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what do we need to do before we send men back ?
A couple of things I came up with a An orbiter to map the Moon in detail especially the poles. Many areas of the Moon today are not mapped to 20 m resolution we can easily do 10m for the entire moon and 1-2m for selected portions. A follow on to Prospector getting a better idea of where the hydrogen is. A radar map to give us a picture at depth of the Moons surface. A couple of landers at potential base sites would be usefull. What did I miss in my quick list? |
#2
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"Dholmes" wrote in message .. .
what do we need to do before we send men back ? A couple of things I came up with a An orbiter to map the Moon in detail especially the poles. Many areas of the Moon today are not mapped to 20 m resolution we can easily do 10m for the entire moon and 1-2m for selected portions. A follow on to Prospector getting a better idea of where the hydrogen is. A radar map to give us a picture at depth of the Moons surface. A couple of landers at potential base sites would be usefull. What did I miss in my quick list? Development of: - Solar Electric tug to transport cargo from LEO to Lunar Orbit - Lunar chemistry kit, to extract Oxygen from lunar soils - Construction techniques appropriate to lunar conditions, e.g cut and cover - Edible plants that can grow in a lunar cycle - Cheap and easy (not neccessarily efficient) solar cells that can be manufactured on the moon or in space. - Virtual Reality controlled robots for work on the lunar surface, controlled in doors or even from Earth. - Remote controlled digging machines that can collect ores from the lunar surface |
#3
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![]() "Alex Terrell" wrote in message om... "Dholmes" wrote in message .. . what do we need to do before we send men back ? A couple of things I came up with a An orbiter to map the Moon in detail especially the poles. Many areas of the Moon today are not mapped to 20 m resolution we can easily do 10m for the entire moon and 1-2m for selected portions. A follow on to Prospector getting a better idea of where the hydrogen is. A radar map to give us a picture at depth of the Moons surface. A couple of landers at potential base sites would be usefull. What did I miss in my quick list? Development of: - Solar Electric tug to transport cargo from LEO to Lunar Orbit This seems more of a long term goal not prereturn. Personally I prefer Solar thermal. - Lunar chemistry kit, to extract Oxygen from lunar soils - Construction techniques appropriate to lunar conditions, e.g cut and cover Both very useful. - Edible plants that can grow in a lunar cycle I really do not see a need for this artificial lighting can easily supplement real light or even replace it. - Cheap and easy (not neccessarily efficient) solar cells that can be manufactured on the moon or in space. Again very useful longterm but seems more of a later item. - Virtual Reality controlled robots for work on the lunar surface, controlled in doors or even from Earth. - Remote controlled digging machines that can collect ores from the lunar surface Both useful a simple brick making device may be useful as well. |
#4
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Dholmes wrote:
I really do not see a need for this artificial lighting can easily supplement real light or even replace it. There is no way you can grow plants for any practical purpose (e.g. food) with artificial light. To grow 1 acre (10000 m²) you would need 14 MW power - which means at least a nuclear fission reactor, which Greenpeace would never allow to be launched from Earth. It is perhaps more than anything else the question of growing plants that make Mars a much more favorable destination than the Moon, because of its 24 hour day. -- Steen Eiler Jørgensen "Time has resumed its shape. All is as it was before. Many such journeys are possible. Let me be your gateway." |
#5
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![]() "Steen Eiler Jørgensen" wrote in message . .. Dholmes wrote: I really do not see a need for this artificial lighting can easily supplement real light or even replace it. There is no way you can grow plants for any practical purpose (e.g. food) with artificial light. To grow 1 acre (10000 m²) you would need 14 MW power - which means at least a nuclear fission reactor, which Greenpeace would never allow to be launched from Earth. Last time I checked with hydroponics it took to grow the vast majority of the required food less then 10 kw per person . So 14 MW supplemented with some real light plus a little meat and luxuries from Earth would support 2000+ people. I do not see a Lunar base approaching 2000 people for a long time. It is perhaps more than anything else the question of growing plants that make Mars a much more favorable destination than the Moon, because of its 24 hour day. For a colony I would agree but for a base I do not. |
#6
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Last time I checked with hydroponics it took to grow the vast majority of
the required food less then 10 kw per person . So 14 MW supplemented with some real light plus a little meat and luxuries from Earth would support 2000+ people. I do not see a Lunar base approaching 2000 people for a long time. I heard they grow canabis plants under grow lights in Canada, so they can't be spotted from the air. If it can be done on the Earth, it can be done on the Moon. Tom |
#7
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Dholmes wrote:
There is no way you can grow plants for any practical purpose (e.g. food) with artificial light. To grow 1 acre (10000 m²) you would need 14 MW power - which means at least a nuclear fission reactor, which Greenpeace would never allow to be launched from Earth. Last time I checked with hydroponics it took to grow the vast majority of the required food less then 10 kw per person . Yeah, his figures are off by a factor or three. People grow huge farms of illegal drugs inside their houses with heatlamps and hydroponics. |
#8
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JRS: In article , seen in
news:sci.space.policy, Steen Eiler Jørgensen posted at Sun, 16 Nov 2003 14:29:58 :- There is no way you can grow plants for any practical purpose (e.g. food) with artificial light. To grow 1 acre (10000 m²) you would need 14 MW power - which means at least a nuclear fission reactor, which Greenpeace would never allow to be launched from Earth. 10000m^2 is a hectare, not an acre, which is 4840 square yards; 1 ha = 2.471 acres. Stick to SI units; let those who only understand Imperial units make their own mistakes. Granted, Danish acres might be bigger than ours. You can halve that power, since plants are used to night and day; and reduce it further, to allow for angle-of-incidence and for clouds. You can halve it again, if power can be stored until night and the plants can use real sunlight or light from solar power during the lit fortnight. -- © John Stockton, Surrey, UK. / © Web URL:http://www.merlyn.demon.co.uk/ - FAQish topics, acronyms, & links. Correct = 4-line sig. separator as above, a line precisely "-- " (SoRFC1036) Do not Mail News to me. Before a reply, quote with "" or " " (SoRFC1036) |
#9
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Dr John Stockton wrote:
10000m^2 is a hectare, not an acre, which is 4840 square yards; 1 ha = 2.471 acres. Stick to SI units; let those who only understand Imperial units make their own mistakes. Granted, Danish acres might be bigger than ours. Oops. I'm sorry - my mistake. I thought 'acre' was english for 'hektar'. Thanks for clearing this up. And no - Danish acres aren't bigger than yours ;-) You can halve that power, since plants are used to night and day; and reduce it further, to allow for angle-of-incidence and for clouds. Well, true. You can halve it again, if power can be stored until night and the plants can use real sunlight or light from solar power during the lit fortnight. Well, in principle, you're right. *If* you can store that much energy without much loss for 14 days, *then* it's not an energy issue any longer. But still, technically, t's just a lot easier on Mars ![]() -- Steen Eiler Jørgensen "Time has resumed its shape. All is as it was before. Many such journeys are possible. Let me be your gateway." |
#10
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Dholmes wrote:
What did I miss in my quick list? Development of a communications relay satellite in a halo orbit around the L2 Lagrange point in the Earth-Moon-system, providing a communications link to the far side of the Moon. From http://www.tsgc.utexas.edu/archive/design/farside.html "During the construction phase, a satellite in an L2 halo orbit will relay data from the lunar surface to a geostationary satellite in Earth orbit to the Earth's surface. When the base becomes fully operational, however, a radio-free sky is desired to take accurate astronomical readings. Therefore, a fiber optic cable will be used as a communication link from the base to a transmitter/receiver station on the near side of the Moon. It will be laid out by a robotic rover from the base to the limb of the Moon. From there, the signal can be broadcasted directly to Earth without interfering with astronomical observations." From http://www.tsgc.utexas.edu/archive/design/farside2.html "To provide constant communication with the lunar nearside base as well as Earth, a communication system was devised where the relaying point is a satellite in a halo orbit about the L2 unstable libration point. This would permit full coverage of the lunar farside and the constant monitoring of the construction activities being conducted. Since L2 is an unstable libration point, stationkeeping burns totaling 93.3 fps/yr and period control burns totaling 240 fps/yr will have to be conducted in order to maintain the orbit. After three years, the satellite at L2 will be refueled and moved to the stable libration point L5, where it will remain throughout the lifetime of the observatory." From http://adsabs.harvard.edu/cgi-bin/np...TIN...9512644B "Project ECHO: Electronic Communications from Halo Orbit - Abstract: The design of a communications relay to provide constant access between the Earth and the far side of the Moon is presented. Placement of the relay in a halo orbit about the L2 Earth-Moon Lagrange point allows the satellite to maintain constant simultaneous communication between Earth and scientific payloads on the far side of the Moon. The requirements of NASA's Discovery-class missions adopted and modified for this design a total project cost should not exceed $150 million excluding launch costs, launch must be provided by Delta-class vehicle, and the satellite should maintain an operational lifetime of 10 to 15 years. The spacecraft will follow a transfer trajectory to the L2 point, after launch by a Delta II 7925 vehicle in 1999. Low-level thrust is used for injection into a stationkeeping-free halo orbit once the spacecraft reaches the L2 point. The shape of this halo orbit is highly elliptical with the maximum excursion from the L2 point being 35000 km. A spun section and despun section connected through a bearing and power transfer assembly (BAPTA) compose the structure of the spacecraft. Communications equipment is placed on the despun section to provide for a stationary dual parabolic offset-feed array antenna system. The dual system is necessary to provide communications coverage during portions of maximum excursion on the halo orbit. Transmissions to the NASA Deep Space Network 34 m antenna include six channels (color video, two voice, scientific data from lunar payloads, satellite housekeeping and telemetry and uplinked commands) using the S- and X-bands. Four radioisotope thermoelectric generators (RTG's) provide a total of 1360 W to power onboard systems and any two of the four Hughes 13 cm ion thrusters at once. Output of the ion thrusters is approximately 17.8 mN each with xenon as the propellant. Presence of torques generated by solar pressure on the antenna dish require the addition of a 'skirt' extending from the spun section of the satellite for balance. Total mass of the satellite is approximately 900 kg at a cost of $130 million FY99." I wasn't able to find a suitable illustration on the web, so I scanned an illustration (it's a very rough sketch!) from a book I have ("Voyage through the Universe - Spacefarers", Time-Life Books 1989, Danish ed., pp. 58-59): http://www.dsri.dk/~sej/pics/lunar_halo_orbit.jpg -- Steen Eiler Jørgensen "Time has resumed its shape. All is as it was before. Many such journeys are possible. Let me be your gateway." |
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