Why does Arabsat 6A need a Falcon Heavy to launchWhat missions could be done with Orion on Falcon Heavy?Falcon 9R as SSTOWhat would the challenges be in developing a Falcon Heavy with three or four strap-on boosters?Why is the first launch of Falcon Heavy sending a car instead of something useful?Was anything else about the Falcon Heavy test launch “off nominal” besides the center core return?What accounted for the total mass of the Tesla/Starman?How much payload can Falcon Heavy Reusable lift?Why doesn't SpaceX deploy some module to cover whole fairing like a rain coat just before sea landing?Does the downrange position of an ASDS vary, depending on payload mass?What is meant by “a high-energy geostationary orbit”? (SpaceX Arabsat 6A)

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Why does Arabsat 6A need a Falcon Heavy to launch


What missions could be done with Orion on Falcon Heavy?Falcon 9R as SSTOWhat would the challenges be in developing a Falcon Heavy with three or four strap-on boosters?Why is the first launch of Falcon Heavy sending a car instead of something useful?Was anything else about the Falcon Heavy test launch “off nominal” besides the center core return?What accounted for the total mass of the Tesla/Starman?How much payload can Falcon Heavy Reusable lift?Why doesn't SpaceX deploy some module to cover whole fairing like a rain coat just before sea landing?Does the downrange position of an ASDS vary, depending on payload mass?What is meant by “a high-energy geostationary orbit”? (SpaceX Arabsat 6A)













7












$begingroup$


Is it just me or does a falcon heavy seem like a bit of an overkill to launch Arabsat 6A?



Falcon Heavy - GEO payload: 26,700 kilograms



Arabsat 6A - weight: ~6000 kilograms



Wouldn't some other launch options be more appropriate or is there something about the launch of Arabsat 6A that needs the additional power?










share|improve this question









New contributor




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







$endgroup$











  • $begingroup$
    Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
    $endgroup$
    – Criggie
    Apr 4 at 23:37






  • 1




    $begingroup$
    The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
    $endgroup$
    – asgallant
    Apr 5 at 15:35
















7












$begingroup$


Is it just me or does a falcon heavy seem like a bit of an overkill to launch Arabsat 6A?



Falcon Heavy - GEO payload: 26,700 kilograms



Arabsat 6A - weight: ~6000 kilograms



Wouldn't some other launch options be more appropriate or is there something about the launch of Arabsat 6A that needs the additional power?










share|improve this question









New contributor




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







$endgroup$











  • $begingroup$
    Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
    $endgroup$
    – Criggie
    Apr 4 at 23:37






  • 1




    $begingroup$
    The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
    $endgroup$
    – asgallant
    Apr 5 at 15:35














7












7








7





$begingroup$


Is it just me or does a falcon heavy seem like a bit of an overkill to launch Arabsat 6A?



Falcon Heavy - GEO payload: 26,700 kilograms



Arabsat 6A - weight: ~6000 kilograms



Wouldn't some other launch options be more appropriate or is there something about the launch of Arabsat 6A that needs the additional power?










share|improve this question









New contributor




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







$endgroup$




Is it just me or does a falcon heavy seem like a bit of an overkill to launch Arabsat 6A?



Falcon Heavy - GEO payload: 26,700 kilograms



Arabsat 6A - weight: ~6000 kilograms



Wouldn't some other launch options be more appropriate or is there something about the launch of Arabsat 6A that needs the additional power?







spacex launch falcon-9 falcon-heavy






share|improve this question









New contributor




Jay Laughlin 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 question









New contributor




Jay Laughlin 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 question




share|improve this question








edited Apr 4 at 18:41







Jay Laughlin













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asked Apr 4 at 18:27









Jay LaughlinJay Laughlin

1016




1016




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New contributor





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






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











  • $begingroup$
    Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
    $endgroup$
    – Criggie
    Apr 4 at 23:37






  • 1




    $begingroup$
    The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
    $endgroup$
    – asgallant
    Apr 5 at 15:35

















  • $begingroup$
    Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
    $endgroup$
    – Criggie
    Apr 4 at 23:37






  • 1




    $begingroup$
    The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
    $endgroup$
    – asgallant
    Apr 5 at 15:35
















$begingroup$
Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
$endgroup$
– Criggie
Apr 4 at 23:37




$begingroup$
Is there anything else being launched ? 20k kilos of spare capacity could carry 3 more satellites, assuming there's physically room for them. Perhaps its like a bus, where not every seat is sold yet.
$endgroup$
– Criggie
Apr 4 at 23:37




1




1




$begingroup$
The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
$endgroup$
– asgallant
Apr 5 at 15:35





$begingroup$
The given payload figure is for a fully expendable Falcon Heavy. In fully reusable mode, the payload is 8000kg to GTO, still more than Arabsat 6A requires and allows for up to 2000kg of GTO ridesharing (potentially more if they can be dropped off in LEO on the way, but I don't know if that is ever done).
$endgroup$
– asgallant
Apr 5 at 15:35











3 Answers
3






active

oldest

votes


















7












$begingroup$

@geoffc's answer explains why Falcon Heavy over Falcon 9, but the reason for why not any of the other options is likely cost.



It's difficult to say with certainty what the launch costs would be, since costs are negotiated per launch, and are affected by a large number of factors (target orbit, payload mass, fuel costs, ridesharing, etc). Estimates put Falcon 9/Falcon Heavy's main competitors Ariane 5 at around $178M, Atlas 5 at $109M-179M, and Proton-M at about $100M1. Expendable Falcon 9 and Fully Reusable Falcon Heavy both cost an estimated $90M, and as @geoffc pointed out, FH has greater GTO capacity than F9, so the launch could use some combination of more favorable orbit and extra ridesharing capacity to reduce the effective launch cost.



Source



1 this reflects the likely cost as of the time when Arabsat 6A's launch was being negotiated; Proton-M has since been price-cut to be competitive to Falcon-9






share|improve this answer








New contributor




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






$endgroup$








  • 4




    $begingroup$
    Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
    $endgroup$
    – TooTea
    Apr 5 at 7:59


















9












$begingroup$

6000 Kg is actually pretty big. I am sure SpaceX offered some discounts to attract a customer for Falcon Heavy.



So I will ignore the other options (Atlas 5 with side boosters, Ariane 5, or Proton) and focus on why not a Falcon 9.



Falcon 9's numbers are lower to GTO, Wikipedia has it around 5500kg reusable. 8300kg expendable, and SpaceX's point is, if you are bigger than a Falcon 9 can handle and still land, better off moving to a Falcon Heavy.



Also there are different GTO orbits, the higher the 'energy' the less work (aka burned up fuel) the satellite needs to do to get to a circular GEO orbit. SpaceX does aim for a lower of the set, usually to allow recovery.






share|improve this answer









$endgroup$




















    2












    $begingroup$

    I know the SpaceX website does list the Falcon 9 as having a 8,300 kg payload to GTO Falcon 9 GTO but the wiki for Falcon 9 launches also shows that the Telstar 18V / Apstar-5C launch on Sept. 10, 2018 was 7,060 kg to GTO and a successful drone ship landing was achieved with the Falcon 9 Wiki-Launch 61. This would be a higher weight than the Arabsat 6 and also a GTO launch that did a successful drone ship landing so it was a reusable launch.



    The Arabsat 6 also uses powerful hypergolic main engine to boost to GEO from GTO according to Nasaspaceflight. There is no mention on the peak it will be sent in GTO but the satellite using those engines instead of electric seems to point to it needing a lot of thrust to circularize it's orbit.



    Unless there are some other specs that show this is being put in a different GTO orbit or higher it seems like the Falcon 9 reusable could launch this satellite.



    There must be another explanation such as SpaceX discount to use this as a Falcon Heavy qualification flight for the USAF or something else.






    share|improve this answer








    New contributor




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






    $endgroup$













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      3 Answers
      3






      active

      oldest

      votes








      3 Answers
      3






      active

      oldest

      votes









      active

      oldest

      votes






      active

      oldest

      votes









      7












      $begingroup$

      @geoffc's answer explains why Falcon Heavy over Falcon 9, but the reason for why not any of the other options is likely cost.



      It's difficult to say with certainty what the launch costs would be, since costs are negotiated per launch, and are affected by a large number of factors (target orbit, payload mass, fuel costs, ridesharing, etc). Estimates put Falcon 9/Falcon Heavy's main competitors Ariane 5 at around $178M, Atlas 5 at $109M-179M, and Proton-M at about $100M1. Expendable Falcon 9 and Fully Reusable Falcon Heavy both cost an estimated $90M, and as @geoffc pointed out, FH has greater GTO capacity than F9, so the launch could use some combination of more favorable orbit and extra ridesharing capacity to reduce the effective launch cost.



      Source



      1 this reflects the likely cost as of the time when Arabsat 6A's launch was being negotiated; Proton-M has since been price-cut to be competitive to Falcon-9






      share|improve this answer








      New contributor




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






      $endgroup$








      • 4




        $begingroup$
        Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
        $endgroup$
        – TooTea
        Apr 5 at 7:59















      7












      $begingroup$

      @geoffc's answer explains why Falcon Heavy over Falcon 9, but the reason for why not any of the other options is likely cost.



      It's difficult to say with certainty what the launch costs would be, since costs are negotiated per launch, and are affected by a large number of factors (target orbit, payload mass, fuel costs, ridesharing, etc). Estimates put Falcon 9/Falcon Heavy's main competitors Ariane 5 at around $178M, Atlas 5 at $109M-179M, and Proton-M at about $100M1. Expendable Falcon 9 and Fully Reusable Falcon Heavy both cost an estimated $90M, and as @geoffc pointed out, FH has greater GTO capacity than F9, so the launch could use some combination of more favorable orbit and extra ridesharing capacity to reduce the effective launch cost.



      Source



      1 this reflects the likely cost as of the time when Arabsat 6A's launch was being negotiated; Proton-M has since been price-cut to be competitive to Falcon-9






      share|improve this answer








      New contributor




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






      $endgroup$








      • 4




        $begingroup$
        Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
        $endgroup$
        – TooTea
        Apr 5 at 7:59













      7












      7








      7





      $begingroup$

      @geoffc's answer explains why Falcon Heavy over Falcon 9, but the reason for why not any of the other options is likely cost.



      It's difficult to say with certainty what the launch costs would be, since costs are negotiated per launch, and are affected by a large number of factors (target orbit, payload mass, fuel costs, ridesharing, etc). Estimates put Falcon 9/Falcon Heavy's main competitors Ariane 5 at around $178M, Atlas 5 at $109M-179M, and Proton-M at about $100M1. Expendable Falcon 9 and Fully Reusable Falcon Heavy both cost an estimated $90M, and as @geoffc pointed out, FH has greater GTO capacity than F9, so the launch could use some combination of more favorable orbit and extra ridesharing capacity to reduce the effective launch cost.



      Source



      1 this reflects the likely cost as of the time when Arabsat 6A's launch was being negotiated; Proton-M has since been price-cut to be competitive to Falcon-9






      share|improve this answer








      New contributor




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






      $endgroup$



      @geoffc's answer explains why Falcon Heavy over Falcon 9, but the reason for why not any of the other options is likely cost.



      It's difficult to say with certainty what the launch costs would be, since costs are negotiated per launch, and are affected by a large number of factors (target orbit, payload mass, fuel costs, ridesharing, etc). Estimates put Falcon 9/Falcon Heavy's main competitors Ariane 5 at around $178M, Atlas 5 at $109M-179M, and Proton-M at about $100M1. Expendable Falcon 9 and Fully Reusable Falcon Heavy both cost an estimated $90M, and as @geoffc pointed out, FH has greater GTO capacity than F9, so the launch could use some combination of more favorable orbit and extra ridesharing capacity to reduce the effective launch cost.



      Source



      1 this reflects the likely cost as of the time when Arabsat 6A's launch was being negotiated; Proton-M has since been price-cut to be competitive to Falcon-9







      share|improve this answer








      New contributor




      asgallant 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




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









      answered Apr 4 at 22:52









      asgallantasgallant

      1862




      1862




      New contributor




      asgallant is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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      New contributor





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






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







      • 4




        $begingroup$
        Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
        $endgroup$
        – TooTea
        Apr 5 at 7:59












      • 4




        $begingroup$
        Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
        $endgroup$
        – TooTea
        Apr 5 at 7:59







      4




      4




      $begingroup$
      Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
      $endgroup$
      – TooTea
      Apr 5 at 7:59




      $begingroup$
      Also, this being the first revenue flight of FH (and the second overall), I'm pretty sure that SpaceX went out of their way to make the FH price really attractive this time, no matter what are their long-term price targets or costs.
      $endgroup$
      – TooTea
      Apr 5 at 7:59











      9












      $begingroup$

      6000 Kg is actually pretty big. I am sure SpaceX offered some discounts to attract a customer for Falcon Heavy.



      So I will ignore the other options (Atlas 5 with side boosters, Ariane 5, or Proton) and focus on why not a Falcon 9.



      Falcon 9's numbers are lower to GTO, Wikipedia has it around 5500kg reusable. 8300kg expendable, and SpaceX's point is, if you are bigger than a Falcon 9 can handle and still land, better off moving to a Falcon Heavy.



      Also there are different GTO orbits, the higher the 'energy' the less work (aka burned up fuel) the satellite needs to do to get to a circular GEO orbit. SpaceX does aim for a lower of the set, usually to allow recovery.






      share|improve this answer









      $endgroup$

















        9












        $begingroup$

        6000 Kg is actually pretty big. I am sure SpaceX offered some discounts to attract a customer for Falcon Heavy.



        So I will ignore the other options (Atlas 5 with side boosters, Ariane 5, or Proton) and focus on why not a Falcon 9.



        Falcon 9's numbers are lower to GTO, Wikipedia has it around 5500kg reusable. 8300kg expendable, and SpaceX's point is, if you are bigger than a Falcon 9 can handle and still land, better off moving to a Falcon Heavy.



        Also there are different GTO orbits, the higher the 'energy' the less work (aka burned up fuel) the satellite needs to do to get to a circular GEO orbit. SpaceX does aim for a lower of the set, usually to allow recovery.






        share|improve this answer









        $endgroup$















          9












          9








          9





          $begingroup$

          6000 Kg is actually pretty big. I am sure SpaceX offered some discounts to attract a customer for Falcon Heavy.



          So I will ignore the other options (Atlas 5 with side boosters, Ariane 5, or Proton) and focus on why not a Falcon 9.



          Falcon 9's numbers are lower to GTO, Wikipedia has it around 5500kg reusable. 8300kg expendable, and SpaceX's point is, if you are bigger than a Falcon 9 can handle and still land, better off moving to a Falcon Heavy.



          Also there are different GTO orbits, the higher the 'energy' the less work (aka burned up fuel) the satellite needs to do to get to a circular GEO orbit. SpaceX does aim for a lower of the set, usually to allow recovery.






          share|improve this answer









          $endgroup$



          6000 Kg is actually pretty big. I am sure SpaceX offered some discounts to attract a customer for Falcon Heavy.



          So I will ignore the other options (Atlas 5 with side boosters, Ariane 5, or Proton) and focus on why not a Falcon 9.



          Falcon 9's numbers are lower to GTO, Wikipedia has it around 5500kg reusable. 8300kg expendable, and SpaceX's point is, if you are bigger than a Falcon 9 can handle and still land, better off moving to a Falcon Heavy.



          Also there are different GTO orbits, the higher the 'energy' the less work (aka burned up fuel) the satellite needs to do to get to a circular GEO orbit. SpaceX does aim for a lower of the set, usually to allow recovery.







          share|improve this answer












          share|improve this answer



          share|improve this answer










          answered Apr 4 at 18:38









          geoffcgeoffc

          56k10162310




          56k10162310





















              2












              $begingroup$

              I know the SpaceX website does list the Falcon 9 as having a 8,300 kg payload to GTO Falcon 9 GTO but the wiki for Falcon 9 launches also shows that the Telstar 18V / Apstar-5C launch on Sept. 10, 2018 was 7,060 kg to GTO and a successful drone ship landing was achieved with the Falcon 9 Wiki-Launch 61. This would be a higher weight than the Arabsat 6 and also a GTO launch that did a successful drone ship landing so it was a reusable launch.



              The Arabsat 6 also uses powerful hypergolic main engine to boost to GEO from GTO according to Nasaspaceflight. There is no mention on the peak it will be sent in GTO but the satellite using those engines instead of electric seems to point to it needing a lot of thrust to circularize it's orbit.



              Unless there are some other specs that show this is being put in a different GTO orbit or higher it seems like the Falcon 9 reusable could launch this satellite.



              There must be another explanation such as SpaceX discount to use this as a Falcon Heavy qualification flight for the USAF or something else.






              share|improve this answer








              New contributor




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






              $endgroup$

















                2












                $begingroup$

                I know the SpaceX website does list the Falcon 9 as having a 8,300 kg payload to GTO Falcon 9 GTO but the wiki for Falcon 9 launches also shows that the Telstar 18V / Apstar-5C launch on Sept. 10, 2018 was 7,060 kg to GTO and a successful drone ship landing was achieved with the Falcon 9 Wiki-Launch 61. This would be a higher weight than the Arabsat 6 and also a GTO launch that did a successful drone ship landing so it was a reusable launch.



                The Arabsat 6 also uses powerful hypergolic main engine to boost to GEO from GTO according to Nasaspaceflight. There is no mention on the peak it will be sent in GTO but the satellite using those engines instead of electric seems to point to it needing a lot of thrust to circularize it's orbit.



                Unless there are some other specs that show this is being put in a different GTO orbit or higher it seems like the Falcon 9 reusable could launch this satellite.



                There must be another explanation such as SpaceX discount to use this as a Falcon Heavy qualification flight for the USAF or something else.






                share|improve this answer








                New contributor




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






                $endgroup$















                  2












                  2








                  2





                  $begingroup$

                  I know the SpaceX website does list the Falcon 9 as having a 8,300 kg payload to GTO Falcon 9 GTO but the wiki for Falcon 9 launches also shows that the Telstar 18V / Apstar-5C launch on Sept. 10, 2018 was 7,060 kg to GTO and a successful drone ship landing was achieved with the Falcon 9 Wiki-Launch 61. This would be a higher weight than the Arabsat 6 and also a GTO launch that did a successful drone ship landing so it was a reusable launch.



                  The Arabsat 6 also uses powerful hypergolic main engine to boost to GEO from GTO according to Nasaspaceflight. There is no mention on the peak it will be sent in GTO but the satellite using those engines instead of electric seems to point to it needing a lot of thrust to circularize it's orbit.



                  Unless there are some other specs that show this is being put in a different GTO orbit or higher it seems like the Falcon 9 reusable could launch this satellite.



                  There must be another explanation such as SpaceX discount to use this as a Falcon Heavy qualification flight for the USAF or something else.






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                  New contributor




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                  I know the SpaceX website does list the Falcon 9 as having a 8,300 kg payload to GTO Falcon 9 GTO but the wiki for Falcon 9 launches also shows that the Telstar 18V / Apstar-5C launch on Sept. 10, 2018 was 7,060 kg to GTO and a successful drone ship landing was achieved with the Falcon 9 Wiki-Launch 61. This would be a higher weight than the Arabsat 6 and also a GTO launch that did a successful drone ship landing so it was a reusable launch.



                  The Arabsat 6 also uses powerful hypergolic main engine to boost to GEO from GTO according to Nasaspaceflight. There is no mention on the peak it will be sent in GTO but the satellite using those engines instead of electric seems to point to it needing a lot of thrust to circularize it's orbit.



                  Unless there are some other specs that show this is being put in a different GTO orbit or higher it seems like the Falcon 9 reusable could launch this satellite.



                  There must be another explanation such as SpaceX discount to use this as a Falcon Heavy qualification flight for the USAF or something else.







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