What are “Ohms burns” in the context of Scott Kelly, KSP, and the Space Shuttle?

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15
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2












The Ars Technica video Astronaut Scott Kelly teaches orbital mechanics with Kerbal Space Program (also in YouTube) is a little bit humorous.



When Scott Kelley is talking about orbit circularization he says (per the on-screen captioning):




Actually the Space Shuttle has two Ohms burns generally.




Question: What are Ohms burns, and why are two needed?



enter image description here




Ars Technica's Lee Hutchinson sits down with astronaut Scott Kelly while they play Kerbal Space Program. Scott Kelly uses his experiences on the real International Space Station to give his opinion on the accuracy of the video game.








share|improve this question





















  • The first link in your question doesn't go where it appears it should go.
    – Organic Marble
    Aug 3 at 0:10







  • 4




    I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
    – Organic Marble
    Aug 3 at 0:19






  • 1




    wow we just made the same correction!
    – uhoh
    Aug 3 at 0:27






  • 2




    I wanted to watch the video! Thanks to the youtube link I found it.
    – Organic Marble
    Aug 3 at 0:38






  • 3




    @OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
    – Digger
    yesterday















up vote
15
down vote

favorite
2












The Ars Technica video Astronaut Scott Kelly teaches orbital mechanics with Kerbal Space Program (also in YouTube) is a little bit humorous.



When Scott Kelley is talking about orbit circularization he says (per the on-screen captioning):




Actually the Space Shuttle has two Ohms burns generally.




Question: What are Ohms burns, and why are two needed?



enter image description here




Ars Technica's Lee Hutchinson sits down with astronaut Scott Kelly while they play Kerbal Space Program. Scott Kelly uses his experiences on the real International Space Station to give his opinion on the accuracy of the video game.








share|improve this question





















  • The first link in your question doesn't go where it appears it should go.
    – Organic Marble
    Aug 3 at 0:10







  • 4




    I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
    – Organic Marble
    Aug 3 at 0:19






  • 1




    wow we just made the same correction!
    – uhoh
    Aug 3 at 0:27






  • 2




    I wanted to watch the video! Thanks to the youtube link I found it.
    – Organic Marble
    Aug 3 at 0:38






  • 3




    @OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
    – Digger
    yesterday













up vote
15
down vote

favorite
2









up vote
15
down vote

favorite
2






2





The Ars Technica video Astronaut Scott Kelly teaches orbital mechanics with Kerbal Space Program (also in YouTube) is a little bit humorous.



When Scott Kelley is talking about orbit circularization he says (per the on-screen captioning):




Actually the Space Shuttle has two Ohms burns generally.




Question: What are Ohms burns, and why are two needed?



enter image description here




Ars Technica's Lee Hutchinson sits down with astronaut Scott Kelly while they play Kerbal Space Program. Scott Kelly uses his experiences on the real International Space Station to give his opinion on the accuracy of the video game.








share|improve this question













The Ars Technica video Astronaut Scott Kelly teaches orbital mechanics with Kerbal Space Program (also in YouTube) is a little bit humorous.



When Scott Kelley is talking about orbit circularization he says (per the on-screen captioning):




Actually the Space Shuttle has two Ohms burns generally.




Question: What are Ohms burns, and why are two needed?



enter image description here




Ars Technica's Lee Hutchinson sits down with astronaut Scott Kelly while they play Kerbal Space Program. Scott Kelly uses his experiences on the real International Space Station to give his opinion on the accuracy of the video game.










share|improve this question












share|improve this question




share|improve this question








edited Aug 3 at 0:26









Organic Marble

44.5k2113191




44.5k2113191









asked Aug 2 at 22:31









uhoh

26.3k1083329




26.3k1083329











  • The first link in your question doesn't go where it appears it should go.
    – Organic Marble
    Aug 3 at 0:10







  • 4




    I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
    – Organic Marble
    Aug 3 at 0:19






  • 1




    wow we just made the same correction!
    – uhoh
    Aug 3 at 0:27






  • 2




    I wanted to watch the video! Thanks to the youtube link I found it.
    – Organic Marble
    Aug 3 at 0:38






  • 3




    @OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
    – Digger
    yesterday

















  • The first link in your question doesn't go where it appears it should go.
    – Organic Marble
    Aug 3 at 0:10







  • 4




    I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
    – Organic Marble
    Aug 3 at 0:19






  • 1




    wow we just made the same correction!
    – uhoh
    Aug 3 at 0:27






  • 2




    I wanted to watch the video! Thanks to the youtube link I found it.
    – Organic Marble
    Aug 3 at 0:38






  • 3




    @OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
    – Digger
    yesterday
















The first link in your question doesn't go where it appears it should go.
– Organic Marble
Aug 3 at 0:10





The first link in your question doesn't go where it appears it should go.
– Organic Marble
Aug 3 at 0:10





4




4




I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
– Organic Marble
Aug 3 at 0:19




I'm surprised to hear Kelly say that. The OMS-1 burn was deleted for STS-41C and subsequent when the "Direct Insertion" technique became standard. During his entire astronaut career OMS-1 burns weren't performed. Perhaps spending 95.5% of a year in space affects the memory :)
– Organic Marble
Aug 3 at 0:19




1




1




wow we just made the same correction!
– uhoh
Aug 3 at 0:27




wow we just made the same correction!
– uhoh
Aug 3 at 0:27




2




2




I wanted to watch the video! Thanks to the youtube link I found it.
– Organic Marble
Aug 3 at 0:38




I wanted to watch the video! Thanks to the youtube link I found it.
– Organic Marble
Aug 3 at 0:38




3




3




@OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
– Digger
yesterday





@OrganicMarble, ya gotta remember that, of all the Space Shuttle Ascents Scott has "flown" over the years, well over 99% of them were in the simulator. And, since simulator ascents were virtually never nominal (normal), a goodly percentage of them involved an OMS-1 burn...sort of "sticks in the memory!"
– Digger
yesterday











2 Answers
2






active

oldest

votes

















up vote
41
down vote













That's a mistranscription of OMS Burn, or Orbital Maneuvering System burn. The OMS system is how the shuttle changed its orbital characteristics. You can read about it here. One, two or more might have been used to fine tune the orbit, avoid space debris, rendezvous with the space station, etc.






share|improve this answer






























    up vote
    16
    down vote













    Since the questioner also asks "why are two needed" and the other answer didn't address that:



    Early shuttle missions flew a "standard insertion" ascent. This required two burns of the Orbital Maneuvering System after the main engines shut down and the external tank was jettisoned. The first burn (OMS-1) raised the apogee of the orbit, and the second one (OMS-2) circularized the orbit by raising the perigee.



    For STS-41C and subsequent, "direct insertion" ascents were flown. The trajectory was shaped so that a higher apogee was achieved on the main engines, and only the OMS-2 burn (it retained that name) was required.



    These graphs from the Shuttle Crew Operations Manual show the performance advantage of direct insertion missions.



    enter image description here



    Incidentally, "direct insertion" implied that the external tank was released into a higher orbit and it flew a lot further around the Earth before reentering, than it had for the standard insertion missions.



    enter image description here



    The OMS (and the aft Reaction Control Systems) were contained in pods on either side of the Orbiter's vertical tail.



    enter image description here



    Here is a cutaway drawing of the pod, with some pertinent info, from the 1985 Space Shuttle Press Reference.



    enter image description here






    share|improve this answer



















    • 1




      There was an additional OMS burn on day 02 of STS-103.
      – JdeBP
      2 days ago






    • 1




      There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
      – Organic Marble
      2 days ago











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    2 Answers
    2






    active

    oldest

    votes








    2 Answers
    2






    active

    oldest

    votes









    active

    oldest

    votes






    active

    oldest

    votes








    up vote
    41
    down vote













    That's a mistranscription of OMS Burn, or Orbital Maneuvering System burn. The OMS system is how the shuttle changed its orbital characteristics. You can read about it here. One, two or more might have been used to fine tune the orbit, avoid space debris, rendezvous with the space station, etc.






    share|improve this answer



























      up vote
      41
      down vote













      That's a mistranscription of OMS Burn, or Orbital Maneuvering System burn. The OMS system is how the shuttle changed its orbital characteristics. You can read about it here. One, two or more might have been used to fine tune the orbit, avoid space debris, rendezvous with the space station, etc.






      share|improve this answer

























        up vote
        41
        down vote










        up vote
        41
        down vote









        That's a mistranscription of OMS Burn, or Orbital Maneuvering System burn. The OMS system is how the shuttle changed its orbital characteristics. You can read about it here. One, two or more might have been used to fine tune the orbit, avoid space debris, rendezvous with the space station, etc.






        share|improve this answer















        That's a mistranscription of OMS Burn, or Orbital Maneuvering System burn. The OMS system is how the shuttle changed its orbital characteristics. You can read about it here. One, two or more might have been used to fine tune the orbit, avoid space debris, rendezvous with the space station, etc.







        share|improve this answer















        share|improve this answer



        share|improve this answer








        edited Aug 2 at 23:04


























        answered Aug 2 at 22:51









        BobT

        63136




        63136




















            up vote
            16
            down vote













            Since the questioner also asks "why are two needed" and the other answer didn't address that:



            Early shuttle missions flew a "standard insertion" ascent. This required two burns of the Orbital Maneuvering System after the main engines shut down and the external tank was jettisoned. The first burn (OMS-1) raised the apogee of the orbit, and the second one (OMS-2) circularized the orbit by raising the perigee.



            For STS-41C and subsequent, "direct insertion" ascents were flown. The trajectory was shaped so that a higher apogee was achieved on the main engines, and only the OMS-2 burn (it retained that name) was required.



            These graphs from the Shuttle Crew Operations Manual show the performance advantage of direct insertion missions.



            enter image description here



            Incidentally, "direct insertion" implied that the external tank was released into a higher orbit and it flew a lot further around the Earth before reentering, than it had for the standard insertion missions.



            enter image description here



            The OMS (and the aft Reaction Control Systems) were contained in pods on either side of the Orbiter's vertical tail.



            enter image description here



            Here is a cutaway drawing of the pod, with some pertinent info, from the 1985 Space Shuttle Press Reference.



            enter image description here






            share|improve this answer



















            • 1




              There was an additional OMS burn on day 02 of STS-103.
              – JdeBP
              2 days ago






            • 1




              There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
              – Organic Marble
              2 days ago















            up vote
            16
            down vote













            Since the questioner also asks "why are two needed" and the other answer didn't address that:



            Early shuttle missions flew a "standard insertion" ascent. This required two burns of the Orbital Maneuvering System after the main engines shut down and the external tank was jettisoned. The first burn (OMS-1) raised the apogee of the orbit, and the second one (OMS-2) circularized the orbit by raising the perigee.



            For STS-41C and subsequent, "direct insertion" ascents were flown. The trajectory was shaped so that a higher apogee was achieved on the main engines, and only the OMS-2 burn (it retained that name) was required.



            These graphs from the Shuttle Crew Operations Manual show the performance advantage of direct insertion missions.



            enter image description here



            Incidentally, "direct insertion" implied that the external tank was released into a higher orbit and it flew a lot further around the Earth before reentering, than it had for the standard insertion missions.



            enter image description here



            The OMS (and the aft Reaction Control Systems) were contained in pods on either side of the Orbiter's vertical tail.



            enter image description here



            Here is a cutaway drawing of the pod, with some pertinent info, from the 1985 Space Shuttle Press Reference.



            enter image description here






            share|improve this answer



















            • 1




              There was an additional OMS burn on day 02 of STS-103.
              – JdeBP
              2 days ago






            • 1




              There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
              – Organic Marble
              2 days ago













            up vote
            16
            down vote










            up vote
            16
            down vote









            Since the questioner also asks "why are two needed" and the other answer didn't address that:



            Early shuttle missions flew a "standard insertion" ascent. This required two burns of the Orbital Maneuvering System after the main engines shut down and the external tank was jettisoned. The first burn (OMS-1) raised the apogee of the orbit, and the second one (OMS-2) circularized the orbit by raising the perigee.



            For STS-41C and subsequent, "direct insertion" ascents were flown. The trajectory was shaped so that a higher apogee was achieved on the main engines, and only the OMS-2 burn (it retained that name) was required.



            These graphs from the Shuttle Crew Operations Manual show the performance advantage of direct insertion missions.



            enter image description here



            Incidentally, "direct insertion" implied that the external tank was released into a higher orbit and it flew a lot further around the Earth before reentering, than it had for the standard insertion missions.



            enter image description here



            The OMS (and the aft Reaction Control Systems) were contained in pods on either side of the Orbiter's vertical tail.



            enter image description here



            Here is a cutaway drawing of the pod, with some pertinent info, from the 1985 Space Shuttle Press Reference.



            enter image description here






            share|improve this answer















            Since the questioner also asks "why are two needed" and the other answer didn't address that:



            Early shuttle missions flew a "standard insertion" ascent. This required two burns of the Orbital Maneuvering System after the main engines shut down and the external tank was jettisoned. The first burn (OMS-1) raised the apogee of the orbit, and the second one (OMS-2) circularized the orbit by raising the perigee.



            For STS-41C and subsequent, "direct insertion" ascents were flown. The trajectory was shaped so that a higher apogee was achieved on the main engines, and only the OMS-2 burn (it retained that name) was required.



            These graphs from the Shuttle Crew Operations Manual show the performance advantage of direct insertion missions.



            enter image description here



            Incidentally, "direct insertion" implied that the external tank was released into a higher orbit and it flew a lot further around the Earth before reentering, than it had for the standard insertion missions.



            enter image description here



            The OMS (and the aft Reaction Control Systems) were contained in pods on either side of the Orbiter's vertical tail.



            enter image description here



            Here is a cutaway drawing of the pod, with some pertinent info, from the 1985 Space Shuttle Press Reference.



            enter image description here







            share|improve this answer















            share|improve this answer



            share|improve this answer








            edited Aug 3 at 1:06


























            answered Aug 3 at 0:37









            Organic Marble

            44.5k2113191




            44.5k2113191







            • 1




              There was an additional OMS burn on day 02 of STS-103.
              – JdeBP
              2 days ago






            • 1




              There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
              – Organic Marble
              2 days ago













            • 1




              There was an additional OMS burn on day 02 of STS-103.
              – JdeBP
              2 days ago






            • 1




              There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
              – Organic Marble
              2 days ago








            1




            1




            There was an additional OMS burn on day 02 of STS-103.
            – JdeBP
            2 days ago




            There was an additional OMS burn on day 02 of STS-103.
            – JdeBP
            2 days ago




            1




            1




            There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
            – Organic Marble
            2 days ago





            There were many additional OMS burns for deorbit, rendezvous, etc. STS-39 had 16 of them. space.stackexchange.com/questions/17687/…
            – Organic Marble
            2 days ago













             

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