How is the CG of rocket found after the complete assembly











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Using CAD modeling, the center of gravity of a rocket can be easily predicted. But in reality, after the assembly, the CG will not be exactly at the place given by the model because of difference in manufacturing of components and other assemblies like plumbing and wiring etc.



So, how is CG determined after complete assembly of the rocket?










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  • 6




    for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
    – JCRM
    2 days ago






  • 3




    If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
    – Uwe
    2 days ago






  • 4




    @JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
    – Level River St
    2 days ago















up vote
8
down vote

favorite












Using CAD modeling, the center of gravity of a rocket can be easily predicted. But in reality, after the assembly, the CG will not be exactly at the place given by the model because of difference in manufacturing of components and other assemblies like plumbing and wiring etc.



So, how is CG determined after complete assembly of the rocket?










share|improve this question




















  • 6




    for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
    – JCRM
    2 days ago






  • 3




    If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
    – Uwe
    2 days ago






  • 4




    @JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
    – Level River St
    2 days ago













up vote
8
down vote

favorite









up vote
8
down vote

favorite











Using CAD modeling, the center of gravity of a rocket can be easily predicted. But in reality, after the assembly, the CG will not be exactly at the place given by the model because of difference in manufacturing of components and other assemblies like plumbing and wiring etc.



So, how is CG determined after complete assembly of the rocket?










share|improve this question















Using CAD modeling, the center of gravity of a rocket can be easily predicted. But in reality, after the assembly, the CG will not be exactly at the place given by the model because of difference in manufacturing of components and other assemblies like plumbing and wiring etc.



So, how is CG determined after complete assembly of the rocket?







rockets center-of-gravity






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share|improve this question













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share|improve this question








edited 2 days ago









uhoh

33.3k16114408




33.3k16114408










asked 2 days ago









Amar

1,009527




1,009527








  • 6




    for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
    – JCRM
    2 days ago






  • 3




    If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
    – Uwe
    2 days ago






  • 4




    @JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
    – Level River St
    2 days ago














  • 6




    for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
    – JCRM
    2 days ago






  • 3




    If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
    – Uwe
    2 days ago






  • 4




    @JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
    – Level River St
    2 days ago








6




6




for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
– JCRM
2 days ago




for launch vehicles, knowing the exact CoG isn't necessary -- the software compensates for the behaviour of the vehicle, not the cause.
– JCRM
2 days ago




3




3




If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
– Uwe
2 days ago




If a very strict quality control is used during manufacture, every part and every subassembley is weighted at different steps of manufacture. If actual weight is different to planned weight, reject the part until the reason for weight difference is found and resolved. You don't want a rocket with substantial differences in structural weight.
– Uwe
2 days ago




4




4




@JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
– Level River St
2 days ago




@JCRM indeed the the CoG varies massively during launch! Liquid fuelled rockets generally have the O2 tank forward of the fuel tank to get the CoG as far forward as possible and so enhance the effect of gimballing the engines. But when the fuel is spent, the CoG moves back. Not to mention the effects of propellant slosh...
– Level River St
2 days ago










3 Answers
3






active

oldest

votes

















up vote
14
down vote













Modern CAD software is very good and can include the mass of every zip tie and weld if it's made with enough care. If the real life doesn't match up with plans, the whole rocket can be put on multiple load sensors and from that the CG can be calculated. However, finding the CG is still important, especially in flight when mass is changing due to fuel consumption and rocket staging.



When an object is in flight or is not constrained, it rotates about its CG. This means if you spread accelerometers around the object and compare the different readings of those sensors, the CG can be calculated quickly. For more detail on this technique, you can read this paper: https://www.mdpi.com/1424-8220/14/9/17567/htm






share|improve this answer






























    up vote
    7
    down vote













    For the Apollo program, there was a device that measured the weight and balance of the completed modules. Page 9-4 of the Apollo Program Summary Report describes the steps in manufacturing the Command Module:




    9.1.1.3 Final operations: In the final phase of command module manufacturing, the vehicle was cycled through another tumble-and-clean operation in which the vehicle was rotated through 360° in each axis to dislodge and remove debris. The weight and center of gravity were then determined, and the vehicle was subjected to an integrated test (sec. 9.1.5). The command module was subsequently moved to the shipping area and prepared for shipment. Such items as crew couches and crew equipment were removed, packed, and shipped separately.




    The manufacturing of the Service Module is described on page 9-6:




    Following the tests, the vehicle was cycled through the tumble-and-clean positioner to dislodge and remove debris. The cleaned vehicle was then weighed and its center of gravity determined. On completion of these operations, the vehicle was placed in the integrated test stand for the integrated test series described in section 9.1.5. The integrated test completed the manufacturing, test, and checkout operations, and the vehicle was mounted on a shipping pallet and prepared for shipment.




    Both operations were performed on a piece of equipment called the "weight and balance fixture":



    CSM manufacturing equipment






    share|improve this answer




























      up vote
      0
      down vote













      The exact CG position is (never?) required



      You just need a good CAD approximation (and maybe verifying the CG of complicated heavy parts if strong doubts still exist). Then you qualify your GNC algorithms taking into account all the variations you can predict (and some marging for the ones you cannot).



      When accelerometers are used, for example on Ariane, it is to measure the dynamic state of the launcher, i.e. which dynamic structural mode is active, to avoid control errors (and amplifying dynamic mode)






      share|improve this answer








      New contributor




      Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.


















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        3 Answers
        3






        active

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        3 Answers
        3






        active

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        active

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        up vote
        14
        down vote













        Modern CAD software is very good and can include the mass of every zip tie and weld if it's made with enough care. If the real life doesn't match up with plans, the whole rocket can be put on multiple load sensors and from that the CG can be calculated. However, finding the CG is still important, especially in flight when mass is changing due to fuel consumption and rocket staging.



        When an object is in flight or is not constrained, it rotates about its CG. This means if you spread accelerometers around the object and compare the different readings of those sensors, the CG can be calculated quickly. For more detail on this technique, you can read this paper: https://www.mdpi.com/1424-8220/14/9/17567/htm






        share|improve this answer



























          up vote
          14
          down vote













          Modern CAD software is very good and can include the mass of every zip tie and weld if it's made with enough care. If the real life doesn't match up with plans, the whole rocket can be put on multiple load sensors and from that the CG can be calculated. However, finding the CG is still important, especially in flight when mass is changing due to fuel consumption and rocket staging.



          When an object is in flight or is not constrained, it rotates about its CG. This means if you spread accelerometers around the object and compare the different readings of those sensors, the CG can be calculated quickly. For more detail on this technique, you can read this paper: https://www.mdpi.com/1424-8220/14/9/17567/htm






          share|improve this answer

























            up vote
            14
            down vote










            up vote
            14
            down vote









            Modern CAD software is very good and can include the mass of every zip tie and weld if it's made with enough care. If the real life doesn't match up with plans, the whole rocket can be put on multiple load sensors and from that the CG can be calculated. However, finding the CG is still important, especially in flight when mass is changing due to fuel consumption and rocket staging.



            When an object is in flight or is not constrained, it rotates about its CG. This means if you spread accelerometers around the object and compare the different readings of those sensors, the CG can be calculated quickly. For more detail on this technique, you can read this paper: https://www.mdpi.com/1424-8220/14/9/17567/htm






            share|improve this answer














            Modern CAD software is very good and can include the mass of every zip tie and weld if it's made with enough care. If the real life doesn't match up with plans, the whole rocket can be put on multiple load sensors and from that the CG can be calculated. However, finding the CG is still important, especially in flight when mass is changing due to fuel consumption and rocket staging.



            When an object is in flight or is not constrained, it rotates about its CG. This means if you spread accelerometers around the object and compare the different readings of those sensors, the CG can be calculated quickly. For more detail on this technique, you can read this paper: https://www.mdpi.com/1424-8220/14/9/17567/htm







            share|improve this answer














            share|improve this answer



            share|improve this answer








            edited 2 days ago

























            answered 2 days ago









            Dragongeek

            3,2671330




            3,2671330






















                up vote
                7
                down vote













                For the Apollo program, there was a device that measured the weight and balance of the completed modules. Page 9-4 of the Apollo Program Summary Report describes the steps in manufacturing the Command Module:




                9.1.1.3 Final operations: In the final phase of command module manufacturing, the vehicle was cycled through another tumble-and-clean operation in which the vehicle was rotated through 360° in each axis to dislodge and remove debris. The weight and center of gravity were then determined, and the vehicle was subjected to an integrated test (sec. 9.1.5). The command module was subsequently moved to the shipping area and prepared for shipment. Such items as crew couches and crew equipment were removed, packed, and shipped separately.




                The manufacturing of the Service Module is described on page 9-6:




                Following the tests, the vehicle was cycled through the tumble-and-clean positioner to dislodge and remove debris. The cleaned vehicle was then weighed and its center of gravity determined. On completion of these operations, the vehicle was placed in the integrated test stand for the integrated test series described in section 9.1.5. The integrated test completed the manufacturing, test, and checkout operations, and the vehicle was mounted on a shipping pallet and prepared for shipment.




                Both operations were performed on a piece of equipment called the "weight and balance fixture":



                CSM manufacturing equipment






                share|improve this answer

























                  up vote
                  7
                  down vote













                  For the Apollo program, there was a device that measured the weight and balance of the completed modules. Page 9-4 of the Apollo Program Summary Report describes the steps in manufacturing the Command Module:




                  9.1.1.3 Final operations: In the final phase of command module manufacturing, the vehicle was cycled through another tumble-and-clean operation in which the vehicle was rotated through 360° in each axis to dislodge and remove debris. The weight and center of gravity were then determined, and the vehicle was subjected to an integrated test (sec. 9.1.5). The command module was subsequently moved to the shipping area and prepared for shipment. Such items as crew couches and crew equipment were removed, packed, and shipped separately.




                  The manufacturing of the Service Module is described on page 9-6:




                  Following the tests, the vehicle was cycled through the tumble-and-clean positioner to dislodge and remove debris. The cleaned vehicle was then weighed and its center of gravity determined. On completion of these operations, the vehicle was placed in the integrated test stand for the integrated test series described in section 9.1.5. The integrated test completed the manufacturing, test, and checkout operations, and the vehicle was mounted on a shipping pallet and prepared for shipment.




                  Both operations were performed on a piece of equipment called the "weight and balance fixture":



                  CSM manufacturing equipment






                  share|improve this answer























                    up vote
                    7
                    down vote










                    up vote
                    7
                    down vote









                    For the Apollo program, there was a device that measured the weight and balance of the completed modules. Page 9-4 of the Apollo Program Summary Report describes the steps in manufacturing the Command Module:




                    9.1.1.3 Final operations: In the final phase of command module manufacturing, the vehicle was cycled through another tumble-and-clean operation in which the vehicle was rotated through 360° in each axis to dislodge and remove debris. The weight and center of gravity were then determined, and the vehicle was subjected to an integrated test (sec. 9.1.5). The command module was subsequently moved to the shipping area and prepared for shipment. Such items as crew couches and crew equipment were removed, packed, and shipped separately.




                    The manufacturing of the Service Module is described on page 9-6:




                    Following the tests, the vehicle was cycled through the tumble-and-clean positioner to dislodge and remove debris. The cleaned vehicle was then weighed and its center of gravity determined. On completion of these operations, the vehicle was placed in the integrated test stand for the integrated test series described in section 9.1.5. The integrated test completed the manufacturing, test, and checkout operations, and the vehicle was mounted on a shipping pallet and prepared for shipment.




                    Both operations were performed on a piece of equipment called the "weight and balance fixture":



                    CSM manufacturing equipment






                    share|improve this answer












                    For the Apollo program, there was a device that measured the weight and balance of the completed modules. Page 9-4 of the Apollo Program Summary Report describes the steps in manufacturing the Command Module:




                    9.1.1.3 Final operations: In the final phase of command module manufacturing, the vehicle was cycled through another tumble-and-clean operation in which the vehicle was rotated through 360° in each axis to dislodge and remove debris. The weight and center of gravity were then determined, and the vehicle was subjected to an integrated test (sec. 9.1.5). The command module was subsequently moved to the shipping area and prepared for shipment. Such items as crew couches and crew equipment were removed, packed, and shipped separately.




                    The manufacturing of the Service Module is described on page 9-6:




                    Following the tests, the vehicle was cycled through the tumble-and-clean positioner to dislodge and remove debris. The cleaned vehicle was then weighed and its center of gravity determined. On completion of these operations, the vehicle was placed in the integrated test stand for the integrated test series described in section 9.1.5. The integrated test completed the manufacturing, test, and checkout operations, and the vehicle was mounted on a shipping pallet and prepared for shipment.




                    Both operations were performed on a piece of equipment called the "weight and balance fixture":



                    CSM manufacturing equipment







                    share|improve this answer












                    share|improve this answer



                    share|improve this answer










                    answered 2 days ago









                    Dr Sheldon

                    4,0081342




                    4,0081342






















                        up vote
                        0
                        down vote













                        The exact CG position is (never?) required



                        You just need a good CAD approximation (and maybe verifying the CG of complicated heavy parts if strong doubts still exist). Then you qualify your GNC algorithms taking into account all the variations you can predict (and some marging for the ones you cannot).



                        When accelerometers are used, for example on Ariane, it is to measure the dynamic state of the launcher, i.e. which dynamic structural mode is active, to avoid control errors (and amplifying dynamic mode)






                        share|improve this answer








                        New contributor




                        Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                        Check out our Code of Conduct.






















                          up vote
                          0
                          down vote













                          The exact CG position is (never?) required



                          You just need a good CAD approximation (and maybe verifying the CG of complicated heavy parts if strong doubts still exist). Then you qualify your GNC algorithms taking into account all the variations you can predict (and some marging for the ones you cannot).



                          When accelerometers are used, for example on Ariane, it is to measure the dynamic state of the launcher, i.e. which dynamic structural mode is active, to avoid control errors (and amplifying dynamic mode)






                          share|improve this answer








                          New contributor




                          Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                          Check out our Code of Conduct.




















                            up vote
                            0
                            down vote










                            up vote
                            0
                            down vote









                            The exact CG position is (never?) required



                            You just need a good CAD approximation (and maybe verifying the CG of complicated heavy parts if strong doubts still exist). Then you qualify your GNC algorithms taking into account all the variations you can predict (and some marging for the ones you cannot).



                            When accelerometers are used, for example on Ariane, it is to measure the dynamic state of the launcher, i.e. which dynamic structural mode is active, to avoid control errors (and amplifying dynamic mode)






                            share|improve this answer








                            New contributor




                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.









                            The exact CG position is (never?) required



                            You just need a good CAD approximation (and maybe verifying the CG of complicated heavy parts if strong doubts still exist). Then you qualify your GNC algorithms taking into account all the variations you can predict (and some marging for the ones you cannot).



                            When accelerometers are used, for example on Ariane, it is to measure the dynamic state of the launcher, i.e. which dynamic structural mode is active, to avoid control errors (and amplifying dynamic mode)







                            share|improve this answer








                            New contributor




                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.









                            share|improve this answer



                            share|improve this answer






                            New contributor




                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.









                            answered yesterday









                            Olivier

                            1012




                            1012




                            New contributor




                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.





                            New contributor





                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.






                            Olivier is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                            Check out our Code of Conduct.






























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