Why was it necessary to program InSight with an ability to land in dust storms?











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If the entire event of EDL (Entry - Descent - Landing) is going to take only 7 minutes and if the command to begin could be signalled based on ground weather conditions, why was it necessary to take the extra effort to program the capability to land in dust storms?



Why not make use of dynamic weather monitoring and only initiate entry when the conditions are perfect?










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    up vote
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    down vote

    favorite
    1












    If the entire event of EDL (Entry - Descent - Landing) is going to take only 7 minutes and if the command to begin could be signalled based on ground weather conditions, why was it necessary to take the extra effort to program the capability to land in dust storms?



    Why not make use of dynamic weather monitoring and only initiate entry when the conditions are perfect?










    share|improve this question


























      up vote
      35
      down vote

      favorite
      1









      up vote
      35
      down vote

      favorite
      1






      1





      If the entire event of EDL (Entry - Descent - Landing) is going to take only 7 minutes and if the command to begin could be signalled based on ground weather conditions, why was it necessary to take the extra effort to program the capability to land in dust storms?



      Why not make use of dynamic weather monitoring and only initiate entry when the conditions are perfect?










      share|improve this question















      If the entire event of EDL (Entry - Descent - Landing) is going to take only 7 minutes and if the command to begin could be signalled based on ground weather conditions, why was it necessary to take the extra effort to program the capability to land in dust storms?



      Why not make use of dynamic weather monitoring and only initiate entry when the conditions are perfect?







      mars nasa landing insight entry-descent-landing






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      edited Nov 28 at 22:13

























      asked Nov 26 at 17:15









      karthikeyan

      1,296923




      1,296923






















          3 Answers
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          active

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          up vote
          89
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          accepted










          Because it's at the end of a 6 month cruise and there's no turning back.



          InSight will not enter closed orbit around Mars - its trajectory is hyperbolic so either it misses Mars entirely or it enters the atmosphere.



          There were six planned course corrections during the cruise phase, the final one of which - TCM 6 - occurred on the day of the landing. This was to precisely target the landing site and would have made very little difference to the entry time - certainly not enough to wait out a dust storm.






          share|improve this answer






























            up vote
            32
            down vote













            InSight doesn't enter Martian orbit before EDL; it plows straight into Mars' atmosphere from interplanetary space. Thus, the time of landing is pretty much un-alterable after its final midcourse correction maneuvers; it cannot wait for perfect weather conditions to land.






            share|improve this answer




























              up vote
              8
              down vote













              To deal with dust storms, two of the changes between Phoenix and InSight are mechanical in nature:





              • InSight uses a thicker heat shield, partly to handle the possibility of being sandblasted by a dust storm.


              • InSight’s parachute suspension lines use stronger material.



              https://mars.nasa.gov/insight/timeline/landing/entry-descent-landing/




              The landing site needs to be both flat and level, and reconnaissance helped to choose the optimal site. Nonetheless, there still could be boulders or small hills that should be avoided. Therefore, there are cameras and radar that help the computer decide the best place for landing, and thrust appropriately. These cameras and radar can be blinded by dust storms.






              share|improve this answer





















              • Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                – Wayne Conrad
                Nov 26 at 20:34






              • 3




                @WayneConrad: All 3 reasons contributed to the design change.
                – Dr Sheldon
                Nov 26 at 20:36






              • 7




                +1 for the how, but it actually misses the question of why.
                – DarkDust
                Nov 26 at 20:59






              • 2




                @WayneConrad: The wind, not the dust itself.
                – Dr Sheldon
                Nov 27 at 14:09






              • 6




                No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                – Wayne Conrad
                Nov 27 at 16:42











              Your Answer





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              3 Answers
              3






              active

              oldest

              votes








              3 Answers
              3






              active

              oldest

              votes









              active

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              votes






              active

              oldest

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              up vote
              89
              down vote



              accepted










              Because it's at the end of a 6 month cruise and there's no turning back.



              InSight will not enter closed orbit around Mars - its trajectory is hyperbolic so either it misses Mars entirely or it enters the atmosphere.



              There were six planned course corrections during the cruise phase, the final one of which - TCM 6 - occurred on the day of the landing. This was to precisely target the landing site and would have made very little difference to the entry time - certainly not enough to wait out a dust storm.






              share|improve this answer



























                up vote
                89
                down vote



                accepted










                Because it's at the end of a 6 month cruise and there's no turning back.



                InSight will not enter closed orbit around Mars - its trajectory is hyperbolic so either it misses Mars entirely or it enters the atmosphere.



                There were six planned course corrections during the cruise phase, the final one of which - TCM 6 - occurred on the day of the landing. This was to precisely target the landing site and would have made very little difference to the entry time - certainly not enough to wait out a dust storm.






                share|improve this answer

























                  up vote
                  89
                  down vote



                  accepted







                  up vote
                  89
                  down vote



                  accepted






                  Because it's at the end of a 6 month cruise and there's no turning back.



                  InSight will not enter closed orbit around Mars - its trajectory is hyperbolic so either it misses Mars entirely or it enters the atmosphere.



                  There were six planned course corrections during the cruise phase, the final one of which - TCM 6 - occurred on the day of the landing. This was to precisely target the landing site and would have made very little difference to the entry time - certainly not enough to wait out a dust storm.






                  share|improve this answer














                  Because it's at the end of a 6 month cruise and there's no turning back.



                  InSight will not enter closed orbit around Mars - its trajectory is hyperbolic so either it misses Mars entirely or it enters the atmosphere.



                  There were six planned course corrections during the cruise phase, the final one of which - TCM 6 - occurred on the day of the landing. This was to precisely target the landing site and would have made very little difference to the entry time - certainly not enough to wait out a dust storm.







                  share|improve this answer














                  share|improve this answer



                  share|improve this answer








                  edited Nov 26 at 22:33

























                  answered Nov 26 at 17:54









                  Jack

                  7,35013152




                  7,35013152






















                      up vote
                      32
                      down vote













                      InSight doesn't enter Martian orbit before EDL; it plows straight into Mars' atmosphere from interplanetary space. Thus, the time of landing is pretty much un-alterable after its final midcourse correction maneuvers; it cannot wait for perfect weather conditions to land.






                      share|improve this answer

























                        up vote
                        32
                        down vote













                        InSight doesn't enter Martian orbit before EDL; it plows straight into Mars' atmosphere from interplanetary space. Thus, the time of landing is pretty much un-alterable after its final midcourse correction maneuvers; it cannot wait for perfect weather conditions to land.






                        share|improve this answer























                          up vote
                          32
                          down vote










                          up vote
                          32
                          down vote









                          InSight doesn't enter Martian orbit before EDL; it plows straight into Mars' atmosphere from interplanetary space. Thus, the time of landing is pretty much un-alterable after its final midcourse correction maneuvers; it cannot wait for perfect weather conditions to land.






                          share|improve this answer












                          InSight doesn't enter Martian orbit before EDL; it plows straight into Mars' atmosphere from interplanetary space. Thus, the time of landing is pretty much un-alterable after its final midcourse correction maneuvers; it cannot wait for perfect weather conditions to land.







                          share|improve this answer












                          share|improve this answer



                          share|improve this answer










                          answered Nov 26 at 17:53









                          Russell Borogove

                          79.3k2261347




                          79.3k2261347






















                              up vote
                              8
                              down vote













                              To deal with dust storms, two of the changes between Phoenix and InSight are mechanical in nature:





                              • InSight uses a thicker heat shield, partly to handle the possibility of being sandblasted by a dust storm.


                              • InSight’s parachute suspension lines use stronger material.



                              https://mars.nasa.gov/insight/timeline/landing/entry-descent-landing/




                              The landing site needs to be both flat and level, and reconnaissance helped to choose the optimal site. Nonetheless, there still could be boulders or small hills that should be avoided. Therefore, there are cameras and radar that help the computer decide the best place for landing, and thrust appropriately. These cameras and radar can be blinded by dust storms.






                              share|improve this answer





















                              • Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                                – Wayne Conrad
                                Nov 26 at 20:34






                              • 3




                                @WayneConrad: All 3 reasons contributed to the design change.
                                – Dr Sheldon
                                Nov 26 at 20:36






                              • 7




                                +1 for the how, but it actually misses the question of why.
                                – DarkDust
                                Nov 26 at 20:59






                              • 2




                                @WayneConrad: The wind, not the dust itself.
                                – Dr Sheldon
                                Nov 27 at 14:09






                              • 6




                                No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                                – Wayne Conrad
                                Nov 27 at 16:42















                              up vote
                              8
                              down vote













                              To deal with dust storms, two of the changes between Phoenix and InSight are mechanical in nature:





                              • InSight uses a thicker heat shield, partly to handle the possibility of being sandblasted by a dust storm.


                              • InSight’s parachute suspension lines use stronger material.



                              https://mars.nasa.gov/insight/timeline/landing/entry-descent-landing/




                              The landing site needs to be both flat and level, and reconnaissance helped to choose the optimal site. Nonetheless, there still could be boulders or small hills that should be avoided. Therefore, there are cameras and radar that help the computer decide the best place for landing, and thrust appropriately. These cameras and radar can be blinded by dust storms.






                              share|improve this answer





















                              • Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                                – Wayne Conrad
                                Nov 26 at 20:34






                              • 3




                                @WayneConrad: All 3 reasons contributed to the design change.
                                – Dr Sheldon
                                Nov 26 at 20:36






                              • 7




                                +1 for the how, but it actually misses the question of why.
                                – DarkDust
                                Nov 26 at 20:59






                              • 2




                                @WayneConrad: The wind, not the dust itself.
                                – Dr Sheldon
                                Nov 27 at 14:09






                              • 6




                                No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                                – Wayne Conrad
                                Nov 27 at 16:42













                              up vote
                              8
                              down vote










                              up vote
                              8
                              down vote









                              To deal with dust storms, two of the changes between Phoenix and InSight are mechanical in nature:





                              • InSight uses a thicker heat shield, partly to handle the possibility of being sandblasted by a dust storm.


                              • InSight’s parachute suspension lines use stronger material.



                              https://mars.nasa.gov/insight/timeline/landing/entry-descent-landing/




                              The landing site needs to be both flat and level, and reconnaissance helped to choose the optimal site. Nonetheless, there still could be boulders or small hills that should be avoided. Therefore, there are cameras and radar that help the computer decide the best place for landing, and thrust appropriately. These cameras and radar can be blinded by dust storms.






                              share|improve this answer












                              To deal with dust storms, two of the changes between Phoenix and InSight are mechanical in nature:





                              • InSight uses a thicker heat shield, partly to handle the possibility of being sandblasted by a dust storm.


                              • InSight’s parachute suspension lines use stronger material.



                              https://mars.nasa.gov/insight/timeline/landing/entry-descent-landing/




                              The landing site needs to be both flat and level, and reconnaissance helped to choose the optimal site. Nonetheless, there still could be boulders or small hills that should be avoided. Therefore, there are cameras and radar that help the computer decide the best place for landing, and thrust appropriately. These cameras and radar can be blinded by dust storms.







                              share|improve this answer












                              share|improve this answer



                              share|improve this answer










                              answered Nov 26 at 17:58









                              Dr Sheldon

                              4,59411647




                              4,59411647












                              • Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                                – Wayne Conrad
                                Nov 26 at 20:34






                              • 3




                                @WayneConrad: All 3 reasons contributed to the design change.
                                – Dr Sheldon
                                Nov 26 at 20:36






                              • 7




                                +1 for the how, but it actually misses the question of why.
                                – DarkDust
                                Nov 26 at 20:59






                              • 2




                                @WayneConrad: The wind, not the dust itself.
                                – Dr Sheldon
                                Nov 27 at 14:09






                              • 6




                                No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                                – Wayne Conrad
                                Nov 27 at 16:42


















                              • Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                                – Wayne Conrad
                                Nov 26 at 20:34






                              • 3




                                @WayneConrad: All 3 reasons contributed to the design change.
                                – Dr Sheldon
                                Nov 26 at 20:36






                              • 7




                                +1 for the how, but it actually misses the question of why.
                                – DarkDust
                                Nov 26 at 20:59






                              • 2




                                @WayneConrad: The wind, not the dust itself.
                                – Dr Sheldon
                                Nov 27 at 14:09






                              • 6




                                No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                                – Wayne Conrad
                                Nov 27 at 16:42
















                              Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                              – Wayne Conrad
                              Nov 26 at 20:34




                              Are the suspension lines stronger than Phoenix's because of possible dust storms, or because Insight is a little heavier, and its parachute was deployed at mach 1.8 instead of mach 1.7?
                              – Wayne Conrad
                              Nov 26 at 20:34




                              3




                              3




                              @WayneConrad: All 3 reasons contributed to the design change.
                              – Dr Sheldon
                              Nov 26 at 20:36




                              @WayneConrad: All 3 reasons contributed to the design change.
                              – Dr Sheldon
                              Nov 26 at 20:36




                              7




                              7




                              +1 for the how, but it actually misses the question of why.
                              – DarkDust
                              Nov 26 at 20:59




                              +1 for the how, but it actually misses the question of why.
                              – DarkDust
                              Nov 26 at 20:59




                              2




                              2




                              @WayneConrad: The wind, not the dust itself.
                              – Dr Sheldon
                              Nov 27 at 14:09




                              @WayneConrad: The wind, not the dust itself.
                              – Dr Sheldon
                              Nov 27 at 14:09




                              6




                              6




                              No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                              – Wayne Conrad
                              Nov 27 at 16:42




                              No, that's not how wind works on flying objects. If there is potential wind shear during deployment, that could cause increased loads on the parachute. But high wind speeds alone will not. That's because, aerodynamically, the capsule is flying relative to the wind, not relative to the ground.
                              – Wayne Conrad
                              Nov 27 at 16:42


















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