful in future.
