How to communicate with a lunar polar mission?












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We can easily communicate with a spacecraft on the Moon on the near side. The Far Side allows for a L2 halo communication relay satellite easily enough. How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.










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    $begingroup$


    We can easily communicate with a spacecraft on the Moon on the near side. The Far Side allows for a L2 halo communication relay satellite easily enough. How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.










    share|improve this question









    $endgroup$















      4












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      4





      $begingroup$


      We can easily communicate with a spacecraft on the Moon on the near side. The Far Side allows for a L2 halo communication relay satellite easily enough. How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.










      share|improve this question









      $endgroup$




      We can easily communicate with a spacecraft on the Moon on the near side. The Far Side allows for a L2 halo communication relay satellite easily enough. How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.







      the-moon communication lander






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      asked Jan 12 at 15:59









      PearsonArtPhotoPearsonArtPhoto

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          2 Answers
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          $begingroup$

          ESA's unimaginatively named Lunar Lander mission, sadly cancelled in 2012, was a south polar lunar mission. They planned to use line-of-sight communications and just accept the periodic periods of communication loss.




          Another mission constraint is the unavailability of an orbiter for communications
          relay. As a
          consequence, the potential landing site must have sufficient visibility of Earth
          to be able
          to send
          engineering and scientific data and to receive commands.This is generally achieved at the potential landing sites at the
          poles, where Earth visibility has a windows of approximately 14
          days, due to the fact that the Earth centre follows a pattern of
          approximately ±6.5° in elevation every months, constrained to
          approximately ±8° in azimuth.




          source






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            $begingroup$


            How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.




            A constellation of three or more evenly-spaced relay satellites (the higher they are, the fewer you need) in fairly high polar lunar orbit would be sufficient to maintain continuous contact with sites near either pole. No such constellation exists today but it should be straightforward to establish one. Shackleton might require a few more satellites in the constellation to ensure that one is always above the crater rim, if constant contact is required.






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              2 Answers
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              2 Answers
              2






              active

              oldest

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              active

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              $begingroup$

              ESA's unimaginatively named Lunar Lander mission, sadly cancelled in 2012, was a south polar lunar mission. They planned to use line-of-sight communications and just accept the periodic periods of communication loss.




              Another mission constraint is the unavailability of an orbiter for communications
              relay. As a
              consequence, the potential landing site must have sufficient visibility of Earth
              to be able
              to send
              engineering and scientific data and to receive commands.This is generally achieved at the potential landing sites at the
              poles, where Earth visibility has a windows of approximately 14
              days, due to the fact that the Earth centre follows a pattern of
              approximately ±6.5° in elevation every months, constrained to
              approximately ±8° in azimuth.




              source






              share|improve this answer









              $endgroup$


















                5












                $begingroup$

                ESA's unimaginatively named Lunar Lander mission, sadly cancelled in 2012, was a south polar lunar mission. They planned to use line-of-sight communications and just accept the periodic periods of communication loss.




                Another mission constraint is the unavailability of an orbiter for communications
                relay. As a
                consequence, the potential landing site must have sufficient visibility of Earth
                to be able
                to send
                engineering and scientific data and to receive commands.This is generally achieved at the potential landing sites at the
                poles, where Earth visibility has a windows of approximately 14
                days, due to the fact that the Earth centre follows a pattern of
                approximately ±6.5° in elevation every months, constrained to
                approximately ±8° in azimuth.




                source






                share|improve this answer









                $endgroup$
















                  5












                  5








                  5





                  $begingroup$

                  ESA's unimaginatively named Lunar Lander mission, sadly cancelled in 2012, was a south polar lunar mission. They planned to use line-of-sight communications and just accept the periodic periods of communication loss.




                  Another mission constraint is the unavailability of an orbiter for communications
                  relay. As a
                  consequence, the potential landing site must have sufficient visibility of Earth
                  to be able
                  to send
                  engineering and scientific data and to receive commands.This is generally achieved at the potential landing sites at the
                  poles, where Earth visibility has a windows of approximately 14
                  days, due to the fact that the Earth centre follows a pattern of
                  approximately ±6.5° in elevation every months, constrained to
                  approximately ±8° in azimuth.




                  source






                  share|improve this answer









                  $endgroup$



                  ESA's unimaginatively named Lunar Lander mission, sadly cancelled in 2012, was a south polar lunar mission. They planned to use line-of-sight communications and just accept the periodic periods of communication loss.




                  Another mission constraint is the unavailability of an orbiter for communications
                  relay. As a
                  consequence, the potential landing site must have sufficient visibility of Earth
                  to be able
                  to send
                  engineering and scientific data and to receive commands.This is generally achieved at the potential landing sites at the
                  poles, where Earth visibility has a windows of approximately 14
                  days, due to the fact that the Earth centre follows a pattern of
                  approximately ±6.5° in elevation every months, constrained to
                  approximately ±8° in azimuth.




                  source







                  share|improve this answer












                  share|improve this answer



                  share|improve this answer










                  answered Jan 12 at 16:33









                  Organic MarbleOrganic Marble

                  60k3165256




                  60k3165256























                      2












                      $begingroup$


                      How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.




                      A constellation of three or more evenly-spaced relay satellites (the higher they are, the fewer you need) in fairly high polar lunar orbit would be sufficient to maintain continuous contact with sites near either pole. No such constellation exists today but it should be straightforward to establish one. Shackleton might require a few more satellites in the constellation to ensure that one is always above the crater rim, if constant contact is required.






                      share|improve this answer











                      $endgroup$


















                        2












                        $begingroup$


                        How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.




                        A constellation of three or more evenly-spaced relay satellites (the higher they are, the fewer you need) in fairly high polar lunar orbit would be sufficient to maintain continuous contact with sites near either pole. No such constellation exists today but it should be straightforward to establish one. Shackleton might require a few more satellites in the constellation to ensure that one is always above the crater rim, if constant contact is required.






                        share|improve this answer











                        $endgroup$
















                          2












                          2








                          2





                          $begingroup$


                          How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.




                          A constellation of three or more evenly-spaced relay satellites (the higher they are, the fewer you need) in fairly high polar lunar orbit would be sufficient to maintain continuous contact with sites near either pole. No such constellation exists today but it should be straightforward to establish one. Shackleton might require a few more satellites in the constellation to ensure that one is always above the crater rim, if constant contact is required.






                          share|improve this answer











                          $endgroup$




                          How would a polar mission communicate with Earth, especially at a spot like the Shackleton crater? It seems like it would be difficult to see from Earth, and there isn't a convenient orbit like the L2 orbit.




                          A constellation of three or more evenly-spaced relay satellites (the higher they are, the fewer you need) in fairly high polar lunar orbit would be sufficient to maintain continuous contact with sites near either pole. No such constellation exists today but it should be straightforward to establish one. Shackleton might require a few more satellites in the constellation to ensure that one is always above the crater rim, if constant contact is required.







                          share|improve this answer














                          share|improve this answer



                          share|improve this answer








                          edited Jan 13 at 1:52

























                          answered Jan 12 at 20:20









                          Russell BorogoveRussell Borogove

                          89.3k3300384




                          89.3k3300384






























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